WO1998007984A1

WO1998007984A1 - Motor propulsion unit having improved efficiency

Info

Publication number: WO1998007984A1
Application number: PCT/SE1997/001394
Authority: WO
Inventors: Dragoljub Perunicic
Original assignee: Dragoljub Perunicic
Priority date: 1996-08-23
Filing date: 1997-08-22
Publication date: 1998-02-26
Also published as: AU3876397A

Abstract

A wind motor propulsion unit (60) for a generator (6) comprising at least two propellers (64) different in diameter which freely rotate on a shaft (61) of the generator (6) and centrifugal clutches (38) which couple the shaft (61) and the propellers (64) when each achieves certain rotational speed. The generator (6) is mounted on a pole (63) or a frame (23) of two captive rigid balloons (24) having a direction fin (15) to direct the smallest propeller (64) to wind first. The poles of generator rotor (455) having at least two armature windings (456) each having ends connected to a centrifugal switch (449) to close circuit at certain rotational rate of the shaft (61). The armature windings (456) are connected to stationary brushes (458) through slip rings (457) mounted on the shaft (61). The poles of stator generator (453) are of permanent magnets (454). A number of activated propeller (64) and armature windings (456) is in relation to rotational speed which is in relation to velocity of wind and the altitude of the unit (60).

Description

MOTOR PROPULSION UNIT HAVING IMPROVED EFFICIENCY D e s c r i p t i o n Technical Field The present invention relates to a group of invention which harness the kinetic energy of a fluid stream into mechanical motion directly or indirectly and more particularly to motors, turbines and generators Those inventions are technically linked in harnessing the energy of a fluid stream for production of mechanical motion up to the end use forming a single general inventive concept The technical features of each invention of the group are improved in a comparison with the prior art improving features of the group Background Art

In a prior art, a turbine which is disclosed in the international patent application no W097/15491 includes a wind driven turbine which drιves(propels) a water turbine, both coupled to a shaft, which rotates about a vertical axis T e wind turbine uses a principle of a revolving crank of crankshaft The turbine is coupled to a direction fin in order to obtain a desired blade motion or alternating anagular deflections in relation to position of blade on an orbit of crank adjustable relative to the wind direction

The centrifugal force of water turbine takes water out from the center of turbine during rotation of turbine blades The water turbine includes two or more layers of blades or two or more turbines and a remote control cylinder disposable in a gap of ring plate, which couples the layers During fluctuation in velocity of wind, the remote control cylinder adjusts a trust of output water flow just according to strenght of the wind, so that the wind driven turbine and water propulsion turbine perform high efficiency in comparison with a prior art instalation, which are generally constructed to be actuated by one certain flow under optimum conditions, otherwise becomes complitly ineffective If the water turbine is driven with a gasoline motor, the remote control cylinder determinates output water and trust of the water, so that speed can be changed without a gear box and a transmission

The disclosed features in said application W097/15491 are developed in the present invention in order to be used for other application basically using said pπncliples of cranks and multi-layered centnfugal turbine to contribute to the prior art

In the prior art, blades of an air- propeller, for the same radius can not change surface without changing a rotational speed In prior art a higher altitude of a wind turbine is achieved with a higher pole or tower In prior art, all unit must be turned to achieve a position of porpeller against wind In prior art a propeller which rotates about a horizontal axis, in some application (pump or craft) can not transfer a rotational force directly without mechanical transmission In prior art, a turbine of craft with propeller is generally constructed to be actuated by one certain flow under optimum conditions, otherwise becomes useless In prior art, a propeller of aircraft draggs wings which make lifting pressure

In prior art, a speed of a vehicle or a craft, which uses a gasoline motor is changed with a gear box so the motor must operate a high and vanble rpm In prior art, a turbo engine of airplane compress fuel-air mixture with a wide propeller while a small propeller rotates the wide propeller Exhausted gas, after each explosion, expands in all direction pushing blades of the small turbine and the wall of the housing so that kinetical energy of exhausted gas is partly absorbed by the wall of the housing In prior art, internal combustion chambers or cylinders of a gasoline engine are stationary so walls of cylinder partly absorb kinetical energy of expanded gas In prior art, a gasoline engine of a vehicle operates at high and variable rpm mechanically shifting speed and transmiting entire power to front or rear wheels In prior art, constant frequency generating systems, as such disclosed in Jordan s U S Patent No. 4,246,531 , include an exciter stator which is not rotatable and a prime mover output shaft which rotational rate in operation may vary below, but preferably above and not at electrical synchronous speed Such system can not operate when the shaft sometimes or most of time rotates at the synchronous speed In prior art, constant frequency generating systems, as such disclosed in Hucker s Patent No WO86/03907, include rectifiers, field inventors, converters, a damper cage and a wound field exciter or a pemanent magnet exciter in which permanent magnets are disposed in a housing of the exciter The housing is driven by a sprocket disposed on a shaft, including a ring gear and a spur gear to counter-rotate relative to the rotor to increase the relative speed of the exciter in order to reduce the exciter magnetic weight The damper cage minimizes the entire output power variation In prior art, a rotary machine, as disclosed in International Patent No WO 90/03061 includes a stator which acts as torque on a rotor, and at the same time, the rotor also acts on the stator due to the magnetic repulsion and attraction force of the stator and the rotor magnetic poles. Such machine is used as a motive power source for a load which requires the rotational force of different direction of rotation

In prior art, a low-speed generator, in order to increase frequency requires more armature pole windings in a stator or gears to increase rotational speed of a rotor. In prior art, high-speed generator, in order to reduce frequency, requires a special mechanical means to reduce high rotational speed to generate a desired frequency In prior art, a low-driven generator by an alternative energy(wιnd, wave) generates AC output which is rectified in DC, as the generator can not achieve constant output frequency.

In prior, a counter-emf influents on the generator when the generator is coupled to an electric motor, which is under load. Disclosure of the Invention When one set, which consisting of wings, a direction fin and a coupling set, as an individual unit is disposed on the end of each rotor arm, such rotor increases a torque as the lenght of arm is longer Such set may increase surface of each wing without changing radius of the turbine and rotational speed of the rotor If the wind motor-driven generator is disposed on a capitve rigid balloon, a higher efficiency of the motor will be achieved in comparison with the same unit used on the ground due to velocitiy of wind, which increases with a higher altitude A rope, which couples the balloon with an object on the ground or on the craft may change the altitude of the balloon so an adjustment to velocity of wind could be achieved For the same output from the generator on the balloon and one on the ground, the rotor of wind turbine on the ground must have much greater radius then the radius of rotor of wind turbine on the balloon The smaller blades of the present wind turbine at the high alltitude produce less nose.

A level of the water in two coupled containers is the same if the same air pressure is applied on both containers. In the container in which air-pressure drops, level of the water increases. If a container having water on the ground is coupled with a flexiblile hose to a container which is located on a captive rigid balloon, a level of water in the container on the balloon is increased due to a low-air pressure in area around the balloon. New coming water in the container on the ground increases the level of water in both containers at the same time, but on different altitude. Surplus of new coming water from the high altitude or from the container on the balloon falls through another flexibile tube to low altitude to a water turbine with a generator on the ground so a higher water potential is achieved in comparison with relatively small kinetical energy of the incoming water.

If a boiler or container having a freoπ gas, is located on a captive rigid balloon, a magnifying glass on the top of the container and/or a bottom conical mirrors focus sun^'s rays and heat the cooled luiqud freon gas. The gas evaporates driving a gas turbine. The steam of gas is condensated in a heat exchaner which is located at the balloon at low-air temperature around. The gas become luiquid before coming back to the container. A compresor controls a pressure and a point of boiling in the boiler.

The sun^'s rays produce more heat on the altitude of the balloon then on the ground. The turbine which is driven by wind or termo energy drives a generator. The generated electricity is delivered to consumers on the ground or on the craft through a cable. Two captive rigid balloons, which are coupled with a frame, are filled up with helium or freon or similer gas.

The above mentioned power plants could be located much closer to consumers, so there is no need to use or to invest in a very long transmission line, transformers, a huge dam and big generators. Those above mentioned "sources" are unexpendable.

Each time during starting up a motor of an aircraft or a vehicle or craft or machine, a consumption of fuel( gasoline; kβrosine; diesel) is very high due to a heavy load, a resistance, a gravitation, or so. To overcome a requirement for a high torque in the start, the motor must operate at a higher power rate, what causes the high consumption of the fuel.

An elevator may lift up an aircraft on a taking off platform, which is coupled with two captive rigid balloons on a higher altitude.

A runway on the balloon having direction fins, is always automaticaly directed toward the wind as the platform is pivotaly coupled to a rope, which is coupled to the ground. The aircraft should be fasten untill the motor achieves enough power to overcome velocity of the wind. The craft should take off in a direction against the wind. The high velocity of wind may partly interact with wings of the airplane to produce a lifting pressure. Two insulated cylindrical boilers or rigid balloons filled up with freon gas, which are mounted to the wings of the aircraft, may lift the aircraft at a high altitude without using the aircraft^'s motor. An electricity from a network on the ground heats a gas in the boilers while the airplane is on the ground so that the gas evaporates. The aircraft become lighter. A compressor from the ground could control a boiling point and the pressure. The motor of the arcraft should control a taking off and a speed during a flight. During such flight a heater and a compressor, which are coupled to a battery or a generator located on the aircraft may control the altitude. Before landing, the gas freon from the boiler flows through a heat exchanger, which is located outside of the airplane. The gas becomes luquid geting on weight. The aircraft become gradually heavier for landing. There is no need that the aircraft carry the fuel, which is required for taking off and to have a strong and heavy motor. The conusmption of the fuel for lifting of the aircraft is less then the fuel required for taking off on the conventional way, so one part of energy of fuel could be saved. A propeller or jet or turbo engine of an airplane draggs the wings as the airplane going ahead. After, the airplane achieves required speed the wings, due to aerodynamical configuration or a difference in air-pressures between a convex upper and bottom flat part of wings, produce enough lifting pressure to lift the airplane.

A new propeller or turbine consisting of two or more blades having aerodynamical configuration, which are radially coupled to a vertically rotating shaft of the engine, produces a lifting pressure in a cycle, which lifts the aircraft only upward.

A new crankshaft turbine consisting of a blade which is coupled to a crank of a verticaly(or horizontaly) rotating crankshaft may lift and dragg the aircraft with the same turbine.

The airplane with such propeller or turbine may take off or land almost verticaly without any need for a conventional runway(as a helicopter which uses a conventional horizontaly disposed propeller rotating around a vertical axis). The stationary walls of cylinders of the gasoline engine of aircraft or craft or vehicle partly absorb energy

If a centrifugal turbine or pump has an internal combustion chamber in a hole or holes of a centrifugal pump or multy-layered turbine, the absorbtion of kinetical energy of an expanded gas, by the stationary walls, is less.

If a cylinder of the conventional internal combustion piston-cylinder engine is coupled to a crank of the crankshaft, such cylinder acts as a torque on the crankshaft so that the absorbtion of kinetical energy of exploded gas, by the cylinder, is less If a remote control cylinder, which determines number of internal combustion chambers in operation or different diameter centrifugal turbines or different radius of cranks of the crankshaft are in used, the changes of speed are possibe without a mechanical transmission and a box gears Also, the engine or motor may operate at a lower rotational rate, when its required, instead to operate all the time at full power rate as prior art The exhausted gas, after leaving the motor or engine, still takes a lot of heat and kinetical energy. Such energy is lost, producing a global overheating Drops of water, which are dispersed in the internal combustion chamber or the hole of the centrifugal turbine, evaporate so kinetical energy of steam rotates the turbine too This motor is applicable for a craft or generator or a machine The centrifugal pump could be used as a compression unit, but more preferably as a propulsion unit for a craft Generating electricity without a turbine and a rotor of generator could save an energy and cut an investment in production of electricity and maintenance of machines with mechanically rotating parts If a part of conductivity of each coil of insulated wire of a wιndιπg(whιch is supplied with an electrical current) is achieved through fluid as gas or water(whιch is able to conduct electricity), fregments of such fluid flow due to interaction between the magnetic field produced in this fragments by electric current and another stationary magnetic field. Such device operates as a pump

If the fluid flow between the stationary magnetic field, an electric current will be produced in the wire coil of the winding if such fluιd(gas or water) is able to conduct electric current. Such device operates as a generator. This rotorless generator is applicable for an atomic power plant, where produced steam have a very high speed and strength A kinetic energy of fluid will be directly converted (without a turbine) to an electric current Such coil, which wires are disconnected with the fluid operate as any other regular coil, if the end of such disconnected wire have the shortest distance therebetween to make a short-circuit of current A generator, which is driven by a variable-speed source(as wind or runing water or wave or so) may produce a constant frequency output if such generator comprising a secondary motor with exciter or brushes Such generator, if the motive power source is not strong enough could take a difference in energy from a network This generator saves energy as much it may produce A rest will be taken from the network(otherwise all energy is taken from the network) The current from the network secures a constant frequency output A rotor of a small motor which is mounted on a shaft of prime mover, rotates a stator of the motor and a housing at a synchronous speed around the shaft in the counter direction from the rotational direction of the shaft The exciter, which is located in the housing, generates in an exciter rotor, which is fixedly mounted to the shaft and coupled to the rotor of a main generator needed difference in frequency and power to achieved a constant frequency output A reciprocating armature, which is movable located between two electric magnets, interacts with the magnets when DC or AC current supplies windings of magnets and armature As the armature moves, the current circuit is disconnected and a new current circuit follows, making attraction in the opposite direction and so on Connecting a current circuit through a gas or vacum or area with slight harmless radiation (disposing the armature and the magnets in a gas chamber) DC will be connverted in AC or AC will be converted in DC without a mechanical contact or a pulsating device (which produce a pulsating curent) or so Attraction forces between the armature and the stationary magnets determines a speed of the armature^'s movement and a frequency of current As such attraction forces is very easy to regulate its makes an advantage in producing of wanted frequency If windings of the stationary magnets are supplied with AC, the armature will oscilate at the same speed as the speed of the magnetic field of the supplied current alternatively connecting or disconnecting a current circuit, so AC will be rectified in DC, operating as a rectifier Having two slip rings and a commutator in two separate parts mounted on a shaft of small motor, a curent circuit which will be made through a conductive gas or vacum will change DC into AC or vice versa when the motor rotates This and previous mentioned conventer or rectifier may operate if indirect electrical contacts are designed to close circuit at the shortest way

