CN104192309A - Aerodynamic force, shape and weapon layout of modern flying saucer - Google Patents
Aerodynamic force, shape and weapon layout of modern flying saucer Download PDFInfo
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- CN104192309A CN104192309A CN201410421537.5A CN201410421537A CN104192309A CN 104192309 A CN104192309 A CN 104192309A CN 201410421537 A CN201410421537 A CN 201410421537A CN 104192309 A CN104192309 A CN 104192309A
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Abstract
The invention discloses an aerodynamic force, shape and weapon layout of a modern flying saucer. The layout comprises a disk-shaped flying saucer cabin, high-efficiency thrusters arranged in peripheral compartments of the disk-shaped flying saucer cabin, and multiple weapon systems arranged in the peripheral compartments of the disk-shaped flying saucer cabin; a cockpit of the flying saucer is arranged in the center of an upper cover of the disk-shaped flying saucer cabin. The layout is characterized in that the upper cover of the disk-shaped flying saucer cabin is in the shape of an oval arc in symmetry with respect to the central axis of the disk-shaped flying saucer cabin; the bottom of the flying saucer cabin is in the shape of a flat'W' in symmetry with respect to the central axis of the disk-shaped flying saucer cabin; multiple high-efficiency side thrusters arranged in horizontal symmetry are evenly distributed in the peripheral compartments of the disk-shaped flying saucer cabin; multiple high-efficiency lower thrusters arranged in vertical symmetry are evenly distributed in the peripheral compartments of the disk-shaped flying saucer cabin; the cockpit of the flying saucer, which is arranged in the center of the upper cover of the disk-shaped flying saucer cabin, can rotate around the central axis of the disk-shaped flying saucer cabin; the multiple weapon systems are evenly distributed in the peripheral compartments of the disk-shaped flying saucer cabin.
Description
Technical field
The present invention relates to the modern times fly butterfly pneumatic with profile and weapon layout, be applicable to the various aircraft that fly butterfly structure, belong to vehicle technology field.
Background technology
Fly this noun of butterfly sees on the science fiction works of being everlasting, but the newspaper of recent years and also often have report on the net, this may be a kind of aircraft of some developed countries exploitation, may could not disclose because of its technology imperfection, trace it to its cause may be because not efficiently, propelling unit flexibly; The present invention utilizes uncle minister in ancient times's Wei patent of invention: the high efficiency propeller that " 201210457013.2 improve the method for the jet reaction thrust efficiency of aero-engine " manufactures is as power, and design good disc and fly butterfly profile, fly butterfly dream thereby realize for many years real of the mankind.
Summary of the invention
Thereby the object of this invention is to provide a kind of can utilize be arranged on disc fly the jet modern times of realizing any direction flight that flies butterfly of high efficiency propeller flexible rotating in butterfly disk surrounding cabin fly butterfly pneumatic with profile and weapon layout.
