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Publication numberUS3269476 A
Publication typeGrant
Publication dateAug 30, 1966
Filing dateDec 2, 1963
Priority dateDec 2, 1963
Publication numberUS 3269476 A, US 3269476A, US-A-3269476, US3269476 A, US3269476A
InventorsDerek Jones
Original AssigneeCanadair Ltd
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Method to enable a ground effect machine to leap over obstacles
US 3269476 A
Abstract  available in
Previous page
Next page
Claims  available in
Description  (OCR text may contain errors)

' Aug. 30, 1966 D. JONES 3,269,476

METHOD TO ENABLE A GROUND EFFECT MACHINE TO LEAP OVER OBSTACLES Filed Dec. 2, 1963 2 Sheets-Sheet l Aug. 30, 1966 D. JONES 3,269,476

METHOD TO ENABLE A GRQUND EFFECT MACHINE T0 LEAP OVER OBSTACLES Filed Dec. 2, 1963 2 Sheets-Sheet 2 A Tn 112/5 r: 3,269,476 Ce Patented August 30, 1966 3,269,476 METHQD TU) ENABLE A GROUND EFFEQT MAQHINE T LEAP OVER UBSTACLES Derek Jones, Beaconsfield, Quebec, Canada, assignor to Canadair Limited, St. Laurent, Montreal, Quebec, Canada, a corporation of Canada Filed Dec. 2, 1963, Ser. No. 327,177 7 Claims. (Cl. 1807) This invention relates to a ground effect machine and particularly to improvements therein incorporating means to increase the energy of the vehicle sustaining media.

Conventional ground eflect machines hover above land or water on an air bubble or cushion of air disposed within a peripheral air curtain exhausted from the base of the machine. The peripheral air curtain can contain the bubble at an economical power level only when the Vehicle is operating close to the ground or water. Consequently the operating height of .the ground effect machine is normally low. The vehicle can not travel over land which has obstacles, the height of which exceeds the operating height of the machine, without navigating around them. Such detours may be extremely diflicult, and the extra time and fuel consumption involved may seriously limit the operating range of the vehicle.

It has been found that the above disadvantage can be largely overcome and a leaping effect imparted to the vehicle by suddenly applying an increase in energy to the annular peripheral curtain. This energy is generated by water under pressure converted into steam by a flash boiler and then ejected downward into the peripheral air curtain. Other fluids may be used if desired. The extra weight imparted to the machine by this adaption is insignificant.

According to the invention, the improvement in a ground etfect machine adapted to hover over a surface such as land or water on a curtain of air comprises, a fluid supply, means for converting a pre-determined quantity of said fluid into vapour under pressure, and

means for delivering said vapour under pressure to said air curtain whereby the distance separating the bottom of said machine from said surface is suddenly and temporarily increased.

The invention is illustrated by way of example in the accompanying drawings wherein,

FIGURE 1 is a diagrammatic sectional side elevation view, of a ground effect machine constructed in accordance with the present invention.

FIGURE 2 is a plan view of the ground eflfect machine shown in FIG. 1.

FIGURE 3 is a side elevation view, in section, of the ground eflect machine with a gas turbine compressor.

FIGURE 4 is a plan view of a ground eflect machine utilizing a gas turbine compressor.

Referring particularly to FIG. 1, the ground effect machine comprises a fan 1 disposed within a duct 14 adjacent the entrance thereof. The duct 14 terminates in a peripheral or annular outlet portion which surrounds a base 11 of the ground effect machine. The fan 1, when driven, forces air through the duct 14 and discharges from the duct portion 10 thereby creating a curtain of air peripherally disposed around the base 11 to trap a bubble which sustains the ground effect machine in spaced relation with respect to the ground.

The fan 1 is driven by a motor 2, which may be a turbine internal combustion engine or other suitable power source, gas turbine being preferred. The exhaust from the motor discharges from an exhaust pipe 3 and adjacent the outlet thereof is disposed a pivotally mounted pipe 4 in the form of an elbow. The pipe 4 efiectively forms a scoop for directing the exhaust gases from the motor and has a vertically operative position, shown in full lines in FIG. 1 and, an inoperative position, shown by dotted lines. In its operative position the scoop directs exhaust gases from pipe 3 to a heat exchanger 5, and is thereafter discharged to atmosphere through an exhaust duct 6. In the inoperative position, the exhaust gases are discharged directly to atmosphere from the exhaust pipe 3.

Also connected to the heat exchanger is a fluid supply duct 17 which through a pressure pump 8 is connected to a fluid supply reservoir 7. The fluid circulating portion of the heat exchanger has the outlet thereof connected to a conduit 18 which through a valve 15 is connected to an outlet 9. The outlet 9 is disposed within the conduit 14 between the fan 1 and the discharge 10 and consists of an apertured tube which may or may not include detachable nozzles.

FIGURES 1 and 2 illustrate the vehicle in a normal hovering position and the scoop 4 is in a normal inoperative position (i.e., the position illustrated in phantom in FIGURE 1) until such time as the jump characteristic is required. The scoop 4 is swung into a vertical or operative position directing the exhaust gases from the gas turbine 3 through the heat exchanger 5. Water from tank 7 is supplied under pressure by the driven pump 8 to the heat exchanger 5. The water is vaporized in the heat exchanger 5 by the high temperature exhaust gas and the high pressure steam is injected into the air stream in conduit 14 under the control of on-otf valve 15. The vapour injected into the air stream causes the machine to increase hovering height.