Brief Description of the Drawings A number of each figure which illustrates a unit or a part of the unit in the drawings corresponds to the number of claim in which such unit or the part of unit is disclosed or discπbed in the claιm(s)

Figs 1-10 illustrate a wind motor which has two types of turbines and two types of wings and two types of coupling sets,

Fig 11 illustrates a wind motor having different diameter of conventional propellers, Figs 12 15 illustrate devices which drives a centrifugal turbine,

Figs 16-17 illustrate two types of turbine driven by water,

Figr 18-21 illustrate two types of device for harnessing wave energy

Fig 22 and Fιg.24 illustrate a device using solar energy,

Fιg.23 illustrates a turbine driven by water or steam, Figs 25-36 illustrate fuel motors having different types of centrifugal turbine, which have an internal combustion chamber

Fιgs.37-45 illustrate fuel motors having different types of reciprocating cylinder, as an internal combustion chamber

Figs 46-48 illustrate fuel motors having stationary cylinders, Figs 49-55 illustrate two types of propulsion turbine,

Figs.56-61 illustrate different types of device for lifting off an aircraft,

Figs.62-70 illustrate a turboless and rotorless generator or pump,

Figs 71 -79 illustrate variable speed generators,

Fιgs.80-85 illustrate generators or motors having reciprocating selenoid and magnet, Figs 86-89 illustrate different types of electric motors,

Fιgs.90-94 illustrate conventers or rectifiers,

Fιgs.95 illustrates a reciprocating pump or compressor,

Fιgs.96-97 illustrate reciprocating wind driven and propuslsion turbines for a craft, Fig 98 illustrates a wind driven generator, Fig 99 ilustrates a device for harnessing of surples of steam Fig 100 illustrates an improvement for solar collector Best Mode for Carrying Out the Invention The wind motors as shown in Figs 5,1 1 ,98 and the water motors as shown in Figs 16,17,23 are driven by a variable motive power of fluιd(wιnd,water) As those motor having different diameter of turbines, such motor may be driven by different speed and different strenght of a fluid stream in order to extract maximum available kinetical energy of a fluid stream At the same time the wind driven or water dirven motor drives only one propulsion unit as a generator, which is shown in

The wind driven motor drives a water propulsion unit as a centrifugal water turbine shown in Fig.50 or a crankshaft turbine shown in Fig 53 The centrifugal and crankshaft turbines also have different diameters and different output trust to match to the energy of wind stream The variable speed driven generators shown in Figs 74,76,77 also have different diameter of rotor to match and to extract corresponding energy of fluid

The consumption units, as electric motors, as shown in Figr 81 84,86,88 and 89 require from the generators or network different energy for start and different energy for opperation The consumption units, which use fuel motors as shown in Figs 26,27,30,31 ,32,34,35,41 ,42,47,48 require different energy from such motors for the start and for the operation As such motors having different diameter of turbines such motor may change rotational speed and torque to match the rotational speed and torque which is required by the consumption unit In the start, when speed of consumption unit is low, a high torque is required so the greater diameter of layers of centrifugal turbine or crank of crankshaft turbine would be used As speed incresed the smallest size of turbines will be used As such small turbine do not require the same power as the power which is required by the greater turbine a consumption of fuel will be adjusted according to the requirement and saving of fuel will be achieved This is an advantage in comparison with a conventional fuel motor which operates all the time at high rotational speed to be ready for any fluctuation in requirement irrespectively from the real requirement from the consumption unit

Claims

1 A wind motor propulsion unιt(1 ) for an object(2) as a craft(3) or an aιrcraft(4) or a pump(5) or a generator(6) comprising a wind turbιne(7) which is mounted to a vertical rotatable shaft(8) to provide propulsion of the object(2) on rotation of the turbιne(7) by the wind, wherein the turbιne(7) comprising a rotor(9) which consists of two or more radially disposed arms(10) or cranks(1 1) each of which mounted on the vertical shaft(8), two or more wing frames(12) each of which having one or two wιngs(13), one or more direction frame(14) each of which having a direction fιn(15), two or more coupling sets(16), each of which couples the wing frame(12) and the direction frame(14), a secundary wing frame(17) which is fixdely mounted to the wing frame(12) at an angle of 90 degrees at the place where the wing frame(12) rotates around a vertical axis a secundary direction frame(18) which is fixedly mounted to the direction frame(14) at an angle of 90 degrees at the place where the direction frame(14) rotates around a vertical axis, a supporting frame(19) of object(2) which supports the rotatable shaft(8), wherein each wιng(13) and each fιn(15) comprising a canvas(20) or double side convex plate(21) of aerodinamical configuration, wherein the rotor rotates by wind irrespectively from the wind direction, characterized in that the coupling set(16) and the direction frame(14) change the angular deflection of wιng(s)(13) against the wind alternately adjusting the deflection of wιng(13) according to the positions of wιng(s)(13) on an orbιt(22) of rotor to achieve a rotation in the same direction.

2 A wind motor propulsion unιt(1 ) according to claim 1 , wherein the supporting frame(19) of wind turbine (7) is located on a frame(23) which is coupled between two captive rigid balloon(24), characterized in that the frame of balloon(23) carries the generator(6) and the wind motor propulsion unιt(1 ) at a high altitude, wherein a rope(25) couples the bailoon(24) with an object(2) on the ground or on the water or in the air, wherein a spool(26) winds up or rewinds the rope(25), wherein a cable(27) couples the generator(6) and an apparatus(28) of object(2) on the ground or on water(craft) or in aιr(other balloon), wherein a spool (26) winds up or rewinds the cable(27), wherein the cable(27) delivers an electrical current to a network(29) or the apparatus(28) on the ground or an electric motor(30) of vehιcle(31 ) or a craft(3) or a machιne(32), wherein each section of balloon(24) which is filled up with helium or other light gas consisting of cylindrical long body(33) with a direction fιn(34), wherein the balloon (24) floating in air following the direction of wind, characterized in that with winding or rewinding the rope(25) the balloon(24) decreases or increases the altitude so that the wind turbιne(7) is protected against excessive rotation maintaining the nominal number of revolution or synchronous speed in relation to the strenght of wind, characterized in that to increase or decrease a rotational rate of the turbιne(7) the balloon(24) needs to increase or decrease an altitude

3 A wind motor propulsion unιt(1 ) according to claim 1 , wherein the arm of rotor(10) is mounted on the shaft(8), wherein each arm(10) comprising a pair of stationary crank(35) which aligned with the arm of rotor(10), a pair of vertical axis of crank (36) , each of which couple the arm of rotor(10) and the crank(35), wherein each direction frame( 4) is rotatable mounted on the axis of crank(36), wherein each wing frame(12) is rotatable mounted on a vertical arm of crank(37), wherein the secundary wing frame(17) is longer then the crank(35),

4 A wind motor propulsion unιt(1 ) according to claim 1 , wherein each crank(1 1 ) of rotor is fixedly mounted on the shaft(8), wherein each wing frame(12) is rotatable mounted to the vertical arm of crank(37), wherein the direction frame(14) is rotatable mounted on the shaft(8), wherein the secundary wing frame(17) is longer then the crank(1 1 )

5 A wind motor propulsion unιt(1 ) according to claim 1 , wherein the wind turbιne(7) comprising two or more rotors(9) each of which having a different diameter of arm(10), wherein the rotor(9) freely rotates around the shaft(8), wherein each rotor(9) includes a centrifugal clutch (38) which couples the shaft(8) and a central ring of rotor{39) if the rotor(9) is driven by wind, characterized in that the centrifugal clutch(38) comprising a balast(40) which frame(41) is coupled to first spπng(42) and first pin of central rιng(43) on one side of the central rιng(39) and coupled to second pιn(44) and second spnng(45) on another side of the central rιng(39), wherein first pιn(43) slides in a hole of balast(46), wherein second pιn(44) slides in a hole of central rιng(47) to couple the shaft(8) having coupling pιns(48) or holes, characterized in that the number of rotor(9) which rotate the shaft(8) is in relation to velocity and strenght of wind.

6. A wind motor propulsion unιt(1 ) according to claim 1, wherein the wing frame(12) comprising two wιngs(13), each of which located on the opposite side from the rotational axis of frame(12), charactenzed in that both wιngs(13) of the frame(12) are in a balance if attacked by the wind, characterized in that wιngs(13) of the wing frame(12) if attacked by wind rotate the arm(10) or crank of rotor(11 ) during all positions of wιngs(13) except if wιngs(13) of wing frame(12) are parallel to the fιn(15) of the direction frame(14) 7 A wind motor propulsion unιt(1) according to claim 1 , wherein the wing frame(12) comprising one wιng(13) which is located on the opposite side relative to the direction fιn(15), characterized in that the wιng(13) and the direction fιn(15) are in a balance if attacked by wind rotating the arm(10) or crank of rotor(11) during all positions of wιng(13) except if the wιπg(13) and the fin(15) are parallel

8 A wind motor propulsion unιt(1) according to claim 1 , wherein the secundary wing frame(17) includes a vertical rod(49) which is pivotaly couple to one lιnk(50) or two links, characterized in that the lιnk(50) slides along an arm of secundary direction frame(51 ) during rotation of arm(10) or crank of rotor(11 ) and the direction frame(14)

9 A wind motor propulsion unιt(1 ) according to claim 1 , wherein the secundary wing frame(17) includes a vertical rod(52) which is pivotaly coupled to an extensible set(53) of the secundary direction frame(18), wherein the extensible set(53) consists of a rod(54) inserted in first tube(55) which is inserted in second tube (56) all coupled together, characterized in that the extensible set(53) changes the lenght during rotation of the arm(10) or the crank of rotor(1 1 ) and the direction frame(14)

10. A wind motor propulsion unιt(1 ) according to claim 1 , wherein the horizontal arms(57) of stationary crank(35) consists of two shock-absorbers(57), characterized in that centrifugal force during high rotational speed of rotor due to a high wind velocity pushs back an extensible rod(59) of shock-absorbers (57) with the wing frame(12) on it to reduce an angular deflection between a wιng(13) or wings and the direction fιn(15) reducing the speed of turbιne(7)

1 1. A wind motor propulsion unιt(60) for a generator(6) comprising: a horizontal shaft(61 ) which is rotatable mounted on a supporting frame of unιt(62) coupled to a high pole(63) or to the frame(23) of two captive rigid balloons(24), one or more generators (6), two or more different in size wind propellers (64) each of which freely mounted on the shaft(61), two or more centrifugal clutches(38) each of which operates for a different rotational speed to couple the shaft(8) and a central ring of propeller(39) when the propeller(64) achieves a certain rotational speed, wherein each propeller(64) consists of two or more radially disposed arms(65) and blades of rotor(66), wherein propellers (64) having different lenghts of arm(65) and blade(66), wherein each centrifugal clutch(38) comprising a balast(40) which frame(41 ) is coupled to first spnng(42) and first pιn(43) of the central rιng(39) on one side of the central rιng(39) and coupled to second pιn(44) and second sprιng(45) on another side of the central rιng(39), wherein first pιn(43) slides in a hole of balast(46), wherein second pιn(44) slides in a hole of central rιng(47) to couple the shaft(8) having coupling pιns(48) or holes, characterized in that the blades(66) of the small size propeller(64) are exposed to the wind stream first, characterized in that the blades(66) of each propeller(64) do not shield blades(66) of other propeller(64), characterized in that a number of propeller(64) which transfer a rotational force to the shaft(8) is in relation to the velocity and strenght of wind 12 A water motor propulsion unιt(67) for a generator(6) comprising a generator(6) having a centrifugal water turbιne(68) or a rotorless generator(69) which is located on the ground, a captive rigid balloon(24) consisting of two cylindrical long body(33) or balasts each of which filled with helium or other light gas having a direction fιn(34), one main contaιner(or resevoιr(s)(70) which is located on the ground or on a tower(72), one secondary coπtaιner(mιnι dam) (71) which is located at the frame of balloons(23) or on the tower(72), two flexible hoses one for ιnflowιng(73) and another one for outflowing (74) water, wherein the main contaιner(70) is larger in size in comparison with the secondary contaιner(71 ) which is smaller in size, wherein both contaιners(70,71 ) are coupled together through the inflowing hose(73), wherein the outfloing hose(74) couples the secondary contaιner(71 ) and the water turbιne(68) or the fluid propulsion generator(69) 13. A water motor propulsion unιt(67) according to claim 12, wherein water inflows in the main contaιner(70) which is located on the ground, wherein the secondary contaιner(71 ) is located on the balloon(24), wherein the water in both contaιners(70,71) achieve a balance in relation to the water and air pressure, wherein a level of water in the secondary contaιner(71 ) is lifted up by a low pressure, wherein such low-pressure keeps a higher water level in the secondary contaιner(71), characterized in that inflowing water in the main contaιner(70) increases water level in both containers (70, 71 ) at the same time characterized in that water in the secondary contaιner(71 ) is on a higher level in comparison with water lever in the main contaιner/70) due to a difference in air- pressures, characterized in that water potential of the outflowing water from the secondary contaιner(71 ) is in relation to the alltitude of the balloon(24), characterized in that the water level in the secondary contaιner(71) is in relation to the air-pressure in the secondary contaιner(71 ), wherein high strength of the outflowing water drives the generator(6), wherein outflowing water supplies a water or an irrigation station

14 A water motor propulsion unιt(67) according to claim 12, whenn the main contaιner(70) which is located on the ground consisting of a conical water boιler(75) having a top magnifying glass(76), wherein the boιler(75) is surrounded by a convex mιrror(77), wherein the secondary contaιner(71) which is located on the balloon(24) is closed, wherein the boιler(75) is located in a focus of the sun s rays reflected by the mιrror(77) heating water producing steam, wherein the magnifying glass(76) focus the sun s rays heating water in the boιler(75) producing steam, wherein steam through the hose(73) inflows in the secondary contaιner(71 ), wherein a condensation is occured in the secondary contaιner(71 ) due to low-temperature on the balloon(24) so water outflowing from the secondary contaιner(71) through the hose(74) to the centrifugal turbιne(68) or the fluid propulsion generator(69).