Modern times fly butterfly pneumatic with profile and weapon layout, comprise that a disc flies butterfly cabin and be arranged on disc to fly the high efficiency propeller in surrounding cabin, butterfly cabin and be arranged on disc to fly the armament systems in surrounding cabin, butterfly cabin, the driving compartment that flies butterfly is arranged on and flies butterfly cabin upper cover centre; It is characterized in that:
1, to fly butterfly cabin upper cover be to fly butterfly cabin circle center shaft as symmetrical ellipse arc taking disc to disc, flying butterfly cabin goes to the bottom as fly more smooth " W " shape that the round center shaft in butterfly cabin is symmetry taking disc, object is in the time flying butterfly horizontal flight, make the air stream flow velocity through flying butterfly cabin upper cover fly the air stream flow velocity of going to the bottom in butterfly cabin much larger than process, in the time of horizontal flight, can produce larger lift thereby make to fly butterfly, disc flies to be evenly equipped with in surrounding cabin, butterfly cabin the efficient side propeller of multiple horizontal symmetrical installations, multiple side propeller spouts all outwardly, the high-speed air flow that is its spout ejection all sprays towards fly butterfly cabin circle central axis direction away from disc, its spout of side propeller can be centered by side propeller axis Arbitrary Rotation in the cone at axis 45o angle, it is arbitrarily angled that the spout that rotates side propeller can make the high-speed air flow of side propeller ejection spray in the cone at axis 45o angle centered by side propeller axis, the spout of side propeller comprises flexible pipe, valve inner tube, valve outer tube, main jet valve, side spray valve, disc flies to be also evenly equipped with in surrounding cabin, butterfly cabin the efficient lower propelling unit of multiple vertical summetry installations, multiple lower propelling unit spouts all down, be that the high-speed air flow of its spout ejection is all towards spraying away from flying the butterfly cabin direction of going to the bottom, lower its spout of propelling unit can be centered by lower propelling unit axis Arbitrary Rotation in the cone at axis 45o angle, can to make the high-speed air flow of lower propelling unit ejection spray in the cone at axis 45o angle centered by lower propelling unit axis arbitrarily angled for the lower angle of rake spout of rotation, lower angle of rake spout comprises flexible pipe, valve inner tube, valve outer tube, main jet valve, side spray valve, lower propelling unit equates with the quantity of side propeller, and lower propelling unit and side propeller are spaced apart, being arranged on and flying the Centromedian butterfly driving compartment that flies of butterfly cabin upper cover is peach shape recklessly, fly butterfly driving compartment and can fly the circle center shaft rotation of butterfly cabin around disc, thereby can coordinate the heading adjustment that flies butterfly to fly the direction of butterfly driving compartment, its long axis of butterfly driving compartment that flies that is peach Hu shape is consistent with the heading that flies butterfly all the time, its objective is and make the microscler butterfly cockpit enclosure that flies can be along flying butterfly flight air flow line, to reduce the air-flow resistance that flies butterfly cabin upper cover, thereby guarantee flies the air-flow Rapid Flow of butterfly cabin upper cover and crosses the driving compartment both sides that fly butterfly cabin upper cover, also can make the operator can be just facing to flying butterfly heading simultaneously, more be conducive to fly the driving of butterfly chaufeur, in disc flies surrounding cabin, butterfly cabin, be evenly equipped with many cover armament systems, these armament systems and side propeller and lower propelling unit are spaced apart, and armament systems comprise the multiple armament systems such as machine gun, cannon, guided missile, rocket projectile, all lower propelling units can manipulate as work simultaneously, also can manipulate as some work, and all side propellers can not be worked simultaneously, can only manipulate as partly work simultaneously, the spout of side propeller and lower angle of rake spout can be centered by propelling unit axis the characteristic of Arbitrary Rotation in the cone at axis 45o angle, make to fly butterfly and can optionally control several lower propelling units or several side propeller work, thereby produce need arbitrarily the thrust of direction, and then can make to fly butterfly flexibly, rapidly flight.
