CN1559817A - Two-purpose automobile convertible into aircraft - Google Patents
Two-purpose automobile convertible into aircraft Download PDFInfo
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- CN1559817A CN1559817A CNA2004100107217A CN200410010721A CN1559817A CN 1559817 A CN1559817 A CN 1559817A CN A2004100107217 A CNA2004100107217 A CN A2004100107217A CN 200410010721 A CN200410010721 A CN 200410010721A CN 1559817 A CN1559817 A CN 1559817A
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- 230000007246 mechanism Effects 0.000 claims description 9
- 230000005540 biological transmission Effects 0.000 claims description 3
- 241000256259 Noctuidae Species 0.000 abstract 1
- 230000009977 dual effect Effects 0.000 abstract 1
- 230000000694 effects Effects 0.000 description 6
- 238000005516 engineering process Methods 0.000 description 5
- 230000008859 change Effects 0.000 description 4
- 238000000034 method Methods 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- 238000007664 blowing Methods 0.000 description 2
- 230000001105 regulatory effect Effects 0.000 description 2
- 210000001367 artery Anatomy 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 244000144983 clutch Species 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 230000003028 elevating effect Effects 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000003912 environmental pollution Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 230000033001 locomotion Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 238000009423 ventilation Methods 0.000 description 1
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Abstract
A car able to run on road and fly in lower sky with lower speed features that two wings and tail wings are symmetrically installed to top of the car, the air inlet blowers are installed to said wings, said wing is composed of wing blades. Said tail ring consists of foldable balance rudder and lifting rudder, the centrifugal blower with dual air outlets is installed to both sides of the car, and the air nozzles are arranged under wings and car bottom.
Description
Technical field
The present invention relates to a kind of land and air double-used automobile, belong to the land and air double-used vehicle.
Background technology
Recent decades, the mankind invented the technical scheme of many kinds of hovercars.Introduce the hovercar that the American invents according to data, realized running on the ground the performance that flies in the sky.It is equipped with several fan drives, respectively by several engine drives, enough big power is arranged, and during exhaust duct air draft vertically downward, produces thrust upwards, can resemble vertical takeoff and landing the helicopter.The somebody has invented various hovercars such as propeller formula, fixed wing formula.Because automotive technology is very ripe, the technology of current aircraft is also very ripe, therefore the basis of the success of having established for the hovercar technology.But because the cost height of aircraft, and aircraft combine with automobile its technical pattern more complicated, make and require highlyer, be technical barrier so reduce cost significantly, and limited the universal of existing hovercar.Again because though existing hovercar can be as the aircraft flight of safety in the sky, but travel on the ground and can't resemble that to navigate within streets and lanes freely the automobile unblocked, because combining with aircraft, automobile make car body elongated or broaden, the inconvenience of travelling in narrow highway section even influence unhampered low of traffic.Though existing hovercar energy vertical takeoff and landing, but because of drive fan or to drive the engine power of propeller big, the noise that produces is big or spray that strong thermal current influence surrounding environment and can not be on common street or the local landing of personnel's vehicle comparatively dense, so has limited the usage range of existing hovercar.
Summary of the invention
The objective of the invention is: a kind of land and air double-used automobile is provided, and this technology is installed on automobile blows wing mechanism and can make automobile flight, landing keep the performance of automobile again, satisfies arteries of communication and requirement of environmental management, and low cost of manufacture.
Technical scheme of the present invention is: a kind of land and air double-used automobile, comprise automobile, it is characterized in that: wing and the empennage with two symmetries of its flexible connection is equipped with at the car body top of automobile, radially air intake blower fan is housed on the wing, the air outlet of this blower fan is corresponding with the fin of wing, the rotating shaft of this blower fan is connected with transmission device by power-transfer clutch, and centrifugal blower is equipped with in the car body both sides.Described fin can be constituted by an active connection for the 3rd section successively by first section of fin, second section of fin, fin.Empennage can be made of the jacking system of folding balanced rudder and balance support rudder.Centrifugal blower can be two air outlet centrifugal blowers, and its pair air outlet is located at respectively on the car body of front and back.The bottom of wing and car body can be respectively equipped with gas spout.