15. A water motor propulsin unιt(67) according to claim 12, wherein the secondary contaιner(71 ) is located on a tower(72) or on the balloon(24), wherein the secondary contaιner(71 ) is hermeticaly closed, wherein the secondary contaιner(71 ) is filled up with water, wherein water level in the secondary contaιner(71) is lifted up by a low pressure which is produced by a vacum pump(5), wherein low-pressure keeps a higher water level in the secondary contaιner(71), wherein the centrifugal turbιne(68) or the fluid propulsion generator(69) is located on the ground level which is below water level of the main contaιner(70), characterized in that the water level in the secondary contaιner(71 ) is in relation to the air-pressure in the secondary contaιner(71 ), characterized in that a water potential of the outflowing water from the secondary contaιner(71 ) is in a relation to the alltitude of the tower(72) or the balloon(24), wherein a high strength of outflowing water from the secondary contaιner(71 ) drives the generator(6), wherein outflowing water supplies a water or an irrigation station. 16 A water motor propulsion unιt(67) according to claim 12, wherein the centrifugal water turbιne(68) comprising a single conical layer(78) of turbine consisting of a wide top ring plate(79) and a narrow bottom ring plate(80) and a plurality of blades(81 ) each of which fixedly and radially mounted between sides of two rings (79,80), a conical housing (82) of turbine having an extension

05 openιng(83) located on conical side of the housιng(82) for outflowing water, a vertical inflowing tube(84) which is coupled to the wide hole of housιng(82) for inflowing water, a shaft(85) of turbine which is rotatable located in the housing (82), a cross-rods (86) which couples the wide ring plate (79) and the shaft(85), a dιsk(87) which couples the narrow ring plate(80) with the shaft(85), wherein water inflows through hole of the wide ring plate(79), wherein the shaft(85) drives the generator(6) ,

10 characterized in that if strength of the inflowing water increases or decrease the level of water, which attacks on blades of the turbιne(81 ) between the top and bottom ring plates(79,80) then speed and torque of turbine increases or decreases accordingly so that any water stream may drive the turbιne(68) in such range irrespectively from size of the turbιne(68), characterized in that such turbιne(68) is used if the water stream is changable

15 17 A water motor propulsion unιt(67) according to claim 12, wherein the centrifugal water turbιne(68) comprising, two or more conical layers (78) of turbine each of which consisting of a wide- top ring plate(79) and a narrow-bottom πng plate(80) and a plurality of blades(81) which are fixedly mounted between sides of two rings plates (79,80), a conical housιng(82) of turbine having two or more extension openιngs(83) located on the conical side of housιng(82) for outflowing water, a

20 vertical inflowing tube(84) which is coupled to the wide hole of housιng(82) for inflowing water, a tubular shaft(88) of turbine which is rotatable located on the shaft (85), two different size generators(6) one coupled to the shaft(85) and another one coupled to the tubular shaft(88), a cross- rods(86) which couples the wide πng plate(79) of each layer(78) with the shaft(85) or with the tubular shaft(88) respectively, a dιsk(87) which couples the narrow ring plate(80) of each layer(78) with the 5 shaft(85) and the tubular shaft(88) respectively; wherein water inflows from the wide hole of turbιne(68), wherein the shaft(85) and the tubular shaft(88) drive the generators(6), characterized in that if the strength of the inflow water increases or decrease then the different layers (78) are attacked by water so torque and speed of one or both turbines increase or decrease accordingly, charactenzθd in that such turbιne(68) is used if the water stream is changable 18 A water/wave motor propulsion (89) unit for a generator(6) comprising a generator(6) having a centrifugal turbιne(90) or a rotorless generator(69), a stationary pιston(91 ) which is located just above a level of ocean or sea water, a water tower(92) consisting of a vertical inflow/outflow tube(93) 5 which is fixedly mounted to the stationary pιston(91 ), a floating reciprocating open top cylιnder(94) which is reciprocated by wave relative to the stationary pιston(91 ), wherein the cylιnder(94) receives water if level of water falls, wherein wave lifts the cylιnder(94) pushing water in the inflow/outflow tube(93), wherein water outflows from the tube(93) when the cylιnder(94) drops following wave making a space for an incoming water from the tube{93) characterized in that alternatating inflowing

10 and outflowing water drives the centrifugal turbιne(90) of the generator(6) or the fluid propulsion generator(69)

19. An air/wave motor propulsion unιt(95) for a generator(6) comprising a generator(6) having a centrifugal turbιne(90) or a generator(6) having a centrifugal piston turbιne(96) or a rotorless generator(69), a cave or down-turn hull(97) having air between water or wave and the top

15 coverιng(98), wherein the generator(6) is located on the top coverιng(98), characterized in that the generator(6) is driven by an alternating outflowing stream of the air which is produced by the wave pressure on the air in the down-turned hull(97) or the cave and an inflowing stream of the air which inflowing in the hull (97) or cave due to a low pressure which is produced by falling level of the water 20 A propulsion unιt(89,95) according to claim 18 or 19, wherein the centrifugal turbιne(90)

20 comprising, a number of conventional concav blades(99) or convex/flat blades which are radially mounted between a bottom and a top ring plate(100,101), a stationary cylindrical housιng(102) which surrounding the blades of turbιne(99), two openιngs(103 104) each of which unsymetπcaly and diametrically located on the opposite cylindrical side of the housιng(102), characterized in that the turbιne(90,96) rotates in the same direction irrespectively from direction of the fluid stream

2521 A propulsion unιt(95) according to claim 19, wherein the centrifugal piston turbιne(96) comprising, a centrifugal turbιne(105) which is coupled with a reciprocating pιston(106), a stationary cylindrical housιπg(107), two cylindrical housing extensιons(108,109) of the housιng(107), two open- top turbine extensιons(110,1 11 ) of the turbιne(105) each of which coupled with one of holes(113) of the ring plate(1 12), a valve(1 14), two turbine brιdges(1 15,1 16) of the turbine extension^ 10,11 1 ), two housing brιdges(1 17,118) of the housing extensιons(108, 109), two shafts(119,120) which are rotatable mounted through the brιdges(1 10,1 1 1 ) to the housιng(107), a housing openιng(121 ) on cylindrical side of the housιng(107), two valve openιngs(122) of the valve(114), wherein the valve(1 14) is mounted on the housing openιng(121 ), characterized in that the pιston(106) alternates by inflowing or outflowing stream from one turbine

10) to another extensιon(111) and vice versa, characterized in that the pιston(106) directs air to the layer of the turbιne(105) from fπst and second extensιon(1 10 111 ) alternatively, characterized in that piston of the valve(123) and the pιston(106) of the tuπbine operate asynchronously so when the top turbine

10) is open then the top extension of valve(123) is closed and vice versa both pιston(106,123) being activated by the inflowing or outflowing stream alternataly

22. A solar motor propulsion unιt(124) for a generator(6) comprising a generator(6) having a centrifugal turbιne(90) or a rotorless generator(69), a heat exchanger(125), two captive rigid balloons(24) filled up with helium consisting of two body(33) coupled with the frame(23), a compressor) 126), a conical boιler(75) having a gas freon or so which is located with a wide opening upward on the frame(23) of balloons(24), a magnifying glass(76) which is hermeticaly mounted on the wide top opening of boιler(75), a convex mιrror(77) which is located on the frame(23) of balloons(24) surrounding the boιler(75), a cable(27) which transfers electric current to an apparatus(28) or an electric motor(30) on the ground, a rope(25) which couples the balloon(24) with an object(2) on the ground or water or air wherein the boιler(75) is located in a focus of the sun s rays reflected by the mιrror(77) heating gas producing steam, wherein the magnifying glass(76) focus the sun s rays heating the gas in the boιler(75) producing steam, wherein steam through a tube(127) inflows in the centrifugal turbιne(90) or in the rotorless generator(69), wherein steam drives the turbιne(90) with the generator(6) or directly converting a mechnical energy in an electrical current through the fluid generator(69), wherein gas outflows from the turbιne(90) through a tube(128) to the heat exchanged 125) where a condensation is occured due to low-temperature so the gas become luquid, wherein luquid gas through the compressor(126) and the outflow tube (128) coming back in the boιler(75), wherein the compressor^ 26) regulates a pressure and a boiling point of gas, wherein the compressor 126) is driven by an electric motor(30) which receives current from a battery or the generator(6), characterized in that as a low-temperature and a strenght of the sun s rays are in relation with an altitude the cooling and heating of gas in the boιler(75) are increased or decreased if the altitude of the balloon (24) is increased or decreased

0523 A propulsion unιt(67,124) according to claim 12 or 22, wherein the centrifugal turbιne(67) comprising two or more cylindrical layers(129) of turbine each of which consisting of ring plates(130,131) and a plurality of blades(132) of turbine which are fixedly mounted between sides of two ring plates(130,131 ), a cylindrical housιng(133) of turbine having two or more openιngs(134) located on the cylindrical side, a remote control cylιnder(135) of turbine which reciprocating between

10 inner edges of blades(132) and holes of ring plates(136), a shaft(137) of turbine which is rotatable located at the housιng(133), a dιsk(138) or cross-bars (139) or propeller(140) which couples the last ring plate (130) and the shaft(137), wherein all holes of ring plates (136) having the same diameter, wherein the control cylιnder(135) is coupled to an inflowing tube(141 ) by a flexible hose(142), wherein water inflows from another tube(143) and another housing openιng(144) on the flat side if

15 any through the cross-bars(139) or propeller(140), wherein the control cylιnder(135) slides along the inner side of a squirrel cage(145) which is mounted on the flat side of the housing openιng(146), characterized in that the control cylιnder(135) couples a fluid stream and layers of the turbιne(129) increasing or decreasing outflow from the layers of turbιne(129) and from the housιng(133), characterized in that the control cylιnder(135) determines speed and output rotational rate of the

20 shaft(137) 24. A propulsion unιt(124) according to claim 22, wherein the propulsion unιt(124) for the generator(6) comprising a plurality of conical boιlers(75) each with gas(freon or so) and a top covering magnifying glass(76) which are located in a focus of a concav mιrror(s)(77) collecting sun s rays, wherein each boιler(75) is coupled through the secundary inflowing and outflowing tubes

25 to the mam inflowing and outflowing tubes respectively, wherein the mam inflowing and outflowing tubes (147, 148) collecting and conducting steam to the turbιne(90) or generator(6) and returning back luquid gas to the boιlers(75) respectivelly. 25. A fuel(gasolιne or diesel or kerosene) motor propulsion unιt(151) for an object(2) as an aιrcraft(4) or a craft(3) or a vehιcle(31 ) or a generator(6) or a machιne(32) or a pump(152) or a compressor 153) comprising a centrifugal turbιne(154) having a plurality of radially located aerodinamically shaped blades(155) each of which fixedly mounted between sides of two ring plates(156,157), a stationary cylindrical housιng(158) of turbine having one or more openιngs(159) on the cylindrical side, a shaft(160) of turbine which is rotatable mounted on the housing (158), a dιsk(161) or cross-bars(162) or propeller) 163) which couples one ring plate(156) and the shaft(160), a gap(164) which is located between the holes of ring plates(165) and inner edges of blades(155), an internal combustion chamber(166) comprising a space which is located in the gap(164) of turbine or between inner edges of blades(155) and holes of ring plates(165), a compression unιt(167), a fuel pump(168) and a fuel tube(169) for supplying of fuel to the chamber(166), characterized in that the internal combustion chamber(166) is located in the gap(164) of turbine, wherein the compression unιt(167) continously compress a fuel/air mixture in the internal combustion chamber(166), wherein the inflowing openιng(170) of compression unit is wider then the outflowing openιng(s) of the housingO 59), characterized in that the fuel/air mixture continiously exploding in the internal chamber(166), characterized in that the expanding gas from the chamber(166) attack blades(155) of turbine producing a high pressure on the peripheral side of each blade(155) to rotate the turbιne(154), characterized in that the centrifugal turbιne(154) drives the shaft(160) and the compression unιt(167) 6 A fuel motor propulsion unιt(151 ) according to claim 25, wherein the centrifugal turbιne(154) having a conical shape comprising an aιr-fan(171 ) of compression unit which is fixedly mounted to the wide hole of ring plate(172), a tubular shaft(173) which is fixedly mounted to the narrow hole of ring plate(174) and rotatable mounted to the conical shaped housιng(175), a shaft(160) which is fixedly mounted to the tubular shaft(173) and the fan(171 ), an internal combustion chamber(177) which comprising a gap(178) between the fan(171) and inner edges of blades(179) of turbine and a hole of tubular shaft(180), wherein the fuel is inserted through the hole of tubular shaft(180), characterized in that in the start when rotational speed of the turbιne(154) is low the expanding gas attack on all blades(179) of turbine mostly rotating the part of turbιne(154) with the wide opening to produce a high torque, characterized in that when the turbιne(154) increases in rotational speed, the fan(171 ) produces a high stream of air, which moves compression of fuel mixture and explosion respectively closer to the narrow part of turbine! 154) to increase rotational speed of the turbιne(154), characterized in that the centrifugal turbιne(154) having concav shape 27 A fuel motor propulsion unιt(151 ) according to claim 25, wherein the centrifugal turbιne(154) having a conical shape comprising an aιr-fan(171 ) of compression unit which is fixedly mounted to the wide hole of ring plate(172), a propeller (163) which is fixedly mounted to the narrow hole of ring plate(174), a tubular shaft( 173) which is coupled to the propellerf 163) and rotatable coupled to the housιng(175), a shaft(176) which is fixedly mounted to the tubular shaft(173) and to the fan(171) and rotatable coupled to the housing) 175), an internal combustion charπber(177) which comprising a gap(178) between the fan( 171 ) and inner edges of blades of turbιne(179) and the blades of propeller(181 ) and a hole of tubular shaft( 180), wherein the fuel is inserted through the tubular shaft(173), wherein the blades of fan (182) inflow air in the chamber(177) while the blades of propeller(181 ) outflow gas from the chamber(177), characterized in that in the start when rotational speed of the turbine (154) is low the expanding gas attack on all blades of turbine (179) mostly rotating the part of turbine with the wide opening to produce a high torque, characterized in that when the turbιne(154) increases in rotational speed, the fan(171 ) produces a high stream of air, which moves compression of fuel mixture and explosion respectively closer to the narrow part of turbιne(154) to increase in rotational speed and to decrease in torque, characterized in that the centrifugal turbιne(154) and the propeller(163) drive the shaft(176) and the fan(171) of compression unit.