2, the structure of side propeller is identical with lower angle of rake structure, propelling unit is by total air flue, flexible pipe, valve inner tube, valve outer tube, main jet valve, side spray valve composition, valve inner tube is arranged in valve outer tube, valve inner tube is less than valve outer tube, valve inner tube and valve outer tube are that concentric is installed, valve inner tube is main airway, the passage of valve outer wall of inner tube and valve outer tube wall composition is side air flue, side air flue air nozzle is side spray valve, main airway air nozzle is main jet valve, the high velocity air of main jet valve ejection is parallel with main airway, and high velocity air cone axis and the main airway cylinder axis of the ejection of main jet valve are overlapping, the valve outer tube nozzle end of side spray valve is an arc to main airway bending, the high velocity air that makes the high velocity air of side air flue ejection directly spray to the ejection of main airway main jet valve from the side spray valve ejection of side air flue just will leave the main jet valve position of main airway, thereby make the high velocity air of side spray valve ejection form one highdensity " air cushion " in main jet valve spout district, the high velocity air of main jet valve ejection is sprayed directly on on this highdensity " air cushion ", and then the larger reaction thrust of formation, the component direction of the high velocity air of side spray valve ejection on main airway axis, the high velocity air that sprays with the main jet valve component direction on main airway axis is contrary, the high velocity air axis of side spray valve ejection becomes a Ф angle, 90 o < Ф < 120o with main airway axis, high velocity air is introduced into total air flue, and then enter flexible pipe, after flexible pipe, major part enters into main airway, fraction enters into side air flue, the side spray air-flow spraying from the side spray valve of side air flue forms one highdensity " air cushion " at main jet valve exit end, the main jet air-flow spraying from the main jet valve of main airway is sprayed on this highdensity " air cushion ", and the reaction thrust that consequent reaction thrust produces through the high velocity air of single-nozzle ejection than the high velocity air of identical speed, same traffic is larger, flexible pipe is metallic hose or rubber tube or the nylon hose etc. of resistant to elevated temperatures metallic hose or non-refractory, regulate angle of rake high velocity air amount size, can regulate angle of rake thrust.
The present invention compared with prior art has the following advantages:
1, the stable and reliable for performance butterfly that flies is not also really made in countries in the world.
2, the propelling unit that utilizes Wei uncle minister in ancient times invention, can produce high thrust, and this propelling unit can be the high speed thermal current that jet engine produces, and can be also the high speed cold air-flow that impeller or turbo type blower fan produce.
3, the spout of side propeller and lower angle of rake spout can be in the cone at 45o angle, propelling unit axis the characteristic of Arbitrary Rotation, make to fly butterfly and can optionally control several lower propelling units or several side propeller work, thereby produce need arbitrarily the thrust of direction, and then can make to fly butterfly flexibly, rapidly flight.
Brief description of the drawings
Fig. 1 is the generalized section of the embodiment of the present invention;
Fig. 2 is schematic top plan view embodiment illustrated in fig. 1;
Fig. 3 is middle propelling unit embodiment illustrated in fig. 1, the weapon schematic diagram of arranging;
Fig. 4 is middle propeller structure schematic diagram embodiment illustrated in fig. 1.
In Fig. 1-4: 1, side propeller 2, lower propelling unit 3, fly butterfly cabin upper cover 4, fly butterfly cabin and go to the bottom 5, driving compartment 6, driving compartment caping 7, fly butterfly cabin 8, side cambered surface 9, cockpit enclosure lateral margin 10, armament systems 11, total air flue 12, total air flow 13, flexible pipe 14, valve inner tube 15, valve outer tube 16, side air flue 17, primary air 18, main airway 19, sidewind 20, main jet valve 21, side spray valve 22, main jet air-flow 23, side spray air-flow.
Detailed description of the invention
