CN105922830A - Flying electric vehicle - Google Patents

Flying electric vehicle Download PDF

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Publication number
CN105922830A
CN105922830A CN201510760599.3A CN201510760599A CN105922830A CN 105922830 A CN105922830 A CN 105922830A CN 201510760599 A CN201510760599 A CN 201510760599A CN 105922830 A CN105922830 A CN 105922830A
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CN
China
Prior art keywords
wing
flight
folding
seat
electric automobile
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Granted
Application number
CN201510760599.3A
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Chinese (zh)
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CN105922830B (en
Inventor
刘奥宇
刘思佳
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Yusi Feifei Automobile Hubei Province Co.,Ltd.
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Individual
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Priority to CN201510760599.3A priority Critical patent/CN105922830B/en
Publication of CN105922830A publication Critical patent/CN105922830A/en
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Publication of CN105922830B publication Critical patent/CN105922830B/en
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Abstract

The invention discloses a flying electric vehicle, which is formed by combining a chassis, wheels, storage batteries, a speed controller, a wheel motor, a propeller motor and a wing. The invention is characterized in that the pure electric flying vehicle enables the motor to drive the wheels and an engine to drive the propeller to operate, the flying electric vehicle can drive autonomously, the wing can automatically unfold and fold, the flying electric vehicle has a totally enclosed housing, and the flying state of the wing is controlled by a mechanical and electrical integration control mechanism mounted on the housing.

Description

Flight electric automobile
Technical field
The present invention relates to both can aloft fly, can drive voluntarily on ground again after landing walking, wing can before and after manipulation the most up and down, the flight electric motor car that manipulates up and down of left and right, belong to empty, two-purpose traffic tool technical field.
Background technology
The general-purpose aircraft of prior art uses fixed-wing, aircraft relies on vertical tail control aircraft to carry out left and right turn, tailplane aircraft is relied on to carry out oscilaltion, dynamic-delta-wing aircraft uses movable wing, horizontal rotating shaft and vertical hanging hinge is relied on to combine, utilize triangle stick control wing to tilt and front and back swing up and down and control aircraft left and right turn and oscilaltion, in order to alleviate flying weight, use on delta-wing aircraft slide trolley is all Unpowered wheel, take-off and landing is required for electromotor and drives propeller to move, dolly does not has the power of self, limit its range of application, additionally, after propeller-parachuting and delta-wing aircraft land, the umbrella wing cannot draw in by auto-folder, it is difficult in short time walk, this drawback never has good technical scheme solve.
Summary of the invention
It is an object of the invention to overcome the deficiencies in the prior art, it is provided that one both can aloft be flown, the land and air double-used vehicles of walking after landing, can be driven rapidly again on ground voluntarily.nullThe technical scheme is that and be achieved in that: the slide trolley structure of delta-wing aircraft and front-wheel foot controlled steering mechanism are thoroughly improved,Wheel is by driving force motor、Power accumulator、The electric-powered system that speed setting controller is bonded provides driving force,Wheel is controlled to turn to by manual steering mechanism、Propeller 22、Electromotor 21 is arranged on hovercar rear portion,The power of airflight level is provided for hovercar,Wing 16 is for can automatically draw in、The triangle collapse wing of Automatic-expanding or trapezoidal folded wing、Chain connection is hung by single hole between flight electric car body hanger bracket and wing 16,Electronic control system controls wing 16 around hinge suspension ring 17 the most up and down by tubulose stick 12、Left and right rotates upwardly and downwardly,The state of flight controlling hovercar constitutes and can aloft fly,The flight electric automobile of walking can be driven again on ground after landing,Front-wheel、On Rear wheel support frame, amortisseur is set,Amortisseur can also be not provided with,Front-wheel may be configured as one and takes turns and may be alternatively provided as two wheel constructions,Trailing wheel can arrange two-wheeled or a wheel construction,Driving force motor is arranged on front-wheel hub or is arranged on rear-wheel hub or is arranged on the wheel shaft of rear two-wheeled,Manpower