28. A fuel motor propulsion unιt(151 ) according to claim 25, wherein the centrifugal turbιne(154) comprising two compression unιts(167) each of which having an aιr-fan(171 ) which is mounted in the hole of ring plate(165) of the turbιne(154), a tubular shaft(173) which is fixedly mounted to one fan(171 ) and rotatable mounted to the cylindrical housιng(175), a shaft(176) which is fixedly mounted to another fan(171 ) and rotatable mounted to the housιng(175), an internal combustion chambβr(166) which comprising a gap(164) between both fans(171) and inner edges of blades of turbιne(155) and a hole of tubular shaft(180), wherein the fuel is inserted through hole of the tubular shaft(180), wherein both fans(171) are of the same diameter, wherein the turbιne(154) having cylindrical shape, wherein the blades of one fan(182) are orientated in the opposite direction from the blades of another fan(182), characterized in that both fans(171 ) intflow air in the turbιne(154) to compress a fuel/air mixture during rotation of the shaft(176), characterized in that when the turbιne(154) increases in rotational speed the fans(171 ) produce a high stream of air which moves compression of fuel mixture and explosion closer to the central part of turbιne(154) to increase in rotational speed, characterized in that the centrifugal turbιne(154) drives the shaft(176) and the fans(171 ) of compression unit

29 A fuel motor propulsion unιt(151 ) according to claim 25, wherein the centrifugal turbιne(154) comprising two or more cylindrical layers(183) each of which consisting of two ring plates (156, 157) and a plurality of blades(155) which are fixedly mounted between sides of two ring plates(156,157), a remote control cylιnder(184) which reciprocating in holes of the ring plates(165), an aιr-fan(171 ) of compression unit which is fixedly mounted to the shaft(160) outside from the cylindrical housιng(158), a dιsk(161 ) or another fan(171) of compression unit which is fixedly mounted in the last hole of ring plate(165) and on the shaft(160), a flexible hose(185) which is coupled to the control cylιnder(184) far from the housιng(158), a tube(s)(186) which is mounted in the wall of control cylιnder(184) to deliver fuel to the internal combustion chambers(166), a sparking arc or plug(187) which is fixedly mounted to the end of control cylιnder(184), wherein the control cylιnder(184) slides along inner side of a squirrel cage(188) which is mounted on the flat side of the housing openιng(189), wherein the control cylιnder(184) all the time surrounding the fan(171), characterized in that the control cylιnder(184) is movable relative to the fan(171 ) and the ring plates of tubιne(156,157) and inner edges of blades(155), characterized in that air and fuel are delivered through the control cylιnder(184) and the fan(171 ) and air through another opening on flat side of the housιng(190) if any, characterized in that the control cylιnder(184) increases or decreases a number of internal combustion chambβrs(166) which receive a fuel/air mixture during operation, characterized in that the control cylιnder(184) couples stream of exploded gas with layers of the turbιne(183) increasing or decreasing outflow of gas from the layers of turbιne(183) and from opening of the housιng(159), characterized in that the control cylιnder(184) determines speed and output rotational rate of the shaft(160) 30 A fuel motor propulsion unιt(151 ) according to claim 25 and claim 29, characterized in that the layers(183) of centrifugal turbine are of different diameters and different thicknesses, characterized in that each internal combustion chamber comprising a gap(164) between inner edges of blades(155) and the ring plates(156,157) partly and the opening of control cylιnder(184) and a dιsk(161) or a fan(171 ) which is mounted in the last hole of ring plate(165), characterized in that the layers(183) with the larger diameter and narrow thickness having a high torque and that the layers(183) with the smaller diameter and wide thickness having a high speed

31 A fuel motor propulsion unιt(151 ) according to claim 25 and claim 29, characterized in that the layers(183) of the centrifugal turbine are of the same diameter and of the same thickness, characterized in that the control cylιnder(184) increases or decreases a number of narrow internal combustion chambers(166) which receive the fuel mixture

32 A fuel motor propulsion unιt(151 ) according to any one of claims 25, 29,30 and 32, wherein the control cylιnder(184) comprising a dιsk(191 ) and a cage(192), wherein the cage(192) couples the control cylιnder(184) and the disk (191 ), wherein length of the cage corresponding to length of one layer(183) of the turbine, characterized in that the control cylιnder(184) delivers a fuel mixture to one internal combustion chamber(166) only at the time

33 A fuel motor propulsion unιt(151 ) according to claim 25, wherein the centrifugal turbιne(154) comprising two or more cylindrical layers(193) aligning in the same level each of which having different diameters each of which consisting of two ring plates(156,157) and a plurality of blades(155) which are fixedly mounted between sides of two ring plates (156, 157), a round gap(194) which is located between each two layers(193), one or two remote control ring plates(195) each movable disposed in a round hole(196) on the flat side of the cylindncal housing (158) closing or opening the round gap (194), two compression units (167) each of which having an aιr-fan(171) which is mounted in the hole of ring plate(165) of the centrifugal turbιne(154), a tubular shaft(173) which is fixedly mounted to one fan(171 ) and rotatable mounted to the cylindrical housιng(158), a shaft(176) which is fixedly mounted to another fan(171) and rotatable mounted to the housιng(158), an internal combustion chamber(166) which comprising a gap(164) between both fans(171 ) and inner edges of turbine blades (155) and a hole of tubular shaft(180), wherein the fuel is inserted through the tubular shaft(173), wherein both fans(171) are of the same diameter, wherein the turbιne(154) having cylindrical shape, wherein the blades of one fan(182) are orientated in the opposite direction from the blades(182) of another fan(171), characterized in that both fans(171) intflow air in the turbine gap(164) to compress a fuel/air mixture during rotation of the shaft(176), characterized in that the remote control ring plates(195) opening or closing the round gaps(194) increase and decrease a number of layers(193) which are in operation in order to increase or decrease a torque and speed of the turbine.

34 A fuel motor propulsion unιt(151 ) according to claim 25, wherein the centrifugal turbιne(154) comprising two or more cylindrical layers(183) each of which consisting of two ring plates(156,157) and a plurality of blades(155) which are fixedly mounted between sides of two ring plates (156,157), a compression unιt(167) consisting of a centrifugal multi-layered pamp(197) which is fixedly mounted to the shaft(160) inside the gap(164) of the multi-layered turbine) 198), a remote control cylιnder(184) which reciprocating in a gap(199) between the compression unιt(167) and the multi- layered turbιne(198), a dιsk(161 ) or another fan(171) of compression unit which is fixedly mounted inside of hole of the ring plate(165) of the multi-layered turbιne(198), a flexible fuel hose(185) which is coupled to the control cylιnder(184) far from the housιng(158), a tube(s)(186) which is mounted in wall of the control cylinder to deliver fuel to the internal combustion chambers (166), a sparking arc or plug(187) which is fixedly mounted to the end of control cylιnder(184), wherein the last ring plate of compression unιt( 167) is fixedly mounted to the dιsk(161) or to another fan(171) of the multi-layered turbιne(198), wherein the control cylιnder(184) partly surrounding the compression unιt(167), wherein the control cylιnder(184) is movable in the gap(199) between the compression unιt(167) and the multi-iayerd turbιne(198) relative to outer edges of the blades(200) of the compression unιt(167) and inner edges of the blades(155) of the multi-layered tubιne(198), wherein the control cylιnder(184) slides along the inner side of a squirrel cage(188) which is mounted on flat side of the housing openιng(189), characterized in that the internal combustion chamber(166) comprising a round gap(199) between the compression unιt(167) and the multi-layerd turbιne(198) and the control cylιπder(184) and the dιsk(161 ) or another fan(171 ), characterized in that air and fuel is delivered to the chambers(166) through the control cylιnder(184) and another fan(171) if any, characteπzed in that the control cylιnder(184) increases or decreases a number of layers of the turbine and the pump simultaneously and internal combustion chambers(166) which receive a fuel/air mixture for operation, characterized in that the compression unιt(167) inflows and compresses air in the combustion chambers(166)

05 35 A fuel motor propulsion unιt(151) according to claim 25 and claim 34, wherein the compression unιt(167) is outside from the multi-layered turbιne(198), wherein the multi-layered turbine pump(197) of the compression unιt(167) comprising a control cylιnder(201 ) which is located in an inner gap (202) of the pump(197), wherein the pump turbιne(203) is located in a pump housιπg(204), wherein air inflows in the pump gap(202) through the hole of pump control cylιnder(205) and through 0 a hole of pump(206) disposed on the flat side of housιng(204), wherein a coupling cage(207) couples the control cylinder of pump(201 ) with the control cylinder of mult-layered turbιne(184), wherein the outside opening of the control cylinder of multi-layerd turbιne(184) and an opening (208) on the cylindrical side of pump housιng(204) are coupled with a flexibile coupling hose(209), characterized in that the control cylinders of the turbine and the pump(184,201 ) simultaneously 5 increase or decrease a number of layers of the turbine and the pamp (183,210) keeping control on inflowing air in the internal combustion chambers(166)

36 A fuel(gasolιne or kerosme or diesel) motor propulsion unιt(21 1 ) for an object(2) as a craft(3) or an aιrcraft(4) or a vehιcle(31) or a machιne(32) or a compressor(153) or a pump(152) or a generator(6) comprising a centrifugal turbιne(212) having two or more layers(213) each of which 0 consists of a plurality of radially located aerodinamically shaped blades(21 ) each of which fixedly mounted between sides of two ring plates(215,216), two extended tubes(217,218) each of which fixedly mounted to the hole of ring plate of turbιne(219), two fans(220,221 ) each of which fixedly mounted in the hole of extented tube(222), two tubular shafts of turbιne(223,224) each of which fixedly mounted to the fan(220,221), a stationary cylindrical housing of turbιne(225) having one 5 openmg(226) located on the cylindrical side and two extented cylιnders(227,228) which are fixedly mounted to the flat sides of housing each one for one extented tube(217,218), a gap(229,230) which is located in the extended tubes(217.218) between the fans(220,221) and inner edges of blades(214), a pιston(231) which alternating from one to other extended tube(217,218) through the said gap(229,230), two internal combustion chambers(232,233) each comprising a space which is located in the gap(229,230) of extended tube between the fan(220,221) and the pιston(231), two compression unιts(234,235) each of which consisting of said fan(220,221 ), two fuel tubes(236,237) each of which coupled to the tubular shaft(223,224) for delivering of fuel, wherein the internal

05 combustion chambβrs(232,233) are located in the holes of turbine extented tubes(222), wherein the turbιne(212) drives the fans of compression unιt(220,221 ), wherein the pιston(231 ) reciprocating from one to another chamber(232,233) when is pushed by exploded gas, characterized in that the pιston(231 ) operates as a part of compression unιt(234,235) improving the compression particularly in the starting of unιt(211 )

10 37 A fuel motor propulsion unιt(238) for a reciprocating compressor(239) or a reciprocating pump(240) or a reciprocating generator(241) or a craft(242) comprising two reciprocating open-top cylιnders(243,244) which are coupled with bottom(245,246) to a coupling arm of cylιners(247), two pistons (248,249) each of which having a bent arm(250,251 ) which is coupled to a coupling rod(252,253) of a coupling arm of pιston(254), two internal combustion chambers(255,256) each

15 located in the cylιnder(243,244), two flexible hoses (257 ,258) for exhausted gas each of which coupled with one cylιnder(243,244), two flexible hoses(259,260) for fuel each of which coupled to one cylιnder(243,244), two sparking plugs(261 262) each for one cylιnder(243,244), wherein the pιston(248,249) reciprocates in the cylιnder(243,244), wherein each coupling rod(252,253) is mounted to coupling arm of the pιstons(254) at an angle of 90 degrees, wherein coupling arms of the 0 cylιnder(247) and the pιston(254) are pivotaly coupled to a supporting frame(263), wherein the piston (248,249) and the cylinders (243,244) are located on the shortest part of the coupling arms(247,254) while a water fin of the craft(242) or a permanent magnet of the generator(242) or a piston of compressor(239) or a piston of pump(240) are located on the end of the longest part of coupling arm(247,254), wherein the cylinders (243,244) and the pistons (248, 249) are slightly bent 5 depending on a distance from a axιs(264) of coupling arms, wherein the coupling arms (247,254) are designed to oscillate about a vertical or horizontal axιs(264), characterized in that during each explosion in one of chamber(255,256) the piston (248,249) moves away on one side while the cylιnder(243,244) moves on another side compressing a fuel mixture in another chamber(255;256) and vice versa, characterized in that the cylιnders(243,244) and the pistons (248 ,249) alternating drives the coupling arm(247,254) to compress gas or to pump fluid or to propel the craft(249), characterized in that a reciprocating piston and a reciprocating cylinder of pump(240) or compressor(239) may push a large volume of gas or fluid for each alternation due to the long

05 coupling arm(247,254), characterized in that a torque of the coupling arm(247,254) is increased due to movement of the cylιnders(243,244)

38 A fuel motor propulsion unιt(265) for an object(2) as an aιrcraft(4) or a craft(3) or a vehιcle(31) or a machιne(32) or a generator(6) or a compressor(153) or a pump(152) comprising one or more reciprocating cylιnders(266) each having a middle dιsk(267) which divides a hole of cylιnder(268) in

10 two chambers(269,270) first one for a reciprocating pιston(271) and second one for a stationary pιston(272), a crankshaft(273) having one or more pairs of cranks(274) each of which having two cranks(275), one or more coupling rods(276) each of which couples the reciprocating cylιnder(266) and the crank(275), one or more coupling rods(277) each of which couples the pιston(271 ) and the crank(275), wherein the pιston(271 ) reciprocating inside the first chamber(269), characterized in that