In the embodiment shown in Fig. 1-4: the modern times fly butterfly pneumatic with profile and weapon layout, comprise that a disc flies butterfly cabin 7 and be arranged on disc to fly the high efficiency propeller in 7 surrounding cabins, butterfly cabin and be arranged on disc to fly the armament systems 10 in 7 surrounding cabins, butterfly cabin, the driving compartment 5 that flies butterfly is arranged on and flies butterfly cabin upper cover 3 centres, it is characterized in that: disc flies butterfly cabin upper cover 3 for flying butterfly cabin 7 circle center shafts taking disc as symmetrical ellipse arc, fly butterfly cabin and go to the bottom 4 for fly more smooth " W " shape that the round center shafts in butterfly cabin 7 are symmetry taking disc, object is in the time flying butterfly horizontal flight, make air stream flow velocity through flying butterfly cabin upper cover 3 much larger than through flying go to the bottom 4 air stream flow velocity of butterfly cabin, in the time of horizontal flight, can produce larger lift thereby make to fly butterfly, disc flies to be evenly equipped with in 7 surrounding cabins, butterfly cabin the efficient side propeller 1 of multiple horizontal symmetrical installations, multiple side propeller 1 spouts all outwardly, the high-speed air flow that is its spout ejection all sprays towards fly butterfly cabin 7 circle central axis directions away from disc, side propeller 1 its spout can be centered by side propeller 1 axis Arbitrary Rotation in the cone at axis 45o angle, rotating high-speed air flow that the spout of side propeller 1 can make side propeller 1 spray sprays in the cone at axis 45o angle centered by side propeller 1 axis arbitrarily angled, the spout of side propeller 1 comprises flexible pipe 13, valve inner tube 14, valve outer tube 15, main jet valve 20, side spray valve 21, disc flies to be also evenly equipped with in 7 surrounding cabins, butterfly cabin the efficient lower propelling unit 2 of multiple vertical summetry installations, multiple lower propelling unit 2 spouts all down, be that the high-speed air flow of its spout ejection is all towards spraying away from flying butterfly cabin 4 directions of going to the bottom, lower propelling unit 2 its spouts can be centered by lower propelling unit 2 axis Arbitrary Rotation in the cone at axis 45o angle, the high-speed air flow that the spout of the lower propelling unit 2 of rotation can make lower propelling unit 2 spray sprays in the cone at axis 45o angle centered by lower propelling unit 2 axis arbitrarily angled, the spout of lower propelling unit 2 comprises flexible pipe 13, valve inner tube 14, valve outer tube 15, main jet valve 20, side spray valve 21, lower propelling unit 2 equates with the quantity of side propeller 1, and lower propelling unit 2 is spaced apart with side propeller 1, be arranged on and fly the Centromedian butterfly driving compartment 5 that flies of butterfly cabin upper cover 3 for peach shape recklessly, fly butterfly driving compartment 5 and can fly the 7 circle center shaft rotations of butterfly cabin around disc, thereby can coordinate the heading adjustment that flies butterfly to fly the direction of butterfly driving compartment 5, butterfly driving compartment 5 its long axis that fly that are peach Hu shape are consistent with the heading that flies butterfly all the time, its objective is and make microscler butterfly driving compartment 5 Gai Nengshun that fly fly butterfly flight air flow line, to reduce the air-flow resistance that flies butterfly cabin upper cover 3, thereby guarantee flies the air-flow Rapid Flow of butterfly cabin upper cover 3 and crosses driving compartment 5 both sides that fly butterfly cabin upper cover 3, also can make the operator can be just facing to flying butterfly heading simultaneously, more be conducive to fly the driving of butterfly chaufeur, in disc flies 7 surrounding cabins, butterfly cabin, all have many cover armament systems 10, these armament systems 10 are spaced apart with side propeller 1 and lower propelling unit 2, and armament systems 10 comprise the multiple weapons such as machine gun, cannon, guided missile, rocket projectile, all lower propelling units 2 can manipulate as work simultaneously, also can manipulate as some work, and all side propellers 1 can not be worked simultaneously, can only manipulate as partly work simultaneously, the spout of the spout of side propeller 1 and lower propelling unit 2 can be centered by propelling unit axis the characteristic of Arbitrary Rotation in the cone at axis 45o angle, make to fly that butterfly can optionally be controlled several lower propelling units 2 or several side propeller 1 is worked, thereby produce need arbitrarily the thrust of direction, and then can make to fly butterfly flexibly, rapidly flight.