pedal drive mechanism can also be set on the vehicle frame of flight electric motor car,Manpower pedal drive mechanism can certainly be not provided with,Seat may be configured as single seat for single,The crossbeam of vehicle frame is lengthened backward,Two or three or four seats can be installed,Respectively for two people or three people or four people;nullVehicle frame rear portion arranges electromotor and fixes seat、Electromotor is fixed and is pacified electromotor on seat、Propeller is fixed on engine power output shaft、Safety guard is set around propeller、Safety guard can not also be set,Engine fuel tank is arranged on vehicle frame、The front portion of car is backward,Rear portion arranges forward wing hanger bracket,Front portion arranges wing front overhang hanger 3 backward,Wing front overhang hanger 3 is that two, left and right bracing frame is constituted,Before being easy to reserve for tubulose stick 12、After、Left、Move right the space of operation,Rear portion arranges forward single or double joint wing rear overhang hanger 19,The front portion of car is backward,Rear portion forward before and after hanger bracket be jointly combined into wing hanger bracket,Wing hanger bracket top arranges hinge,The umbrella wing is installed on wing hanger bracket、It is connected through the hinge between wing and electric motor car,Wing hanger bracket can also be hidden in the enclosure of flight electric automobile,Airfoil material is arranged on trapezoidal skeleton or constitutes on dalta wing skeleton,Aerofoil surface material uses the airfoil material identical with prior art delta-wing aircraft,Wing is can Automatic-expanding and the folding wing of gathering automatically,The Automatic-expanding of wing and automatic gathering mechanism be--nut--motor external member actuator by long screw,It is driven through the relative position fixing between bar in the middle part of hinged leading edge of a wing wing to constitute,Certainly actuator can also use the hydraulic jack extensible member of motor-driven to constitute、Or actuator uses cylinder to constitute,The reducing motor reduction gearing that can also use actuator directly engages hinge shaft gear and constitutes.nullWing-body is movable,Manipulation wing motion is controlled by the electronic control system of wing,The electronic control system of wing is bonded by being fixed on the portal frame type X-Y two dimension line slideway electric drive arranged bottom the tubulose stick of wing central shaft and tubulose stick,On the driving slide block of actuator, universal sleeve pipe is set,Tubulose stick passes universal sleeve pipe,Tubulose stick bottom is provided with perpendicular reinforcement cross bar,The left and right sides strengthening cross bar is provided with telescopic lever in the middle part of the leading edge of a wing,It is used for reinforcing the skeleton of wing,After wing draws in, wing afterbody is clamped by telescopic wing collection frame receipts,The wing avoiding flight electric motor car produces to jolt when ground running and causes wing skeleton metal fatigue,The vehicle body of flight electric motor car is open design or carries totally-enclosed or semiclosed shell mechanism,Sheathing material uses alloy in lightweight such as aluminium alloy、Magnalium or use titanium alloy or carbon fiber or Graphene to constitute,Shell moulding can use all fuel-engined vehicles of prior art or electric automobile especially sedan-chair to run moulding,Especially profile shown in Fig. 1 or sports car profile or egg shape profile,Flight electromobile at top or front portion can arrange first aid parachute,Certainly,Also first aid parachute can be not provided with.The motor operated driving mechanism that the flight electric automobile of the present invention is arranged due to wheel; make it have from walking function; wing can draw in automatic by Automatic-expanding simultaneously; the flight electric automobile making the present invention can either aloft freely circle in the air as light aerocraft; arriving at the destination can select again the road that vehicle is few land rapidly and draw rapidly wing in behind overhead; freely drive on highway as common electric car, be rapidly achieved destination.The vehicle body design letter refining of the flight electric automobile of the present invention, light structure, electrokinetic cell uses the accumulator that Unit Weight energy density is big, such as various lithium batteries or lithium-air battery or zinc-air battery or aluminium-air cell, Ni-MH battery, fuel cell, especially graphene battery such as Spain Graphenano company and the graphene battery etc. of Cole Wa Duo university of Spain R & D Cooperation, motor uses portable motor, such as the driving motor of outer rotor hub motor or band differential mechanism.
The present invention is further detailed explanation with specific embodiment below in conjunction with the accompanying drawings.