Advantage of the present invention is: during land locomotion, because coincidence can be rotated at automobile top by rotating mechanism in the wing end of two symmetries on roof panel, radially air intake blower fan is contained in the wing, fin is folding, the folding landing of empennage, neat reasonably arrangement of these parts makes automobile top only increase the thickness of wing, so kept the basic profile of automobile, travel to the not influence of safety traffic The coast is clear in streets and lanes, realized all functions of automobile.Because radially air intake blower fan directly blows the wing of expansion, air-flow is straight, concentrated, even, adjustable, energy consumption is low, so adopt general automobiles driving engine or turboaxle motor just can satisfy the needs of landing, low-altitude low-speed flight, so power is little, noise is low during vertical takeoff and landing, not downward straight blowing gas stream, even so the land and air double-used automobile of present technique on the common street in city or the local landing of personnel's vehicle comparatively dense do not influence the traffic normal order yet, free from environmental pollution, it has widened the usage range of hovercar.Because change the angle of the flaps down rotation that flexibly connects, the angle of attack α of fin is increased or reduce, realize regulating the function of lift, the adjustment rudder is deflection angle up or down, can change pitching moment, realize regulating elevating function, two two air outlet centrifugal blowers of automobile side symmetry, the energy balance of drying forward thrust, blowing energy boosting power ejects under the promotion of air-flow with the control gaseous spout under the booster action of two two air outlet centrifugal blowers at different directions backward, can realize aircraft landing aloft, stop, before fly, turn, functions such as organism balance, its a whole set of technical pattern is simple, and regulation and control are convenient, does not have the complicated mechanism components that is difficult to make, so can significantly reduce cost, a little more than the price of automobile, accepted by people easily, become the popular vehicle.Present technique adopts the basic structure of general-utility car, again for automobile has increased new function, makes automobile have the Lu Wulu can both be unblocked, and this new traffic tool will bring many convenience to the mankind.
Description of drawings
The present invention is further described below in conjunction with accompanying drawing.
Fig. 1 is the structural representation of the land and air double-used automobile of the present invention.
Fig. 2 is the schematic top plan view of Fig. 1 of the present invention.
Fig. 3 is the schematic side view of Fig. 1 of the present invention.
Fig. 4 is a rotating mechanism scheme drawing among Fig. 3 of the present invention.
Fig. 5 is the structural representation of fin of the present invention.
Fig. 6 is the fundamental diagram of wing of the present invention.
Fig. 7 is the structural representation of empennage of the present invention.
Fig. 8 is the structural representation of empennage balanced rudder of the present invention.
Fig. 9 is the scheme drawing of the two air outlet centrifugal blowers of the present invention.
Figure 10 is the structural representation of the land and air double-used automobile wing-folding of the present invention coincidence status.
Figure 11 is the birds-eye view of Figure 10 of the present invention.
Figure 12 is the lateral plan of Figure 10 of the present invention.
1 gas spout among the figure, 2 driving engines, 3 change-speed boxs, 4 automobiles, 5 deflecting plates, 6 protecting wire nets, 7 blower fans of air intake radially, 8 honeycomb screens, 9 centrifugal blowers, 10 end plates, 11 wings, 12 fins, 13 heat pumps, 14 Hydraulic Pumps, 15 empennages, 16 blower fan axles, 17 power-transfer clutchs, 18 Power trains, first section of 19 fin, second section of 20 fin, the 3rd section of 21 fin, 22 rotating mechanisms, 23 roof panels, 24 tooth bars, 25 gears, 26 axostylus axostyles, 27 piston rods, 28 end plate hydraulic rams, 29 piston rods, 30 fixed supports, 31 hydraulic rams, 32 fixed supports, 33 slide bars, 34 slideways, 35 angle of attack α, 36 empennage oil cylinders, 37 jacking systems, 38 joysticks, 39 balanced rudders, first section of 40 balanced rudders, the 3rd section of 41 balanced rudders, 42 air outlets, 43 control cocks, 44 shutoff valves, 45 air outlets.