The structure of side propeller 1 is identical with the structure of lower propelling unit 2, propelling unit is by total air flue 11, flexible pipe 13, valve inner tube 14, valve outer tube 15, main jet valve 20, side spray valve 21 forms, valve inner tube 14 is arranged in valve outer tube 15, valve inner tube 14 is less than valve outer tube 15, valve inner tube 14 is concentric installation with valve outer tube 15, valve inner tube 14 is main airway 18, the passage of valve inner tube 14 outer walls and valve outer tube 15 inwall compositions is side air flue 16, side air flue 16 air nozzles are side spray valve 21, main airway 18 air nozzles are main jet valve 20, the high velocity air that main jet valve 20 sprays is parallel with main airway 18, and the high velocity air cone axis that main jet valve 20 sprays and main airway 18 cylinder axis are overlapping, valve outer tube 15 nozzle end of side spray valve 21 are an arc to main airway 18 bendings, make high velocity air that side air flue 16 sprays from side spray valve 21 ejections of side air flue 16, directly spray to high velocity air that main airway 18 main jet valves 20 spray just will to have left main jet valve 20 positions of main airway 18, thereby make the high velocity air that side spray valve 21 sprays form one highdensity " air cushion " in main jet valve 20 spout districts, the high velocity air that main jet valve 20 is sprayed is sprayed directly on on this highdensity " air cushion ", and then the larger reaction thrust of formation, the component direction of the high velocity air that side spray valve 21 sprays on main airway 18 axis, the high velocity air that sprays with main jet valve 20 component direction on main airway 18 axis is contrary, the high velocity air axis that side spray valve 21 sprays becomes a Ф angle with main airway 18 axis, 90 o < Ф < 120o, high velocity air is introduced into total air flue 11, and then enter flexible pipe 13, after flexible pipe 13, major part enters into main airway 18, fraction enters into side air flue 16, the side spray air-flow 23 spraying from the side spray valve 21 of side air flue 16 forms one highdensity " air cushion " at main jet valve 20 exit end, the main jet air-flow 22 spraying from the main jet valve 20 of main airway 18 is sprayed on this highdensity " air cushion ", and the reaction thrust that consequent reaction thrust produces through the high velocity air of single-nozzle ejection than the high velocity air of identical speed, same traffic is larger, flexible pipe 13 is metallic hose or rubber tube or the nylon hose etc. of resistant to elevated temperatures metallic hose or non-refractory, regulate angle of rake high velocity air amount size, can regulate angle of rake thrust.
Claims (2)
- Modern times fly butterfly pneumatic with profile and weapon layout, comprise that a disc flies butterfly cabin (7) and be arranged on disc to fly the high efficiency propeller in surrounding cabin, butterfly cabin (7) and be arranged on disc to fly the armament systems (10) in surrounding cabin, butterfly cabin (7), the driving compartment (5) that flies butterfly is arranged on and flies butterfly cabin upper cover (3) centre, it is characterized in that: disc flies butterfly cabin upper cover (3) for flying butterfly cabin (7) circle center shaft taking disc as symmetrical ellipse arc, fly butterfly cabin and go to the bottom (4) for fly more smooth " W " shape that the round center shaft in butterfly cabin (7) is symmetry taking disc, object is in the time flying butterfly horizontal flight, make air stream flow velocity through flying butterfly cabin upper cover (3) much larger than through flying the butterfly cabin air stream flow velocity of (4) of going to the bottom, in the time of horizontal flight, can produce larger lift thereby make to fly butterfly, disc flies to be evenly equipped with in surrounding cabin, butterfly cabin (7) the efficient side propeller (1) of multiple horizontal symmetrical installations, multiple side propellers (1) spout all outwardly, the high-speed air flow that is its spout ejection all sprays towards fly butterfly cabin (7) circle central axis direction away from disc, its spout of side propeller (1) can be centered by side propeller (1) axis Arbitrary Rotation in the cone at axis 45o angle, it is arbitrarily angled that the spout that rotates side propeller (1) can make the high-speed air flow of side propeller (1) ejection spray in