Accompanying drawing illustrates:
null1. front-wheel in figure,2. front hub,3. wing hangs side arm,The most totally-enclosed car shell,5. cab windshield,6. car door,7. electric drive Y guide rail,8. electric drive fixes seat,9. tubulose joystick driver car,10. the universal slide cartridge of twin shaft,11. electric drive X guide rails,12. tubulose sticks,13. telescopic levers,14. leading edge of a wing skeletons,15. wing girders,16. wings,17. hinge suspension ring,18. wing collection frames,19. wings hang after-frame,20. Propeller Guard framves,21. electromotors,22. propellers,23. propeller fixed plates,24. engine power output shafts,25. electromotor fixed supports,26. exhaustors,27. fuel tanks,28. trailing wheels,29. rear-wheel hubs,30. crossbeams,32. tubulose operating handle fixed seats,33. ball-type hinge,34. pull bar expansion links,35. pull bar expansion link anti-avulsion pins,36. anti-avulsion cotter ways,37. girder backward pull ropes,38. nut fixing seats,39. screw mandrels,40. nuts,Seat fixed by 41. folding electric machines,42. folding shaft,43. folding electric machines,Seat fixed by 44. folding electric machines,45. wing heads fix seat,46. girder forward pull ropes,47. trouserss,48. auxiliary girder shaft seats,49. auxiliary girders,50. spherical cavities,51. universal spherical sleeve pipes,52. universal spherical sleeve pipe cylindrical cavities,53. spherical cavity upper covers,54. spherical cavity upper cover fixing threaded holes,55. nut rotating shafts,56. rotating shafts.
Fig. 1 is the structural representation of flight electric automobile of the present invention;
Fig. 2 is flight electric automobile folded wing structural representation of the present invention;
Fig. 3 is flight electric automobile wing-folding structural representation of the present invention;
Fig. 4 is the driving bassinet structure schematic diagram being provided with tubulose stick;
Fig. 5 is tubulose joystick driver Herba Plantaginis push mode schematic diagram;
Fig. 6 is folded wing actuator assembly top view;
Fig. 7 is folded wing actuator assembly front view.
Detailed description of the invention:
nullFlight electric automobile shown in Fig. 1,By vehicle frame、Front-wheel 1、Trailing wheel 28、Seat、Driving force motor、Power accumulator、Speed setting controller、Steering mechanism、Braking mechanism、Electromotor 21、Propeller 22、Fuel tank 27、Wing 16、Wing control system is bonded can be from the flight electric automobile of walking,Front-wheel、Trailing wheel arranges amortisseur,Front-wheel may be configured as one and takes turns and may be alternatively provided as two wheel constructions,Trailing wheel can arrange two-wheeled or a wheel construction,Arranging in car arranges essentially identical with the electric motor car of prior art,Seat is set in electric motor car、Driving force motor、Power accumulator、Speed setting controller、Steering mechanism、Braking mechanism,Seat is individual seat or many people seat,Car end arranges electromotor fixed support 25、Electromotor 21 is installed on electromotor fixed support、Propeller 22 is fixed on engine power output shaft,Or propeller 22 is fixed on the speed-changing wheel disc being connected with electromotor,Propeller 22 can be with fixed structure propeller or folding structure propeller,The front portion of flight electric automobile arranges wing front overhang hanger 3 backward,Wing front overhang hanger 3 is that two, left and right bracing frame is constituted,Before being easy to reserve for tubulose stick 12、After、Left、Move right the space of operation,Rear portion arranges forward single or double joint wing rear overhang hanger 19,Front overhang hanger 3 and rear overhang hanger 19 are bonded wing hanger bracket,Wing hanger bracket top arranges hinge seat 17,The umbrella wing 16 is installed on wing hanger bracket、It is connected by hinge axis between wing with wing hanger bracket,Wing 16 is made up of tapered airfoil or dalta wing,Wing is can Automatic-expanding and the folding wing of gathering automatically,--nut--motor external member actuator is separately mounted to folding electric machine and fixes and constitute on seat 44 and leading edge of a wing skeleton 15 by long screw for the Automatic-expanding of wing and automatic gathering mechanism,It is used for driving leading edge of a wing skeleton to launch and drawing in.Certainly the actuator of folded wing can also use the hydraulic jack extensible member of motor-driven to constitute or the actuator of folded wing uses Telescopic-cylinder part to constitute.nullAfter