15 the stationary direction pιston(272) directs linear movement of the cylιnder(266) through the second chamber(270), characterized in that the pιston(271 ) reciprocates relative to the cylιnder(266) as the cylιnder(266) reciprocates relative to the pιston(271), characterized in that the cylιnder(266) reciprocates relative to the stationary direction piston (272), characterized in that the reciprocating cylιnder(266) and the reciprocating piston (272) act as torque on the crankshaft(273)

20 39 A fuel motor propulsion unιt(265) as a pump(152) or a compressor(153) according to claim 25 or claim 38. comprising one reciprocating cylιnder(266) and one pιston(271 ) which are coupled to cranks(275) with coupling rods(276,277), an inflow and an outflow valve and tube(278,279) for first chamber of cylιnder(269), an inflow and an outflow valve and tube(280,281) for second chamber of cylιnder(270), two compression chambers(282,283) which are located in first and second chamber

25 of cylιπder(269,270), characterized in that when the shaft(284) is driven by the fuel motor propulsion unιt(265) the cranks of crankshaft(275) simultaneously move the pιston(271 ) and the cylιnder(268) to pump fluid or to compress gas 40 A fuel motor propulsion unιt(265) according to claim 38, comprising one reciprocating cylιnder(266) and one reciprocating pιston(271 ) which are coupled to cranks of the crankshaft(275) with coupling rods (276,277), an internal combustion and compression chamber(285) which is located in the first chamber of cylιnder(269), a flexible hose(286) for exhausted gas which is coupled to the internal combustion chamber(285), a fuel and an air tube(287 288) which are mounted in the stationary piston (272), a secondary compression chamber(289) which is located in the second chamber of cylιnder{270), a valve(290) which is mounted in the middle disk of cylιnder(267) to couple the internal combustion chamber(285) and the secondary compression chamber(289), a sparking plug(291 ) which is located in the combustion chamber(285) at the dιsk(267) characterized in that when the cylιner(266) moving away from the stationary pιston(272) simultaneously producing a low pressure in the second chamber(270) and compressing fuel mixture in first chamber(269) together with the reciprocating pιston(271 ) so a high pressure therein closes the valve and fuel mixture may inflow in the second chamber of cylinder from tubes of fuel and air which are located in the stationary piston, characterized in that when an explosion of fuel mixture moves the cylinder toward the stationary piston an increased pressure in second chamber opens the valve so that air mixture may inflow in the combustion or first chamber pushing exhausted gas out, characterized in that as the cylinder reciprocating a part of kinetical energy from the exploded gas is extracted instead to be absorbed by the stationary body of cylinder if any 41 A fuel motor propulsion unιt(265) according to claim 38 or claim 40. comprising two or more reciprocating cylιnders(266) with pιstons(271) and two or more pairs of crank(274), characterized in that each cylιnder(266) and each pair of crank(274) are different in the power and in the radius respectively from other cylιnders(266) and cranks(274), characterized in that the cylιnder(266) and the pιston(271 ) which are coupled to pair of crank(274) having larger radius produce a high torque while the cylιnder(266) and the pιston(271 ) which are coupled to pair of crank(274) having shorter radius produce a high speed, characterized in that speed of the shaft is in relation to the size of cylinder and crank of crankshaft so to change speed require to changed the cylinder 42. A fuel motor propulsion unιt(265) according to claim 38 or claim 40, comprising one cylinder or more cylinders (292) which are different in length each of which consisting of a tubular pιston(293) extensible from the cylιnder(292) and a pιston(294) extensible from the tubular pιston(293), two crankshaft(295,296) each having one crank or more cranks(297) which are different in size of length; a coupling rods(298) which couples a crank(297) of first crankshaft(295) with a crank(297) of second crankshaft(296) synchronizing rotation of both crankshafts (295,296) and shafs(299), wherein the cylιnder(292) is rotatable coupled to the crank(297) of first crankshaft(295), wherein the pιston(294) is rotatable coupled to the craπk(297) of second crankshaft(296), wherein the tubular pιston(293) is longitudmaly coupled to the cylιnder(292) on one side and to the piston (293) on another side, wherein an internal combustion chamber(300) is located in the cylιnder(292), characterized in that during each explosion of a fuel mixture in the chamber(300) the tubular pιston(293) and the piston (294) are pushed on one side while the cylιnder(292) is pushed on another side both rotating first and second crankshaft(295,296) simultaneously in the same direction of rotation, characterized in that each explosion is occured when cranks(297) of first and second crankshaft(295;296) have the shortest distance therebetween or when the pιston(294) and the tubular pιston(293) are not extended from the cylιnder(292), characterized in that a compression of a fuel mixture starts in the cylιnder(292) when the crank(297) of first crankshaft(295) is far away from the crank(297) of second crankshaft(296) or when the pιston(294) is extended from the tubular pιston(293) and the tubular piston (293) is extended from the cylιnder(292), characterized in that speed of the shaft(299) is in relation with size of cylιnder(292) and size of crank(297) which are in used so to change speed require to change the cylinder 43. A fuel motor propulsion unιt(265) according to claim 38, comprising two rotatable crankshafts(295;296) each with one or more crank(297), one or more unit each of which with two cylιnders(292) which are rotatable coupled to the crank(297) of first crankshaft(295) and to the crank(297) of second crankshaft{296), a reciprocating pιston(301 ) for each unit which is coupled partly to the cylιnder(292) of first crankshaft(295) and partly to the cylιnder(292) of second crankshaft(296), a coupling rod(298) which couples a crank of first crankshaft(295) with a crank of second crankshaft(296) synchronizing rotation of both crankshafts(295,296) and shafts(299), wherein the internal combustion chambers(300) are located in the cylιnders(292), characterized in that during each explosion of a fuel mixture in each chamber(300) the cylιnders(292) are pushed away from the pιston(301) each one on the opposite side both rotating first and second crankshaft(295,296) simultaneously in the same direction of rotation, characterized in that each explosion is occured when cranks of first and second crankshaft(295,296) have the shortest distance therebetween or when the pιston(301) is not extended from the cylιnders(292), characteπzed in that a compression of a fuel mixture starts when the crank of first crankshaft(295) is far away from the crank of second crankshaft(296) or when the pιston(301) is extended from the cy nders(292)

44 A fuel motor propulsion unιt(151 21 1 ) according to claim 25 or claim 36 wherein the remote contol cylιnder(184) of the centrifugal turbιne(154,212) comprising a connection to a water pump(302) and a means(303) for dispersing water drops into the internal combution chambers(166,233 234), characterized in that the steam which is produced from the water by hot gas increases power of the turbιne(154,212) and reduces a direct heating and pollution of the air

45 A fuel motor propulsion unιt(265) according to claim 38 for a craft{3) or an aιrcraft(4), wherein the crankshaft(273) having two cranks(275) connected to coupling rods(276) or arm(277) each of which couples the reciprocating cylιnder(266) and the reciprocating pιston(271 ) respectively, wherein each crank(275) comprising a blade of propeller(304) which middle point is fixedly mounted to the coupling rod(276) or arm(277) at an angle of 90 degrees at the point where the coupling rod(276) or arm (277) is rotatable coupled to the cran (275), wherein the shaft of crankshaft(284) rotates around a horizontal axιs(305)

46 A fuel motor propulsion unιt(306) for a craft(3) or an aιrcraft(4), comprising a crankshaft(307) having two cranks(308), two stationary internal combustion cylιnders(309,310) each of which coupled to a reciprocating pιston(31 1 ,312), two coupling rods(313,314) each of which couples the pιston(311 ,312) with the crank(308) of crankshaft(307), two blades of propeller(315,316) which middle point is fixedly mounted to the coupling rod(313,314) at an angle of 90 degrees at the point where the coupling rod(313,314) is rotatable coupled to the crank(308), wherein the shaft(317) of crankshaft rotates around a horizontal axιs(318) 47 A fuel motor propulsion unιt(319) for an object(2) as an aιrcraft(4) or a craft(3) or a vehιcle(31) or a machιne(32) or a generator(6) or a compressor(153) or a pump(152) comprising two pairs of stationary cylinders (320) each pair having the length different from other pair, two pairs of cranks(321) of crankshaft(322) each pair having the radius different from other pair, two pairs of pιstons(323) each pair having the length of coupling rod(324) different from other pair, wherein each pair of stationary cylιnder(320) having two cylιnders(325) each of which with a reciprocating pιston(326) therein, wherein each pιston(326) is coupled to one crank of crankshaft (327) with the coupling rod(324), wherein each internal combustion or compression chamber(328) is located in the hole of cylιnder(325), characterized in that a rotational speed of the shaft is in relation to the pair of cylinder which are in operation.

48 A fuel motor propulsion unιt(319) according to claim 47, wherein each pair of crank(321) comprising extensible tubes(330) each of which coupled with one of two arms of the crank(331) which is perpendiculary mounted to the shaft(329), characterized in that when both pair of cylinders (320) increase or decrease a distance from the crankshaft(322) the extensible tubes(330) increase or decrease lenght simultaneously changing a torque and a speed of the shaft(329)

49. A propulsion unιt(151 ,21 1 ,265,319) according to any one of claim 25, 36, 38 and 47, wherein the shaft(160,223,284,329) drives a centrifugal turbιne(332) or a crankshaft turbιne(333) to propel a craft(3) through the water

50. A fuel motor propulsion unιt(151 ,211 ,265,319) according to claim 49, wherein the centrifugal pump(332) comprising two or more cylindrical layers(334) of turbine each of which consisting of ring plates(335) and a plurality of blades(336) which are fixedly mounted between sides of two ring plates(335), a cylindrical housing (337) of turbine having two or more openιngs(338) located on the cylindrical side; a remote control cylιnder(339) which is located between inner edges of blades(336) and holes of ring plates(340), a shaft(341 ) of turbine which is rotatable located in the housιng(337), a dιsk(342) or cross-bars(343) or propeller(344) which couples the last ring plate(335) of turbine and the shaft(341 ), wherein ail holes of ring plates(340) having the same diameter, wherein the diameter and the thickness of layers(334) are equal or different one from another, wherein the water inflows in the chambers(345) and the layers(334) of turbine through the hole of control cylιnder(346) and through the cross-bars (343) or the propeler(344) if any, characterized in that during rotation of the turbιne(332) the remote control cylιnder(339) may increase or decrease a number of the chambers(345) and layers(334) of turbine in which water inflows so outflowing trust and speed of the object are increased or decreased accordingly

51 A fuel motor propulsion unιt(151 , 211 ,265,319) according to any one of claims 25, 36, 38 and 47, wherein the shaft(160,223,284,329) drives a propeller(347) or a crankshaft turbιne(333) to propel an aιrcraft(4) through the air

05 52. A fuel motor propulsion unιt(151 ,21 1 ,265,319) according to claim 51 , wherein the shaft(160,223,224,284,329) rotates around a vertical axιs(348)

53 A fuel motor propulsion unιt(151 ,211 ,265,319) according to claim 49 or claim 51 , wherein the crankshaft turbιne(333) comprising a rotor(349) which consists of a crankshaft(350) with one or two cranks(351) each of which mounted on the vertical shaft(352), one or two blades(353) each

10 rotatable coupled to a vertical arm of crank(354), a direction crank(355) which is rotatable mounted to the shaft(352), one or two coupling arms(356) each couples the blade(353) and the direction crank(355), a remote control handle(357) which is fixely mounted to the direction crank(355) at an angle of 90 degrees, one or two vertical axιs(358) each fixedly mounted to the coupling arm(356), one or two lιnks(359) each pivotaly coupled to the vertical axιs(358) of coupling arm(356) and to a

15 horizontal arm(360) of the direction crank(355), wherein the middle part of each blade(353) is fixedly mounted to the coupling arm(356) at an angle of 90 degrees, wherein the coupling arm(356) is longer then the lenght of crank(351 ). characterized in that during rotation of the shaft(352) the coupling arm(356) slip with the lιnk(359) along the arm of direction crank(360) alternately changing the angular deflection of the blade(353) according to the positons of blade(353) on an orbιt(361 ) of 0 rotor pushing the fluid on one side and the object(2) on another side

54. A fuel motor propulsion unιt(151 ,211 ,265,306,319) according to any of claims 45, 46 and 51 , wherein the blades(362) of the aιrcraft(4) having a convex upper part(363) while the down part(364) is flat.

55 A fuel motor propulsion unιt(151 ,211 ,265,319) according to claim 49, wherein the blades(365) of 5 the craft(3) having double convex (366) or a flat shape(367)

56 An electric propulsion unιt(368) for lifting an aιrcraft(4) comprising two ballast insulated tanks or balloons(369) which are filled with a light gas, preferably with freon, each of which fixedly mounted to a wιng(370) of the aιrplane(371 ) , characterized in that while the aιrplane(371 ) is on the ground a compressor(372) which is located on the ground converts a liquid freon from a prior flight in a gas which inflows in the balloons(369) so the aιrplane(371 ) becomes lighter ready for taking off, characterized in that the aιrplane(371 ) or the helicopter geting an altitude without using own engιne(373) reducing need for a lot of fuel for taking off and reducing need for a strong engine, characterized in that during a flight the gas gradualy becomes liquid due to a low- temperature from outside geting on weight and the aιrplane(371) gradualy losing the altitude so that the engιne(373) of airplane must compensate changes in the altitude if needed

57 An electric propulsion unιt(374) for lifting an aιrcraft(4) comprising a taking off platform(375) located on a frame(376) which is coupled with two ballast tanks or two captive rigid balloons (377), an elevator(378) which is driven by an electric motor(379) to lift an aιrplane(371 ) or helicopter from the ground to the taking off platform (375), characterized in that the aιrpiane(371) or the helicopter geting an altitude without using own engιne(373) reducing need for a lot of fuel for taking off and reducing need for a strong engine (373)

58 A propulsion unιt(1 ,67,124,374) according to any one of claims 2, 12, 22, 56 and 57, wherein each of two captive rigid ballast balloons (24,377) which are coupled to the frame(23,376) consists of an aluminium tank or a pneumatic cylinder or porous cells of aluminium having inside a light gas (helium or freon or so) , wherein the pneumatic cylinder or balloon (24,377) is preferably disposed inside of an aluminium squirrel cage(380) or closed frame, wherein each balloon(24,377) or tank comprising a direction fιn(381 ) which is fixedly mounted to the balloon(24,377) or tank, wherein each balloon(24,377) or tank having a long cylindrical shape, wherein the frame (23,376) could be coupled with the ground with a few small link balloons(382) each floating at different altitude, wherein the rope(25) which ends are coupled to the ground at a certain distance therebetween passing over two spools(383) each of which coupled on the opposite side of the frame(23,376) of balloons to achieve a horizontal position of the frame(23,376), characterized in that the frame(23,376) of balloons which floating and following direction of the wind is pivotaly coupled to the rope(s)(25) 59. A propulsion unιt(368) according to claim 56, wherein the aιrcraft(4) comprising a compressor(384) and a heat exchanger(385), wherein the compressor(384) which is coupled to an electric motor(30) geting electricity from a battery or from a generator(6) coupled to the engιne(373) of aιrcraft(4), characterized in that during the flight the compressor(384) on the aιrplane(371 ) keeps freon as a gas controlmg the altitude, characterized in that for landing the gas from the balloons(369) gradualy inflows in the heat exchanger(385) wherein due to low-temperature from outside becomes gradualy liquid geting on weight so that the aιrplane(371) becomes gradualy havier losing an altitude.