the cone at axis 45o angle centered by side propeller (1) axis, the spout of side propeller (1) comprises flexible pipe (13), valve inner tube (14), valve outer tube (15), main jet valve (20), side spray valve (21), disc flies to be also evenly equipped with in surrounding cabin, butterfly cabin (7) the efficient lower propelling unit (2) of multiple vertical summetry installations, multiple lower propelling units (2) spout all down, be that the high-speed air flow of its spout ejection is all towards spraying away from flying butterfly cabin (4) direction of going to the bottom, its spout of lower propelling unit (2) can be centered by lower propelling unit (2) axis Arbitrary Rotation in the cone at axis 45o angle, can to make the high-speed air flow of lower propelling unit (2) ejection spray in the cone at axis 45o angle centered by lower propelling unit (2) axis arbitrarily angled for the spout of the lower propelling unit (2) of rotation, the spout of lower propelling unit (2) comprises flexible pipe (13), valve inner tube (14), valve outer tube (15), main jet valve (20), side spray valve (21), lower propelling unit (2) equates with the quantity of side propeller (1), and lower propelling unit (2) is spaced apart with side propeller (1), be arranged on and fly the Centromedian butterfly driving compartment (5) that flies of butterfly cabin upper cover (3) for peach shape recklessly, fly butterfly driving compartment (5) and can fly butterfly cabin (7) circle center shaft rotation around disc, thereby can coordinate the heading adjustment that flies butterfly to fly the direction of butterfly driving compartment (5), its long axis of butterfly driving compartment (5) that flies that is peach Hu shape is consistent with the heading that flies butterfly all the time, its objective is and make microscler butterfly driving compartment (5) Gai Nengshun that flies fly butterfly flight air flow line, to reduce the air-flow resistance that flies butterfly cabin upper cover (3), thereby guarantee flies the air-flow Rapid Flow of butterfly cabin upper cover (3) and crosses driving compartment (5) both sides that fly butterfly cabin upper cover (3), also can make the operator can be just facing to flying butterfly heading simultaneously, more be conducive to fly the driving of butterfly chaufeur, in flying surrounding cabin, butterfly cabin (7), disc all has many cover armament systems (10), these armament systems (10) are spaced apart with side propeller (1) and lower propelling unit (2), and armament systems (10) comprise the multiple weapons such as machine gun, cannon, guided missile, rocket projectile, all lower propelling units (2) can manipulate as work simultaneously, also can manipulate as some work, and all side propellers (1) can not be worked simultaneously, can only manipulate as partly work simultaneously, the spout of the spout of side propeller (1) and lower propelling unit (2) can be centered by propelling unit axis the characteristic of Arbitrary Rotation in the cone at axis 45o angle, make to fly butterfly and can optionally control several lower propelling units (2) or several side propeller (1) work, thereby produce need arbitrarily the thrust of direction, and then can make to fly butterfly flexibly, rapidly flight.
- Modern times as claimed in claim 1 fly butterfly pneumatic with profile and weapon layout, it is characterized in that: the structure of side propeller (1) is identical with the structure of lower propelling unit (2), propelling unit is by total air flue (11), flexible pipe (13), valve inner tube (14), valve outer tube (15), main jet valve (20), side spray valve (21) composition, valve inner tube (14) is arranged in valve outer tube (15), valve inner tube (14) is less than valve outer tube (15), valve inner tube (14) is concentric installation with valve outer tube (15), valve inner tube (14) is main airway (18), the passage of valve inner tube (14) outer wall and valve outer tube (15) inwall composition is side air flue (16), side air flue (16) air nozzle is side spray valve (21), main airway (18) air nozzle is main jet valve (20), the high velocity air of main jet valve (20) ejection is parallel with main airway (18), and high velocity air cone axis and main airway (18) the cylinder axis of main jet valve (20) ejection are overlapping, valve outer tube (15) nozzle end of side spray valve (21) is an arc to main airway (18) bending, the high velocity air that makes the high velocity