wing draws in, wing afterbody is clamped by telescopic wing collection frame 18 receipts,The wing avoiding flight electric motor car produces to jolt when ground running and causes wing skeleton metal fatigue,Wing-body is movable,Manipulation wing about 16、Side-to-side movement is to be controlled by the electronic control system of wing,The electronic control system of wing is bonded by being fixed on the portal frame type X-Y two dimension line slideway electric drive arranged bottom the tubulose stick of wing central shaft and tubulose stick,Y-direction is set in electric drive Y guide rail 7 and drives motor,The X guide rail 11 being arranged in Y guide rail is driven to move along Y guide rail,X is set on electric drive X guide rail to driving motor,The tubulose joystick driver car 9 being arranged on X guide rail is driven to move along X guide rail,On tubulose joystick driver car 9, spherical cavity 50 is set,Spherical cavity is closed by the spherical cavity flap of the spherical cavity upper cover 53 on top with bottom and constitutes,And fastened by screw 54 and pull bar,The outside universal spherical sleeve pipe 51 for opening through circular hole inside spherical structure is placed in spherical cavity,Tubulose stick 12 is through universal spherical sleeve pipe 51.The spherical cavity 50 universal spherical sleeve pipe of portal frame type X-Y two dimension line slideway electric drive can also be constituted in being mutually perpendicular to axle dicyclo sleeve pipe and be arranged on the tubular cavity of tubulose joystick driver car 9.The left and right sides of the crossbeam 30 arranged in tubulose stick 12 lower end, and it is provided with telescopic lever 13 between leading edge of a wing skeleton 14, it is used for reinforcing the leading edge skeleton 14 of wing, the vehicle body of flight electric automobile is open design or band totally enclosed frame or semiclosed shell mechanism, sheathing material is alloy in lightweight or carbon fiber or Graphene is constituted, and flight electromobile at top or front portion can arrange first aid parachute also can be not provided with first aid parachute.
nullFig. 2 show flight electric automobile folded wing structural representation of the present invention,Fig. 3 is flight electric automobile wing-folding structural representation of the present invention,In figs. 2 and 3,Folding wings leading edge skeleton 14 front end of the right and left has folding axis hole,Wing head is fixed seat 45 both sides and is also had folding axis hole,The middle part of fixing seat 45 fastens with wing girder 15,Folding shaft 42 is arranged on folding axis hole,The folding wings leading edge skeleton 14 of the right and left can rotate around folding shaft 42,Leading edge of a wing skeleton 14 front portion arranges nut and fixes seat 38,The outer wall of nut 40 is vertically disposed with rotating shaft,Nut rotating shaft 55 is arranged on nut and fixes the position up and down within seat 38,Folding electric machine 43 one end fastens with folding electric machine rotating seat 41,Folding electric machine is fixed and is provided with rotating shaft 56 bottom seat 41,Folding electric machine is fixed the rotating shaft 56 of seat and is arranged on folding electric machine and fixes on seat 44,Folding electric machine 43 is fixed seat 41 by folding electric machine and is rotated around rotating shaft 56,Screw mandrel 39 one end is connected with folding electric machine 43 armature spindle,Other end is socketed on nut 40,The armature spindle of folding electric machine 43 drives screw mandrel 39 to rotate forward or backwards,Foldable nose of wing skeleton 14、Wing launches or draws in;46 is girder forward pull rope, and 37 is girder backward pull rope, provides anti-airfoil bending pulling force upwards by tension ropes before and after girder for girder 15;48 is auxiliary girder shaft seat, 49 is auxiliary girder, the front end of auxiliary girder 49 arranges axis hole, auxiliary girder shaft seat 48 is fixed on leading edge of a wing skeleton 14, and the inwardly protruding position of auxiliary girder shaft seat arranges axis hole, and auxiliary girder 49 is connected on auxiliary girder shaft seat 48 by rotating shaft, and can rotate around the axis, auxiliary girder 49 and leading edge of a wing skeleton 14 form 90 degree of angles of cut or are formed more than 90 degree or be less than 90 degree of angles, and auxiliary girder 49 is in streamlined, and auxiliary girder 49 is distributed in the wing left and right sides.