05 60 A fuel motor propulsion unιt(151 ,) according to any of claims 28, 31 , 34 and 35, wherein the internal combustion chamber(166) or the housing of tubιne(158) consisting of convex upper part and bottom flat part to achieve an aerodinamical configuration, characterized in that the aerodynamical housιng(386) is use as a wing or a part of wing of the aιrplane(371 ), characterized in that the housing (386) is partly mobile to change an angle relative to the fuselage(387) to achieve a

10 perpendicular angle of the aιrplane(371) during taking off or landing 61 A fuel motor propulsion unιt(151 , 211 ,265,319,} according to any of claims 25, 36, 38, 47 and 54, wherein the shaft(160,223,224,284,329) drives a propeller(388) to lift the aιrcraft(4) up, wherein the shaft(160,223,224,284,329) rotates around a vertical axis, wherein the propeller(388) has two or more radially disposed blades(389) each of which having an aerodynamical configuration, wherein

15 the blades of propeller(389) having a convex upper part (390) while the bottom part(391 ) is flat, wherein the bottom flat sιde(391 ) of each blade(389) is disposed downward while the convex upper sιde(390) is disposed upward, wherein the propeller(388) lifts the aιrcraft(4) upward due to a difference between the air-pressures which are produced by the bottom(391) and the upper side (390) of each blade(389)

20 62 A fuel motor propulsion unιt(151 ,211 ,265,319) according to any of claims 25, 36, 38, 46 abd 47, wherein a rotorless generator(69) is coupled to the tube of exhausted gas(392), wherein the generator(69) is propelled by the outflowing exhausted gas from the fuel motor 63. An electric motor propulsion unιt(393) for a pump(394) of fluιd(steam or gas or air or water) comprising rotorless motor(395)

2564 A propulsion unιt(393) according to claim 63, wherein the fluid pump(394) is used for purification of the water from an ocean or sea.

65. A fuel motor propulsion unιt(265) according to claim 38, wherein a rotorless generator(69) is coupled to an internal combustion chamber of the reciprocating cylιnder(269)

66. A wind motor propulsion unιt(396) for a generator(6), comprising a rotorless generator(69) which is located at a high pole(63) or on a frame(23) of two captive rigid balloons(24).

67. A propulsion unιt(67,89;95,124,393) according to any of claims 12, 16, 18, 19, 22, 63, 64 and 65, wherein the rotorless generator(69) comprising, one or more conductive chambers(397) conducting a fluid and an electric current; one or more broken off or interrupted armature(398) or field wιndιngs(399), two plates(400) with a plurality of pιns(401 ), one or more field wιndιngs(402) or a pair of strong permanent magnets(403); one or more open-pole frames(404) each of which having the field wιndιngs(402) or poles(405) of permanent magnet(403), wherein the plates(400) are incorporated in the walls(406) of chamber each one on the opposite side, wherein the poles(405) of frame are incorporated in the walls(406) of another two free sides of the chamber(397) each one on the opposite side, wherein each pιn(401 ) is electncaly insulated from other pιns(401), wherein each wιre(407) of broken off wιndιng(398) is connected with first end(408) to first pιn(410) which is located on first plate(412) and with second end(409) to second pιn(411 ) on second plate(413), characterized in that a location of second pιn(41 1) on second plate(423) is one step apart in comparison with location of first pιn(410) on first plate(412), characterized in that each pιn(401 ) of first plate(412) is accross each pιn(401) of second plate(413) at the shortest distance therebetween, characterized in that each pιn(401) of first plate(412) is electncaly coupled to each pιn(401) of second plate(413) through fluid, characterized in that the ends of each wιre(407) of wιndιng(398) are connected through such pιns(401 ) to obtain the same function of wιndιng(398) as a conventional winding when a fluid in the conductive chamber(397) conducts electric current, characterized in that kinetical energy of each fregment of fluid stream passing through the chamber(397) intβreact with the strong magnetic field so such field moves electrons of fragment from pιns(401 ) of fπst plate(412) to pιns(401 ) of second plate(413) as through any other wire conducting generated electric curent through the fluid and the winding (398), characterized in that when electrons of electric current passing through the wιndιng(398) and the fluid a magnetic field which is produced in fragments of the fluid interact with the stationary magnetic field so such field moves fregments of the fluid through the chamber(397) acting as a motor or a pump.

68. A propulsion unιt(396) according to claim 67. characterized in that the rotorless generator(69) compπsing one chamber(397)

69 A propulsion unιt(393,396) according to any one of claims 62, 63, 65, 66 and 67, characterized in that the rotorless generator(69) comprising two chambers (397) having a broken off wιndιπg(398) which each wιre(407) is broken off in two pιeces(414,415), wherein ends(408,409) of first piece of 05 wιre(414) are connected to first plates(412) of first and second chamber(416,417) while ends of second piece of wιre(415) are connected to second plates(413) of first and second chamber(416,417), wherein a polarity of stationary magnetic field in first chamber(416) is designed to be opposite from the polarity of stationary magnetic field in second chamber(417) to achieve the same direction of current flow in the broken off wιndιng(398) 1070 A propulsion unιt(151 , 211 ,393,396) according to any of claims 25, 36, 62, 63, 65, 66 and 67 wherein the internal combustion chambers(151 ,232) and the conductive chambers(397) comprising a low-radiation harmless source to improve electrical coductivity of fluid.

71 A propulsion unιt(1 , 60,67,89,95,124, 151 ,21 1 ,265,319) according to any of claims 1 , 2, 1 1 , 12, 18, 19, 22, 25, 36, 38 and 47, wherein the shaft(8,61 ,119,160,223,329) drives a rotor of 15 generator (418) to generate an electric current of constant frequency output, wherein the generator(6) comprising, a main generator(419) which rotor(418) is driven by the shaft(420), a field wιndιng(421 ) of the rotor(418) of the main generator(419), a generator housιng(422), a stationary base(423) which supports the generator(6), a housιng(424) which is rotatable mounted on the shaft(420), a secondary electric motor(425) which stator(426) is located in the rotatable housιng(424) 0 while a rotor(427) of the motor is fixedly mounted to the shaft(420); a source of excitation current(428), a rotating transformer or a set of stationary brushes(429) coupled to a set of slip rings (430) or a set of commutator plates (431 ), wherein the stationary brushes (429) are located at the stationary base(423), wherein the slip rιngs(430) or commutator plates(431) are fixedly mounted on the shaft(420) or on a tubular extantιon(432) of rotatable housing, wherein the rotatable 5 housιng(424) is independently rotatable around the shaft(420), wherein the rotor(427) of motor rotates the stator(426) of motor and the housιng(424) as the housιng(424) is not fixedly mounted to the stationary base(423), wherein rotational speed of the shaft(420) varies due to a vaπble motive power source(wιnd, water or so) or due to variation in cemf or resistance from the consumers of electπc current, characterized in that the secondary motor(425)(AC or DC) is designed to rotate the housing around the shaft(420) at an electrical synchronous speed , characterized in that the motor(425) is designed to counter-rotate the housιng(420) relative to rotational direction of the shaft(420)

0572 A propulsion unιt(1 ,60,67,89.95.124,151 ,211 ,265,319) according to claim 71 , wherein the rotatable housιng(424) comprising one or more motors(425) and one or more excιter(433), wherein the stator(434) of exciter having poles(435) of permanent magnets (436) or wound field wιndιng(437), wherein the stator(426) of motor having poles of permanent magnets(436) or wound field wιndιng(437), wherein the rotor(438) of exciter having poles(439) wound with an armature

10 wιndιng(440), wherein the rotor(427) of motor having poles(441 ) of permanent magnets(436) or wound with a field wιndιng(437), wherein the rotors(438,427) of exciter and motor are fixedly mounted to the shaft(420), wherein the main generator(419) comprising one or more generators(419) each of which located in the same housιng(422), wherein each rotor(418) of the mam generator is wound with the field wmdιng(421 ), wherein each stator(442) of mam generator is wound with an

15 armature wιndιng(443), wherein each armature wιndιng(440) of the exciter rotor is electncaly coupled to one field wιndιng(421 ) of the rotor(418) of the main generator, characterized in that the secondary motor(425) maintains to rotate the housιng(424) relative to the shaft(420) at the synchronous speed during variation in rotational rate of the shaft(420) so that the stator of excιter(434) increases or decreases in speed relative to the stationary base(423) when the

20 shaft(420) is slow or increase in speed, characterized in that the stator of excιter(434) when rotating relative to the stationary base (423) rotates relative to the rotor of excιter(438) generating in the armature winding of exciter rotor(440) an additional positive or negative frequency to the frequency which is generated when the rotor of excιter(438) rotates relative to the stator of excιter(434) at rotational rate of the shaft (420) so that an output frequency will establish in the field winding of

25 generator rotor(421 ) a magnetic field which rotates directionally relative to rotational direction of the shaft(420) at a synchronous speed generating an output at desired frequency in the armature winding of generator stator(443) irrespectively from rotational speed of the shaft 73 A propulsion unιt(1 , 60,67 ,89,95,124, 151 ,211 ,265,319) according to claim 71 , wherein the rotatable housιng(424) comprising one or more motor(425) and a set of brushes(444) which are coupled to a set of slip rιngs(445) or commutator plates(446), wherein the stator(426) of motor having poles(447) of permanent magnets(436) or wound field wιndιng(437), wherein the motor rotor(427) having poles(441 ) of wound field wιndιng(437) or permanent magnets(436), wherein the set of slipmg πngs(445) or commutator plates(446) are fixedly mounted to the shaft(420), wherein the mam generator(419) comprising one or more generators (419) each of which located in the same housιng(422), wherein each rotor(418) of the main generator ts wound with a field wιndιng(421 ), wherein each stator(442) of mam generator is wound with an armature wιndιng(443), wherein the set of slip rings (445) or commutator plates (446) is electncaly coupled to one or more field wιndιngs(421 ) of the rotor(418) of the mam generator, characterized in that the stator of motor(426) maintains to rotate at the synchronous speed relative to the shaft(420) during variation in rotational speed of the shaft(420) so that the housing brushes(444) increase or decrease in speed relative to the stationary base(423) when the shaft(420) is slow or increase in speed, characterized in that the housing brushes(444) when rotating relative to the stationary base(423) rotate relative to the shaft(420) and slip πngs(445) or commutator plates(446) supplying a frequency to the commutator plates(446) or slip πngs(445) which rotate relative to housing brushes(444) at rotational rate of the shaft(420) so that such frequency will establish a magnetic field in the field wιndιng(421 ) of generator rotor which rotates directionally relative to rotational direction of the shaft(420) at the synchronous speed generating in the armature wιndιng(443) of generator stator an output at desired frequency irrespectively from rotational rate of the shaft(420) . 74. A propulsion unιt(1 , 60,67,89.95, 124, 151 ,211 ,265,319) according to claim 71 and claim 72, wherein the rotatable housιng(424) comprising one or more motors(425) and excιters(433), wherein the stationary housιng(422) of main generator comprising one or more generators(419), wherein each two or more units of motors(425) and excιters(433) and generators(419) are different in diameters and different in output powers, wherein each stator(426) of motor having poles(447) of permanent magnets(436), wherein each rotor(427) of motor having a field wιndιng(437), wherein each wιπdιng(437;440,421) of the motor rotors and the exciter rotors and the generator rotors is coupled to a centrifugal switch (448;449), characterized in that the first switches (448) or switches of larger units are designed to conduct an electric current in wιndιngs(437, 440,421 ) of rotors when rotational speed of the shaft(420) is low, characterized in that secondary swιtches(449) or switches of smaller units are designed to conduct an electric current in wιndιngs(437,440,421 ) of rotors when rotational rate of the shaft(420) is high, characterized in that when the prime mover(450) increases 05 rotational speed of the shaft(420) then the secondary swιtches(449) activates the rotor wιndιngs(437,440,421 ) of the small units, characterized in that when the shaft(420) increases in speed the exciter stators(434) of the small units decreases in speed relative to armature winding (440) of the rotor exciter so a relatively slight difference in the power and frequency will be taken through the motor(425) from a network(29), characterized in that when the prime mover(450) 10 decreases rotational speed of the shaft(420) then the first swιtches(448) activate the rotor wιndιngs(437,440.421 ) of the large units, characterized in that when the shaft(420) decreases in speed the exciter stators(434) increases in speed relative to armature wιndιngs(440) of the exciter rotor of the larger units so a relatively large difference in power and frequency will be taken through the motor(425) from a network (29) 15 75. A propulsion unιt(1 ,60,67.89,95,124,151 ,211 ,265,319) according to claim 71 and claim 73, wherein the rotatable housιng(424) comprising one or more motors(425) and exciters (433), wherein the stationary housιng(422) of main generator comprising one or more generators(419), wherein each two or more units of motors(425) and excιters(433) and generators(419) are different in diameters and different in output powers, wherein each stators(426) of motor having poles(447) of 20 permanent magnets(436), wherein each rotor(427) of motor having a field wιndιng(437), wherein each wιndιng(440,437,421) of the exciter rotors and the motor rotors and the generator rotors is coupled to a centrifugal switch (448, 449), characterized in that the first switches (448) or switches of larger units are designed to conduct an electric current in wιndιngs(440,437,421 ) when rotational speed of the shaft(420) is low, characterized in that the secondary switches (449) or switches of 25 smaller units are designed to conduct an electric current in wιndιngs(440,437,421 ) when rotational rate of the shaft{420) is high, characterized in that when the prime mover(450) increases rotational speed of the shaft(420) then the secondary swιtches(449) activate the wιndιngs(440,437,421 ) of rotor on the small units, characterized in that when the shaft(420) increases in speed the housing brushes(444) decreases in speed relative to the commutator plates(446) so a relatively slight difference in the power and frequency will be taken through the motor(425) from a network(29), characterized in that when the prime mover(450) decreases rotational speed of the shaft(420) then first swιtches(448) activate the rotor wιndιngs(440, 437,421 ) of the large units, characterized in that when the shaft(420) decreases in speed the housing brushes(444) increases in speed relative to the commutator plate(446) so a relatively large difference in the power and the frequency will be taken through the motor(425) from a network(29)