air of side air flue (16) ejection directly spray to main airway (18) main jet valve (20) ejection from side spray valve (21) ejection of side air flue (16) just will leave main jet valve (20) position of main airway (18), thereby make the high velocity air of side spray valve (21) ejection form one highdensity " air cushion " in main jet valve (20) spout district, the high velocity air of main jet valve (20) ejection is sprayed directly on on this highdensity " air cushion ", and then the larger reaction thrust of formation, the component direction of the high velocity air of side spray valve (21) ejection on main airway (18) axis, the high velocity air that sprays with main jet valve (20) component direction on main airway (18) axis is contrary, the high velocity air axis of side spray valve (21) ejection becomes a Ф angle with main airway (18) axis, 90 o < Ф < 120o, high velocity air is introduced into total air flue (11), and then enter flexible pipe (13), after flexible pipe (13), major part enters into main airway (18), fraction enters into side air flue (16), the side spray air-flow (23) spraying from the side spray valve (21) of side air flue (16) forms one highdensity " air cushion " at main jet valve (20) exit end, the main jet air-flow (22) spraying from the main jet valve (20) of main airway (18) is sprayed on this highdensity " air cushion ", consequent reaction thrust is than identical speed, the reaction thrust that the high velocity air of same traffic produces through the high velocity air of single-nozzle ejection is larger, flexible pipe (13) is metallic hose or rubber tube or the nylon hose etc. of resistant to elevated temperatures metallic hose or non-refractory, regulate angle of rake high velocity air amount size, can regulate angle of rake thrust.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410421537.5A CN104192309A (en) | 2014-08-26 | 2014-08-26 | Aerodynamic force, shape and weapon layout of modern flying saucer |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410421537.5A CN104192309A (en) | 2014-08-26 | 2014-08-26 | Aerodynamic force, shape and weapon layout of modern flying saucer |
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| Publication Number | Publication Date |
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| CN104192309A true CN104192309A (en) | 2014-12-10 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410421537.5A Pending CN104192309A (en) | 2014-08-26 | 2014-08-26 | Aerodynamic force, shape and weapon layout of modern flying saucer |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105083562A (en) * | 2015-09-24 | 2015-11-25 | 康柱 | Tercel I |
| CN105947199A (en) * | 2016-05-03 | 2016-09-21 | 王西银 | Autoroatation self-flinging antigravity butterfly-shaped aircraft |
| CN108995808A (en) * | 2018-08-31 | 2018-12-14 | 耿天侃 | It can the annular wing disc-shaped flying craft that can hover of VTOL |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1110238A (en) * | 1993-03-10 | 1995-10-18 | 龙英 | Flying saucer vehicle |
| CN2320534Y (en) * | 1997-06-03 | 1999-05-26 | 王镇宇 | Rotary aircraft |
| US20020153449A1 (en) * | 2000-08-08 | 2002-10-24 | Hatzistelios Nikolaos C | Flying disk shaped flying/space vehicle with the use of a new technic of thrust through the rolling of a wheel |
| CN101628626A (en) * | 2008-07-20 | 2010-01-20 | 尚德敏 | Disk aircraft |
-
2014
- 2014-08-26 CN CN201410421537.5A patent/CN104192309A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1110238A (en) * | 1993-03-10 | 1995-10-18 | 龙英 | Flying saucer vehicle |
| CN2320534Y (en) * | 1997-06-03 | 1999-05-26 | 王镇宇 | Rotary aircraft |
| US20020153449A1 (en) * | 2000-08-08 | 2002-10-24 | Hatzistelios Nikolaos C | Flying disk shaped flying/space vehicle with the use of a new technic of thrust through the rolling of a wheel |
| CN101628626A (en) * | 2008-07-20 | 2010-01-20 | 尚德敏 | Disk aircraft |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105083562A (en) * | 2015-09-24 | 2015-11-25 | 康柱 | Tercel I |
| CN105947199A (en) * | 2016-05-03 | 2016-09-21 | 王西银 | Autoroatation self-flinging antigravity butterfly-shaped aircraft |
| CN105947199B (en) * | 2016-05-03 | 2017-03-22 | 王西银 | Autoroatation self-flinging antigravity butterfly-shaped aircraft |
| CN108995808A (en) * | 2018-08-31 | 2018-12-14 | 耿天侃 | It can the annular wing disc-shaped flying craft that can hover of VTOL |
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Application publication date: 20141210 |