The specific embodiment
The car body top of land and air double-used automobile (4) is provided with wing (11), the empennage (15) of two symmetries among the figure, automotive engine (2), change-speed box (3), heat pump (13), Hydraulic Pump (14) and power drive system are housed in the car body, two air outlet centrifugal blowers (9) are equipped with in the car body both sides, also can be prerotator, wing and car body bottom surface be respectively equipped with gas spout (1) etc.Wherein automobile (4) has adopted the structure of general-utility car, has all functions of automobile.
Wing (11) is by radially blower fan of air intake (7) and fin (12) constitute.The two ends of wing (11) are provided with two end plates (10), radially the blower fan of air intake (7) is connected by casing and two end plates (10), radially the blower fan axle (16) of air intake is connected with the rotating shaft of Power train (18) on being contained in roof by power-transfer clutch (17), provide power by automotive engine (2), the ventilation inlet of this blower fan is provided with protecting wire net (6) and avoids birds to enter blower fan causing the accident, the air outlet of blower fan is corresponding with fin (12), be provided with honeycomb screen (8) in the air outlet of blower fan, the effect of honeycomb screen (8) is can comb whole air-flow to make air-flow become more straight.Fin (12) constitutes by hinged three sections.First section (19) both sides of fin and two end plates (10) are hinged respectively, end plate hydraulic ram (28) is housed respectively on the two end plates (10), fin first section (19) flexibly connects with the piston rod (29) of hydraulic ram, fin second section (20) is provided with slide bar (33), these slide bar (33) one ends are contained in the slideway (34) of end plate, first section of fin is collapsible or uphold under the effect of hydraulic ram with second section, be respectively equipped with fixed support (30) (32) on fin second section (20) and the fin the 3rd section (21), two fixed supports (30) (32) are hinged respectively with hydraulic ram (31) two ends, fin the 3rd section (21) is under the effect of hydraulic ram (31), can be rotated down certain angle and make its angle of attack α (35) that increases fin, increase lift.Wing one end flexibly connects by rotating mechanism (22) and roof panel (23), rotating mechanism (22) comprises the axostylus axostyle (26) that is connected with the wing end, this axostylus axostyle is packed on the roof panel by bearing seat, install gear (25) on the axostylus axostyle (26), this wheel and rack (24) engagement, the liquid presses piston pole of rotating mechanism (27) acts on the tooth bar (24), promotes tooth bar, gear, axostylus axostyle and wing and goes up rotation at roof panel (23).Deflecting plate (5) is equipped with in the front, top of automobile (2), and it is a streamline contour, can reduce resistance, the protection wing.
Empennage (15) is made up of balanced rudder (39), joystick (38) and jacking system (37), balanced rudder (39) is that three sections combinations are connected by hinge, the 3rd section (41) inwardly doubling of first section (40) of balanced rudder and balanced rudder, joystick (38) is connected with balanced rudder (39), pulling joystick (38) can make balanced rudder deflection up or down, change pitching moment, regulate the aircraft lifting.Jacking system (37) is the movable loop bar structure that cooperates, and controls the action that rises or fall by empennage oil cylinder (36).
Two air outlet centrifugal blowers (9) are packed in the car body both sides of automobile, are respectively equipped with shutoff valve (44) and control cock (43) on two discharge pipes of this blower fan, and two air outlets (42) (45) are located at car body front end, car body rear end respectively,
Wing and car body bottom surface are respectively equipped with symmetrical gas spout (1).
The power system of present technique comprises automotive engine (2), change speed gear box (3), heat pump (13), Hydraulic Pump (14) and driving system thereof, is respectively wheel, blower fan, hydraulic ram, gas spout, braking automobile etc. power is provided.