76 A propulsion unιt(60) according to claim 1 1 , wherein the shaft(61 ) drives rotors(451) of two or more generators(6) having different diameters and output powers wherein the stator(452) of each generator having poles(453) of permanent magnets(454), wherein the rotor(451 ) of each generator having poles(455) wound with armature wιndιngs(456), wherem all rotors(451 ) and stators(452) of generator having the same number of poles(453,455), wherein two or more secundary centrifugal swιtches(449) are mounted on the shaft(61), wherein each swιtch(449) electrically connects two ends of armature wιndιng(456) of the rotor when the shaft(61 ) achieves certain rotational speed, wherein a rotating transformer or a pair of slip πngs(457) which are mounted on the rotor(451 ) are coupled to a pair of stationary brushes(458), characterized in that a number of armature wιndιngs(456) of the rotors in which the current is generated is in relation to rotational speed of the shaft(420)

77 A propulsion unιt(60) according to claim 1 1 , wherein the shaft(61 ) drives rotor(451 ) of generators, wherein the stator(452) of generator having poles(453) of permanent magnets(454), wherein the rotor(451) of generator having two or more armature wιndιngs(456) each of which wound on a rotor pole(455), wherein two or more secundary centrifugal swιtches(449) are mounted on the shaft(61 ), wherein each swιtch(449) is designed to be activated at a certain speed, wherein each swιtch(449) electncaly connects two ends of each rotor armature wιndιng(456) when the staft(61 ) achieves certain rotational speed, wherein a rotating transformer or a pair of slip πngs(457) which are mounted on the rotor(451) are coupled to a pair of stationary brushes(458), characterized in that a number of armature wιndιngs(456) of rotor in which a current is generated is in a relation to rotational speed of the shaft(61) 78 A propulsιon unιt(1 ;60,67,89,95,124,151 ,211 ,265,319) according to any of claims 74, 75, 76 and 77, wherein the secondary swιtch(449) comprising a spπng(459) which one end is fixedly mounted to the shaft(460) while another end having an armature contact(462) which is connected to the armature wιndιng(461 ) of the rotor, wherein the sprιπg(459) and the armature contact(462)

05 reciprocating in an electncaly insulated tube(463), wherein the top of tube(463) having a stationary armature contact(464) which is connected to the another end of the armature wιndιng(461 ) of the rotor, characterized in that when rotational speed of the shaft(460) increases the centrifugal force increases lenght of the sprιng(459) connecting the said armature contacts(462,464) closing a circuit in the wιndιng(461 )

10 79 A propulsion unit (1 60,67,89,95,124,151 ,21 1 265,319) according to claim 74 and claim 75, wherein first swιtch(448) comprising a spring (459) which one end is fixedly mounted to the top of an electncaly insulated tube(463) while another end having an armature contact(462) which is connected to the armature wιndιng(461) of the rotor wherein the bottom of tube(463) is fixedly mounted to the shaft(460), wherein the sprιng(459) and the armature contact(462) reciprocating in

15 the insulated tube(463), wherein the bottom of tube(463) having a stationary armature contact(464) which is connected to the another end of the armature wιndmg(461) of the rotor, characterized in that when rotational speed of the shaft((460) increases the centπfugale force decreases lenght of the spπng(459) disconnecting the said armature contacts(462,464) 80 A propulsion unιt(1 , 60,67,89,95, 124,151,21 1 ,265,319) according to any of claims 1 , 2, 11 , 12,

20 18, 19, 22, 25, 36, 38 and 47, wherein the shaft(465) drives the crankshaft (466) of a reciprocating commutatorless generator(467), wherein the reciprocating generator(467) comprising a reciprocating permanent magnet(468) or a field winding wound(469) on a round core(470) which is coupled through a coupling arm(471) to one crank(472) of crankshaft and a reciprocating selenoid (473) which is coupled through a coupling arm(471 ) to another crank(472) of crankshaft,

25 wherein the permanent magnet(468) or the field wιndιng(469) slides inside the tube(474) of selenoid, wherein the tube(474) of selenoid slides along a stationary direction rod(475), characterized in that the selenoιd(473) moves relative to the permanent magnet(468) or the field wιndιng(469) , characterized in that the permanent magnet(468) or the field wιndιng(469) moves relative to the selenoid (473), characterized in that such alternation of the permanent magnet(468) or the field wιndιng(469) and the selenoιd(473) generates an alternating current in the armature wιndιng(476 ) of selenoid 81 A propulsion unιt(1 , 60,67,89,95, 124, 151 ,21 1 ,265,319) according to any of claims 1, 2, 1 1 , 12,

05 18, 19, 22, 25, 36, 38, 47 and 78, wherein the shaft(465) drives the crankshaft (466) of a reciprocating commutatorless generator(467), wherein the reciprocating generator(467) comprising one or more sets(477) each of which having one main unιt(478) and one or two secondary unιts(479), wherein each unιt(478,479) is coupled through a coupling arm(471 ) to one crank(472) of crankshaft, wherein the crankshaft(466) having two or more pairs of crank(480) each different in

10 length, wherein the main unιt(478) comprising an armature wιndιng(481) which is wound on a round core (482), wherein each secondary unιt(479) comprising three aligned poles(483) consisting of a middle pole(484) and two penpherial poles(485), wherein the middle pole(484) consists of a permanent magnet(486) or wound field wιndιng(487), characterized in that the secondary unιt(479) is fixedly mounted to a tube(488) which slides along a stationary direction rod(475), characterized in

15 that the core(482) of the mam unit slides inside the tube(488) of the secondary unit, characterized in that the mam unιt(478) alternates relative to the secondary unιt(479) and vice versa, characterized in that during movement of the mam and secondary unιts(478,479) from first position to second position and back two cycles of alternaing current are produced in the armature wιndιng(481) of the main unit, wherein each coupling arm(471 ) comprising a secondary centrifugal swιtch(449) which is 0 located on the rotating part of arm(471) around the crank(472), wherein each swιtch(449) is electncaly coupled to the armature wιndιng(481) of the main unit, characterized in that a number of armature wιndιngs(481) in which a current is generated is in relation to rotational speed of the crankshaft(466) or the shaft(465) 82. A propulsion unιt(1 ,60,67,89,95,124,151 ,211 ,265,319) according to claim 80, wherein the 5 selenoιd(473) of the secondary unιt(479) includes a secondary permanent magnet(489) or wound field wιndιng(490) which is coupled to a crak(472) of secondary crankshaft(491 ), wherein the shaft(465) is coupled to a variable speed motive power source, wherein the secondary crankshaft(491) is coupled to a rotatable housιng(492) of an electrical secondary motor(493) which is designed to counter rotate the secondary crankshaft(491) relative to rotational direction of the shaft(465) of the prime mover(450) at an electrical synchronous speed, wherein the rotor(494) of motor is fixedly mounted to the shaft(465), wherein the rotatable housιng(492) having the stator(495) of motor, characterized in that the secondary crankshaft(491 ) which is driven by secundary 05 motor(493) maintains alteranation of the secondary permanent magnet(489) relative to the selenoιd(473) at the synchronous speed during variation in rotational rate of the shaft(465) so that the stator of motor(495) and the reciprocating secondary permanent magnet(489) increase or decrease in speed relative to the stationary base(423) when the shaft(465) is slow or increase in speed, characterized in that the secondary permanent magnet(489) when moving relative to the stationary 10 base(423) moves relative to the selenoιd(473) generating in the armature winding of selenoιd(476) an additional positive or negative frequency to the frequency which is generated when the selenoιd(473) moves relative to the permanent magnet(468) at rotational rate of the shaft(465) so that a desired output frequency is generated in the selenoιd(473) irrespectively from rotational speed of the shaft(465) 1583. A propuslion unιt(238) according to claim 37, wherein the reciprocating coupling arms(247;254) of piston and cylinder moves a reciprocating commutatorless generator(496), wherein the generator (496) comprising a reciprocating permanent magnet(497) or wound field wιndιng(498) and a reciprocating selenoιd(499) or three-pole aligning frame(500) , wherein the magnet(497) or core(501) of winding and selenoιd(499) are slightly bent depending of a distance from the 20 rotational axιs(264) of coupling arms, wherein the magnet(497) or core(501) is coupled on both ends to bent rods(502) each of which fixedly mounted to connecting rods(503) which are coupled to the coupling arm(247) at an angle of 90 degrees, characterized in that the magnet(497) or core(501 ) and the selenoιd(499) moves relative each to other generating an alternating current in the selenoid (473). 2584. A propulsion unιt(265) according to claim 43, wherein the crankshafts (273) drives a crankshaft commutatorless generator(504), wherein the generator(504) comprising: two rotatable crankshafts(295;296) each with one crank(297), two solenoids (473) or three-pole aligning frame(500) wherein first one is coupled to the crank(297) of first crankshaft(295) and second one is coupled to the crank(297) of second crankshaft(296), a reciprocating permanent magnet(468) or field winding (469) which is coupled partly to the selenoιd(473) of first crankshaft(295) and partly to the selenoιd(473) of second crankshaft(296), a coupling rod(298) which rotatable couples a crank(297) of first crankshaft(295) with a crank(295) of second crankshaft (296) synchronizing rotation of both

05 crankshafts(295,296) and shafts(299), characterized in that the magnet(468) or wound field wιndιng(469) and the selenoιd(473) move relative one to another, characterized in that during one full rotation of each crank(297) two cycles of alternating current are generated in each selenoιd(473) 85 A propulsion unιt(1 ,60,67 ,89,95,124, 151 ,21 1 ,265,319) according to any of claims 1 , 11 , 12, 18, 22, 25, 36, 38 and 47, wherein the shaft(505) drives a commutatorless generator(506), wherein the

10 generator(506) comprising a rotor(507) and a stator(514) consisting of two or more close-pole frames(508), wherein the flat sides of rotor pole(509) are rotatable disposed between flat sides of frame(508), wherein the rotor(507) comprising two or more permanent magnets(510) or wound field wιndιngs(511 ) radially mounted on the shaft(505) having the flat poles(509) of same polarity located on the same side of rotor(507), wherein the shaft(505) is perpendiculary disposed relative to the

15 poles(509) of rotor, wherein each frame(508) is long enough not to obstruct rotation of the rotor(507), wherein each middle part(512) of the frame which faces the rotor(507) is wound with an armature wιndιng(513), characterized in that one segment of each armature wιndιng(513) facing the rotor poles(509), characterized in that a field of each permanent magnet(510) of the rotor(507) when closing magnetic circuit through the frame(508) generates a current in both armature wιndιngs(513)

20 each wound on one segment of frame(508), characterized in that a field winding which is produced by the generated current closing a magnetic circuit through the frame(508), characterized in that one of magnets(510) of rotor always acts on one of armature wιndιngs(513) so that generated DC power is of the same intensity 86. A propulsion unιt(1 ,60,67,89,95,124,151 ,211,265,319) according to any of claims 1 , 11 , 12, 18,

25 22, 25, 36, 38 and 47, wherein the shaft(515) drives a multi-pole generator(516), characterized in that the generator(516) comprising a plurality of armature wιndιngs(517) each of which wound on separates pole(518) of generator stator(519) and the same number of field wιndιngs(520) which are wound on two poles(521) of stator(522) of an electrical motor(523), wherein each armature wιndιng(517) of generator is connected with one field wιndιng(520) of motor through a swιtch(524), characterized in that when one or more swιtches(524) close circuits in one or more armature wιndιngs(517) a magnetic field of the rotor(525) generates a current in such armature wιndιngs(517), characterized in that a number of activated swιtches(524) increase or decrease a frequency or rotational speed of the rotor(526) of the motor(523)

87 A propulsion unit according to any of claims 76, 77,80, 81 , 83 84 and 85, wherein the AC or DC generator is used as an AC or DC electric motor if the armature or field winding is supplied by current, characterized in that the reciprocating selenoid (473) and the reciprocating permanent magnet(468) or wound field wιπdιng(469) of the electric motor act as a torque on the crankshaft(466)

88. A propulsion unιt(1 , 124,374) according to any of claims 2, 22, 57, 59 and 71 , wherein the electric motor(30) comprising two unιts(527,534), wherein main unιt(527) comprising an induction motor(528) having a rotor(529) consisting of a squirrel cage(530) and a stator(531) consists of poles (532) wound with a field winding (533), characterized in that a secondary unιt(534) comprising a rotor(535) wound with field wιndιngs(537) each of which having ends(538) coupled to a split bottom ring (532) of the squirrel cage(530) between each two bars of cage, characterized in that field wιndιngs(537) of the secondary unιt(534) having the same configuration as the squirrel cage(530), wherein the secondary unιt(534) having a stator(539) which poles(540) are wound with a field winding (541 ), wherein rotors (529, 535) of the main and secondary units are mounted on the same shaft(542), characterized in that a very strong current, which is induced in the start in the squirrel cage (530), supplies the field wιndιngs(537) of the secondary unιt(534) to produce a strong magnetic field due to a big number of wire, characterized in that the supplied current increases voltage in the field wιndιngs(537) of secondary unιt(534) which match with a high voltage of excitation current, characterized in that the strong field of the field winding (537) of secondary unit follows a rotational field of excitation current rotating the shaft(542), characterized in that the secondary unιt(534) improves a torque avoiding sleepery and a negative influence of the conventional induction motor on the network(29).