The pressure increase in the peripheral curtain is immediate due to the high pressure steam being applied instantaneously to the nozzles through the action of a quick action opening valve 15. The sudden increase in curtain energy at the normal hovering height causes a considerable upward momentum to the vehicle, suflicient to enable it to leap over surface obstacles. Upon dissipation of the instantaneous high pressure steam, the vehicle returns to its normal hovering height.

FIGURE 3 illustrates a ground efiect machine which has a gas turbine compressor. A portion of the high pressure air from the compressor acts as the peripheral air curtain. The remainder of the air exhausts to atmos phere or is directed to the heat exchanger as shown in FIGURE 2, the method of operation being the same as described with respect thereto.

In this embodiment the discharge duct 14 also comprises a number of separate channels 16 which project into the peripheral outlet duct 10 (see FIG. 4).

I claim:

1. In a ground effect machine having a primary power supply that produces hot gases and directs them into one channel means and that produces air flow in another channel means having an air outlet substantially beneath the machine, and adapted to hover over a surface such as land or water on a cushion of air retained by a fluid curtain at least partly supplied .through said air outlet, the improvement comprising: a heat exchanger, a water supply communicating through input ducting with said heat exchanger, means for pumping water from said water supply through said input ducting to said chamber, a scoop mounted on said ground effects machine and adapted to selectively direct the hot exhaust gases from said primary power supply to said heat exchanger to convert a predetermined quantity of said water into high pressure steam by being constructed and arranged to be alternatively disposed in an operative mode and an inoperative mode, in only the former of which said hot gases are both captured by said scoop and pass through said scoop to said heat exchanger, an output ducting from said heat exchanger communicated therewith so as to receive said high pressure steam, said output ducting terminating in at least one nozzle interposed in said other channel means, an on-off valve interposed in the fluid path defined in said input ducting and output ducting, whereby said steam under pressure is delivered through said nozzle, other channel means and air outlet to said air cushion only when said scoop is in said operative mode and said on-oif valve is on, and whereby the distance separating the bottom of .the said machine from said surface is suddenly and temporarily increased for the duration of the delivery of steam under pressure to said air cushion.

2. In a ground effect machine according to claim 1 in which the scoop is pivotable between a first operative position in which it is disengaged from the exhaust of the said primary power supply, and a second operative position in which it engages the said exhaust and captures the hot exhaust gases and directs them to the heat exchanger.

3. In a ground effect machine adapted to hover over a surface such as land or water on a cushion of air provided by a primary power source having an exhaust for the discharge of hot gases therefrom, the improvement comprising means for temporarily and intermittently injecting a media of greater density than air into said cushion momentarily to increase the distance separating the bottom of the machine from said surface and sustain it thereat for the duration of said injection, said means comprising a heat exchanger mounted on said machine adjacent said exhaust, a liquid supply connected to said heat exchanger, deflector means disposed intermediate said exhaust and heat exchanger and having a first position directing the hot gases from said primary power source to said heat exchanger to convert a selected quantity of liquid in said heat exchanger into vapour under pressure and movable to a second position permitting said hot gases to bypass said heat exchanger, conduit means connected to said heat exchanger and terminating at the opposite end in at least one nozzle disposed in an air supply for said cushion, and an on/ofi valve in said conduit selectively to inject vapour under pressure from said heat exchanger into said air cushion and thereby suddenly and temporarily raise said machine vertically to provide said greater clearance.

4. The improvement as defined in claim 3 wherein said deflector comprises a scoop pivotally mounted on said machine and pivotable from a first position where it directs the hot gases from the power source to said heat exchanger and to a second position permitting said hot gases to bypass the heat exchanger.

5. The improvement as defined in claim 4 wherein said on/off valve is a quick opening valve.

6. The improvement as defined in claim 5 including a pump for increasing the pressure of the fluid in the heat exchanger.

7. The improvement as defined in claim 6 wherein said conduit terminates in a plurality of apertures disposed in the air supply for said cushion.

References Cited by the Examiner UNITED STATES PATENTS 2,911,789 11/1959 Baker 39.18 3,001,500 9/1961 Pinnes -7 3,170,529 2/1965 Kelley et a1. 180'7 BENJAMIN HERSH, Primary Examiner.

M. S. SALES, Assistant Examiner.

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US2911789 *Aug 27, 1958Nov 10, 1959Gen ElectricRegulating system for steam-gas turbine powerplant
US3001500 *Dec 10, 1959Sep 26, 1961Pinnes Robert WGround-effect machine using steam as working fluid
US3170529 *Apr 8, 1960Feb 23, 1965Garrett CorpLift augmentation means for ground effect machines
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US3417943 *Dec 4, 1964Dec 24, 1968British Aircraft Corp LtdAir jet thrust supported craft
US3434560 *Dec 19, 1966Mar 25, 1969North American RockwellTractor-trailer with ground effect device
US3467213 *Jul 31, 1967Sep 16, 1969Dowty Rotol LtdGas turbine powered air-cushion vehicle with propulsive jet means
US4151893 *Sep 8, 1977May 1, 1979The United States Of America As Represented By The Secretary Of The NavyWing in ground effect vehicle
US6520449 *Jul 16, 2001Feb 18, 2003Vortex Holding CompanyLifting platform with positive horizontal stability
U.S. Classification180/129
International ClassificationB60V1/00, B60V1/02
Cooperative ClassificationB60V1/02
European ClassificationB60V1/02