During the land mode of operation, the wing of two symmetries closes up under the effect of hydraulic ram, and the inside doubling of the balanced rudder of empennage is fallen by jacking system.Profile and performance with general-utility car.
During state of flight, under the effect of hydraulic ram, wing and fin launch simultaneously, and empennage rises, balanced rudder launches.Radially the blower fan axle of air intake blower fan is connected with transmission shaft by power-transfer clutch, engine operation, radially air intake blower fan rotates, wind-force directly blows wing and produces thrust, the difference of pressure effect of fin upper and lower surface air produces lift down, the angle of attack α that regulates fin can increase or reduce lift, the adjustment rudder is deflection angle up or down, the control lifting, discharge pipe energy balance thrust is forward opened in blower fan work in both sides, realize slowing down or braking, open backward then boosting power of discharge pipe, utilize the gas spout that is located at wing and car body bottom surface, scalable pitching balance, prevent lift-over.
Claims (9)
1, a kind of land and air double-used automobile, comprise automobile, it is characterized in that: the wing and the empennage of two symmetries are equipped with in the car body top of automobile, the wing end flexibly connects by rotating mechanism and roof panel, radially air intake blower fan is housed on the wing, the air outlet of this blower fan is corresponding with the fin of wing, and the rotating shaft of this blower fan is connected with transmission device by power-transfer clutch, and centrifugal blower is equipped with in the car body both sides.
2, according to the said a kind of land and air double-used automobile of claim 1, it is characterized in that: described fin is constituted by an active connection for the 3rd section successively by first section of fin, second section of fin, fin.
3, according to claim 1 or 2 said a kind of land and air double-used automobiles, it is characterized in that: empennage is made of the jacking system of folding balanced rudder and balance support rudder.
4, according to claim 1 or 2 said a kind of land and air double-used automobiles, it is characterized in that: the centrifugal blower of car body both sides is located at respectively on the car body of front and back for two air outlet centrifugal blowers, its pair air outlet.
5, according to the said a kind of land and air double-used automobile of claim 3, it is characterized in that: the centrifugal blower of car body both sides is located at respectively on the car body of front and back for two air outlet centrifugal blowers, its pair air outlet.
6, according to claim 1 or 2 said a kind of land and air double-used automobiles, it is characterized in that: the bottom of wing and car body is respectively equipped with gas spout.
7, according to the said a kind of land and air double-used automobile of claim 3, it is characterized in that: the bottom of wing and car body is respectively equipped with gas spout.
8, according to the said a kind of land and air double-used automobile of claim 4, it is characterized in that: the bottom of wing and car body is respectively equipped with gas spout.
9, according to the said a kind of land and air double-used automobile of claim 5, it is characterized in that: the bottom of wing and automobile is respectively equipped with gas spout.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2004100107217A CN100344470C (en) | 2004-03-03 | 2004-03-03 | Two-purpose automobile convertible into aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2004100107217A CN100344470C (en) | 2004-03-03 | 2004-03-03 | Two-purpose automobile convertible into aircraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1559817A true CN1559817A (en) | 2005-01-05 |
| CN100344470C CN100344470C (en) | 2007-10-24 |
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ID=34440014