89. A propulsion unιt(1 ,124,374) according to any of claims 2, 22, 57, 59 and 71 , wherein an electric motor(30) comprising two or more unιts(543) having different diameters and different powers and different number of stator poles (544), wherein the rotor(545) of all unit are fixedly mounted on the same shaft(546), wherein each rotor(545) consists of a squirrel cage(547) or a permanent magnet(548), wherein stator poles(544) of each unit is wound with a field wιndιng(549) which is connected through a swιtch(550), characterized in that a number of activated swιtches(550) increases or decreases rotational speed of the shaft(546) and the ouput rotational force 90. A propulsιon unιt(1 ,60,67,89,95,124,151 ,211 ,265,319) accordιng to any of claims 1 , 1 1 , 12, 18, 22, 25, 36, 38 and 47, wherein the generator(6) is coupled to a rotational conventer(551), wherein the converter(551 ) comprising a small electric motor(552) having a shaft(553) and a set of slip rιngs(554) and a set of commutator plates(555) which are mounted on the shaft(553), wherein the set of slip rιngs(554) ts coupled to the set of stationary burushes(556), wherein the set of commutator plates(555) is coupled to the set of stationary brushes(557), wherein the set of slip ring (554) is conected to a direct current, wherein the motor(552) is designed to rotate at an electrical synchronous speed, characterized in that a cemf from an electric motor(558) of consumer of electric power do not influence on output frequency from the conventer(551 ) or on speed of the shaft(553) of the small electric motor(552), characterized in that rotational speed of the shaft(553) determines a commutation rate or a number of cycles of alternating current or a frequency 91 A propulsion unιt(1, 60,67,89,95,124,151 ,21 1 ,265,319) according to any of claims 1 , 1 1 , 12, 18, 22, 25, 36, 38 and 47, wherein the generator(6) is coupled to a rotational conventer(559), wherein the converter(559) comprising a small electric motor(552) having a shaft(553) and a set of non-slip rιngs(560) and a set of commutator non-slip rιngs(561 ) which are mounted on the shaft(553), wherein the motor(552) is designed to rotate at an electrical synchronous speed, wherein the set of commutator non-slip πngs(561) consists of two separate non-slip rings (562, 563) having conductive convex plates(564) each covering one half of the rιng(562,563), wherein convex plates{564) are mounted on the non-slip rιngs(562.563) on the opposite sides relative each to other, wherein the conventer(559) is located in a chamber(565) with conductive gas or with a low-radiation source which conducts electricity, characterized in that each non-slip rιng(560) and each commutator non-slip rιng(562,563) are coupled indirectlly through the gas or through the air having low-radiation, characteπzed in that the non-slip rings of the commutator set(562,563) are located between two sets of first stationary armature contacts(566) each located on the opposite side of the chamber(565), wherein each non-slip rιngs(560) is coupled indirectly with second stationary armature contact(567), characterized in that each set of the armature contacts(566) of commutator are coupled to an output connection (568), characterized in that current flows through the gas or air between each two conductors which have the shortest distance therebetween, characterized in that the distance between each two non-slip rings is greater then the distance between each stationary contact and non-slip ring, characterized in that a cemf from an electric motor(558) of consumer of electric power do not influence on output frequency from the conventer(551 ) or on speed of the shaft(553) of the small electric motor(552), characterized in that rotational speed of the shaft(553) of motor determines a commutation rate or a number of cycles of alternating current or a frequency 92 A propulsion unιt(1 ,60,67,89,95,124,151, 211 ,265,319) according to any of claims 1 , 11 , 12, 18, 22, 25, 36, 38 and 47, wherein the generator(6) is coupled to a reciprocating conventer(569), wherein the converter(569) comprising a reciprocating unιt(570) and a stationary unιt(571 ), wherein the reciprocating unιt(570) consists of two separated armature cores(572,573) each of which wound with a field wιndιng(574,575), wherein each core(572,573) includes two insulated conductive plates(576,577) each on the opposite side of a rectangular rod of the core(572,573), wherein the armature cores (572, 573) reciprocating between one set of brushes (578) consisting of two round rod(579,580) or pin, wherein first rod(579) of the brushes is located on one side of the cores(572,573) while second rod(580) of the brushes is located on the opposite side of cores (572,573), wherein first rod(579) couples first plate(576) of first core(572) or first plate(576) of second core(573), wherein the second rod(580) of the brushes couples second plate(577) of first or second plate(577) of second core(572,573), wherein the set of brushes(578) is coupled to DC source(589), wherein the plates(576) which are mounted on the same side of core(572) are coupled through conudctors(581 ) to an ouput connection (583), wherein the conductive plates(580) which are mounted on another side of core(573) are coupled through the wιndιngs(574,575) to the same output connectιon(583), wherein the windings are wound on the cores(572,573) to produce such magnetic polarity which opposed each other, wherein the stationary unιt(571 ) comprising two poles(584,585) of an open-pole frame(586), wherein each pole(584,585) is wound with a stationary field wιndιng(587,588) each producing magnetic polarity in the same direction as other when connected to DC source(589), characterized in that the reciprocating unιt(570) is located between poles(584,585) of stationary unit, characterized in that the reciprocating unιt(570) reciprocates

05 between poles(584,585) of stationary unit, characterized in that when first plate(576) is connected to first rod(579) of brushes a current from DC source(589) flows through the output connectιon(583) and through first wιndιng(587) of first core (572) coming to second plate (577) of first core (572) and second rod(580) of brushes coming back to the DC source(589), wherein such current produces a field in first wιndιng(574) which is attracted by a field of first stationary winding (587) moving

10 reciprocating unιt(570) toward the first stationary wιndιng(587) disconnecting the connection between set of brushes(578) and plates(576,577) of first core(572) but closing connection between the set of brushes(578) and the plates (576, 577) of second core(573) to continue the same process which returns the reciprocating unιt(570) on the first positon, characterized in that for each movement of reciprocating unιt(570) from first to second position and back to first positon two cycles of

15 alternamg current are produced in the output connectιon(583), characterized in that increasing or decreasing intensity of current through a resιstor(590) increases or decreases intensity of magnetic field in the stationary unιt(571) which increases or decreases alternation of the reciprocating unιt(570) and an output frequency 93. A propuslison unιt(1 ,60,67,89,95,124,151.211 ,265,319) according to claim 92, characterized in

20 that the conventer(569) is located in a chamber(591 ) with a conductive gas or a source of tow-radiation, characterized in that each rod (579,580) of the set of brushes is located at a small distance from the conductive plate(576,577) of the reciprocating unιt(570) so current is conducted through gas or air with low-radiation, characterized in that there is no friction between the conductive plates(576,577) and rods of the brushes(579,580)

2594. A propulsion unιt(1 ,60,67,89.95,124, 151 ,211 ,265,319) according to any of claims 80, 81 , 90, 91 , 92 and 93, wherein the conventer(569) of DC into AC is used as a rectifιer(592) of AC into DC 95 A propulsion unιt(238) according to claim 37, wherein the reciprocating coupling arms(247,254) of the fuel motor propulsion unιt(238) moves a pιstons(248,249) of a reciprocating pump(240) or reciprocating compressor(239), wherein the pump(240) or the comprβssor(239) comprising, two reciprocating open-top cylιnders(243,244), two pιstons(248,249) each of which reciprocates in the cylιnder(243,244),two flexible inflow hoses(259,260) each of which coupled with one cylιnder(243), two flexible outflow hoses(257,258) each of which coupled to one cylιnder(244), wherein the cylιnders(243,244) and the pιstons(248,249) are slightly bent depending on a distance from an axis of coupling arms(264), wherein the coupling arms(247,254) are designed to oscilate about a vertical or horizontal axis, wherein pιstons(248.249) are coupled to bent arms(250,251 ), wherein the bent arms(250,251 ) are coupled to coupling rods(252,253) of piston which are coupled to the coupling arm(247,254) of cylinder and piston characterized in that during each movement the coupling arm(247.254) moves first pιston(248) away from the bottom of first cylιnder(243) making low-pressure while second piston (249) at the same time moves toward the bottom of second cylιnder(249) compressing fluid therein and vice versa, characterized in that the reciprocating pιstons(248,249) and the reciprocating cylιnders(243,244) of pump or compressor simultaniously pump or compress a large volume of gas or fluid in each alternation due to the long coupling arms(247,254) or lever driven by the propulsion unιt(238,473,468)

96 A wind motor propulsion unιt(593) for a craft(3) comprising a vertical high frame(594) which is fixedly mounted to the craft(3), a verticaly round rod(595) which is movable coupled to the frame(594), a reciprocating wind driven horizontal arm (596) which is fixedly mounted with one end to the vertical rod(595), a reciprocating vertical wind driven fιn(597) having an aerod amical configuration which is fixedly mounted to the end of the wind driven arm(596), a hexagonal rod(598) which is fixedly mounted to the end of the vertical rod(595), a vertical hexagonal control tube(599) which is coupled to the downward part of the verticaly rod(595), a propulsion horizontal arm(600) which is fixedly mounted to the hexagonal tube(599), a flexiblie propulsion vertical water fιn(601) which is fixedly mounted to the end of the propulsion arm(600), a control handle(602) which is fixedly attached to the hexagonal tube(599) to control direction of movement and to couple the hexagonal tube(599) with the hexagonal rod(598), characterized in that a length of the wind driven arm(596) is greater then a length of the propulsion arm(600), characterized in that a surface of the wind driven fιn(597) is greater then a surface of the propulsion fιn(601 ), characterized in that the hexagonal control tube(599) can be lifted up by the control handle(602) to slide off from the hexagonal rod(598) to change an angular angle between the wind driven arm(596) and propulsion arm(600) in order to keep direction of movement irrespectively from direction of wind, characterized in that during oscilation in strenght and direction of wind and due to resistance and elasticity of wind driven arm(597) the wind driven fm(597) alterantes when its pushed by the wind first from one and then from antoher side and so on characterized in that the movement of wind is transfered to the propulsion fιn(601 ) which alternately repulses water moving the craft(3)

97 A wind motor propulsion unιt(603) for a craft(3) comprising a vertical high frame(594) which is fixedly mounted to the craft(3), a verticaly round rod(595) which is movable coupled to a tube of frame(604), a horizontal axιs(605) which couples the frame(594) and the tube(604) of frame, a reciprocating wind driven horizontal arm (596) which is fixedly mounted with one end to the vertical rod (595), a reciprocating horizontal wind driven fin (597) having an aerodmamical convex configuration which is fixedly mounted to the end of the wind driven arm(596), a hexagonal rod(598) which is fixedly mounted to the end of the vertical rod (595), a vertical hexagonal control tube(599) which is coupled to the downward part of the verticaly rod (595), a propulsion horizontal arm (600) which is fixedly mounted to the hexahonal tube(599), a flexib e propulsion horizontal water fιn(601) which is fixedly mounted to the end of the propulsion arm(600), a control handle(602) which is fixedly attached to the hexagonal tube(599) to control direction of movement and to couple the hexagonal tube(599) with the hexagonal rod(598), a direction wind fιn(606) which is fixedly mounted to the upper arm(596) directing the wind driven arm(596) to follow direction of wind, characterized in that the vertical rod(595) which is in the tube of frame(604) alterantes around a horizontal axιs(605), characterized in that a length of the wind driven arm(596) is greater then a length of the propulsion arm (600), characterized in that a surface of the wind driven fin (597) is greater then a surface of the propulsion fιn(601 ), characterized in that the hexagonal control tube(599) can be lifted up by the control handle(602) to slide off from the hexagonal rod(598) to change an angular angle between the wind driven arm(596) and the propulsion arm(600) in order to keep direction of movement independently from direction of wind, characterized in that during oscilation in strenght and direction of wind and due to resistance and elasticity of wind driven arm(596) the wind driven fιn(597) alterantes up anddown when its pushed by the wind first from down and then from upper side and so on, characterized in that the movement of wind is transfered to the propulsion fιn(601 ) which alternately repulses water moving the craft(3) 98. A wind motor propulsion unιt(607) for a generator(6) comprising two or more unιts(608) each of

05 which consists of a generator(6) and a propeller(64), a rotatable frame(62) which couples the generator(6) of each unιt(608), a direction fin ( 15) which directs the frame(62) toward the wind, wherein each propeller(64) rotates around a horizontal shaft(61 ) of the generator(6), wherein unιts(608) having propellers (64) and generators(6) which are different in sizes and power, characterized in that a smaller size unιt(608) is exposed to wind stream first, characterized in that

10 the axis of all propeller or shaft(61 ) of generators are in the same line, characterized in that the blades (66) of each propeller (64) do not shield blades (66) of other propeller(64), wherein the frame(62) is located on a high pole(63) or between two captive rigid balloon(24), characterized in that the frame(62) and the direction fιn(15) are used for a plurality of unιts(608), characterized in that a number of unιts(608) which are in operation is in relation to the velocity and strenght of wind

1599 A water motor propulsion unιt(609) for a generator(6) comprising a source of surplus steam(610), a captive rigid balloon(24), a condenser(611 ) consisting of a closed resevoir which is coupled to the balloon(24), a flexibile steam hose(73) which couples the source of steam(610) and the condenser(611 ), a centrifugal water turbιne(68) which is coupled to a generator(6) located on the ground, a flexibile water hose(74) which couples the condenser(61 1) and the water turbιne(68),

20 characterized in that low-temperature in the condenser(611) condenses inflowing steam in water, characterized in that the water having a high potential to drive the turbιne(68) and the generator(6) to produce electricity, characterized in that a globaie overheating could be reduced 100. A solar propulsion unιt(612) for solar cells or collector(613) comprising a captive rigid balloon(24), a conical bottom mιrror(77) which is located on the balloon(24), a solar collector

25 plate(613) having conical shape which is located in a focus of the mιrror(77), a magnifying glass(76) which covers a wide opening of the conical collector(613), a cable(27) which conducts generated electπcity to an apparatus(28) on the ground, characterized in that the collector(613) is heated by the sun's rays from both side, characterized in that an intensity of the sun's rays is increased by the mirror(77) and by the magnifying glass(76) increasing production of electricity.