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNB2004100107217A Expired - Fee Related CN100344470C (en) | 2004-03-03 | 2004-03-03 | Two-purpose automobile convertible into aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN100344470C (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103009948A (en) * | 2013-01-16 | 2013-04-03 | 温和 | Lift force supplying device of flying car without wings |
| CN103522858A (en) * | 2013-10-16 | 2014-01-22 | 北京航空航天大学 | Flying passenger car |
| CN104369635A (en) * | 2014-10-31 | 2015-02-25 | 蔡闯 | Air-ground amphibious vehicle |
| CN104787329A (en) * | 2013-07-26 | 2015-07-22 | 哈尔滨工程大学 | Lifting single bodies for vertical landing gear with fixed wings |
| CN106275421A (en) * | 2015-06-04 | 2017-01-04 | 陈志石 | A kind of unmanned transporter |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4537373A (en) * | 1979-08-16 | 1985-08-27 | Butts Dennis D | Air vehicle having driven wheels and ducted fans |
| CN1074373C (en) * | 1995-09-29 | 2001-11-07 | 克里斯蒂安·奥德纳松工程公司 | Aircraft with jet flap propulsion |
| US6604706B1 (en) * | 1998-08-27 | 2003-08-12 | Nicolae Bostan | Gyrostabilized self propelled aircraft |
| CN1269307A (en) * | 2000-01-07 | 2000-10-11 | 王新云 | Flyer with centrifugal fan for launching and landing vertically |
| CN2714355Y (en) * | 2004-03-03 | 2005-08-03 | 陈博 | Two purpose automobile used for land and air |
-
2004
- 2004-03-03 CN CNB2004100107217A patent/CN100344470C/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103009948A (en) * | 2013-01-16 | 2013-04-03 | 温和 | Lift force supplying device of flying car without wings |
| CN104787329A (en) * | 2013-07-26 | 2015-07-22 | 哈尔滨工程大学 | Lifting single bodies for vertical landing gear with fixed wings |
| CN104787329B (en) * | 2013-07-26 | 2017-01-25 | 哈尔滨工程大学 | Lifting single bodies for vertical landing gear with fixed wings |
| CN103522858A (en) * | 2013-10-16 | 2014-01-22 | 北京航空航天大学 | Flying passenger car |
| CN104369635A (en) * | 2014-10-31 | 2015-02-25 | 蔡闯 | Air-ground amphibious vehicle |
| CN106275421A (en) * | 2015-06-04 | 2017-01-04 | 陈志石 | A kind of unmanned transporter |
| CN106275421B (en) * | 2015-06-04 | 2018-06-01 | 陈志石 | A kind of unmanned transporter |
Also Published As
| Publication number | Publication date |
|---|---|
| CN100344470C (en) | 2007-10-24 |
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Legal Events
| Date | Code | Title | Description |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| ASS | Succession or assignment of patent right |
Owner name: ZHUHAI YUREN UAV CO., LTD. Free format text: FORMER OWNER: CHEN BO Effective date: 20120319 |
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| C41 | Transfer of patent application or patent right or utility model | ||
| COR | Change of bibliographic data |
Free format text: CORRECT: ADDRESS; FROM: 132013 JILIN, JILIN PROVINCE TO: 519040 ZHUHAI, GUANGDONG PROVINCE |
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| TR01 | Transfer of patent right |
Effective date of registration: 20120319 Address after: 519040 Zhuhai City Sanzao town Jinwan District Jinhu Road No. 16 Patentee after: ZHUHAI YUREN AIRCRAFT Co.,Ltd. Address before: 132013, 27-2-23, Rong Hutong, Jiangnan Great long Tun street, Jilin, Jilin Patentee before: Chen Bo |
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| CP03 | Change of name, title or address |
Address after: 519090 Guangdong province Zhuhai city Zhuhai town of Red Bay area, Shuanghu Road West Road on the north side of No. 6 workshop two Patentee after: ZHUHAI YUREN AGRICULTURAL AVIATION Co.,Ltd. Address before: Zhuhai City Sanzao town Jinwan District Jinhu Road No. 16 Patentee before: ZHUHAI YUREN AIRCRAFT Co.,Ltd. |
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| CP03 | Change of name, title or address | ||
| DD01 | Delivery of document by public notice |
Addressee: Liang Hengdong Document name: payment instructions |
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| DD01 | Delivery of document by public notice | ||
| DD01 | Delivery of document by public notice |
Addressee: ZHUHAI YUREN AGRICULTURAL AVIATION Co.,Ltd. Person in charge of patents Document name: payment instructions |
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| DD01 | Delivery of document by public notice | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20071024 |