Fig. 4 is the structural representation driving car being provided with tubulose stick, and Fig. 5 is tubulose joystick driver Herba Plantaginis push mode schematic diagram.The electronic control system of wing is bonded by being fixed on the portal frame type X-Y two dimension line slideway electric drive arranged bottom the tubulose stick of wing central shaft and tubulose stick, Y-direction is set in electric drive Y guide rail 7 and drives motor, the X guide rail 11 being arranged in Y guide rail is driven to move along Y guide rail, X is set on electric drive X guide rail to driving motor, the tubulose joystick driver car 9 being arranged on X guide rail is driven to move along X guide rail, on tubulose joystick driver car 9, spherical cavity 50 is set, spherical cavity is closed by the spherical cavity flap of the spherical cavity upper cover 53 on top with bottom and constitutes, and fastened by screw 54 and pull bar, the outside universal spherical sleeve pipe 51 for opening through circular hole inside spherical structure is placed in spherical cavity, tubulose stick 12 is through universal spherical sleeve pipe 51.The spherical cavity 50 universal spherical sleeve pipe of portal frame type X-Y two dimension line slideway electric drive can also be constituted in being mutually perpendicular to axle dicyclo sleeve pipe and be arranged on the tubular cavity of tubulose joystick driver car 9.
nullFig. 6 is folded wing actuator assembly top view,Fig. 7 is folded wing actuator assembly front view,38 fix seat for nut,The outer wall of nut 40 is vertically disposed with rotating shaft 55,Nut rotating shaft 55 is arranged on nut and fixes the position up and down within seat 38,Folding electric machine 43 one end fastens with folding electric machine rotating seat 41,Folding electric machine is fixed and is provided with rotating shaft 56 bottom seat 41,Folding electric machine is fixed the rotating shaft 56 of seat and is arranged on folding electric machine and fixes on seat 44,Folding electric machine 43 is fixed seat 41 by folding electric machine and is rotated around rotating shaft 56,Screw mandrel 39 one end is connected with folding electric machine 43 armature spindle,Other end is socketed on nut 40,The armature spindle of folding electric machine 43 drives screw mandrel 39 to rotate forward or backwards,Foldable nose of wing skeleton 14、Wing launches or draws in.

Claims (10)

  1. null1. a flight electric automobile,By wheel、Vehicle frame、Vehicle body、Propeller、Electromotor、Vehicle body hangs hinged wing by single hole and is bonded,It is characterized in that: wheel is by driving force motor、Power accumulator、The electric-powered system that speed setting controller is bonded provides driving force,Wheel is controlled to turn to by manual steering mechanism、The propeller (22) and the airscrew engine (21) that there is provided horizontal flight power are arranged on hovercar rear portion,Wing (16) is for can automatically draw in、The triangle collapse wing of Automatic-expanding or trapezoidal folded wing、Electronic control system controls wing (16) around hinge suspension ring (17) the most up and down by tubulose stick (12)、Left and right rotates upwardly and downwardly the state of flight of control flight electric automobile and constitutes and can aloft fly,The flight electric automobile of walking can be driven again on ground after landing.
  2. Flight electric automobile the most according to claim 1, it is characterized in that: the front-wheel (1) of flight electric motor car is taken turns by one or two-wheeled is constituted, trailing wheel (30) is taken turns by two-wheeled or one and is constituted, the manual steering mechanism of flight electric motor car is made up of steering wheel or tap, the wheel of flight electric automobile drives driving force motor to be wheel hub motor or differential speed motor, wheel hub motor is arranged at front-wheel hub or is arranged at rear-wheel hub, and differential speed motor is arranged in rear two-wheeled connecting shaft.
  3. Flight electric automobile the most according to claim 1, is characterized in that: the electronic control system of wing is bonded by being fixed on the portal frame type X-Y two dimension line slideway electric drive arranged bottom the tubulose stick of wing central shaft and tubulose stick.
  4. 4. according to the flight electric automobile described in claim 1 or 3, it is characterized in that: Y-direction is set in the electric drive Y guide rail (7) of portal frame type X-Y two dimension line slideway electric drive and drives motor, the X guide rail 11 being arranged in Y guide rail is driven to move along Y guide rail, X is set on electric drive X guide rail to driving motor, tubulose joystick driver car (9) being arranged on X guide rail is driven to move along X guide rail, spherical cavity (50) is set on tubulose joystick driver car (9), spherical cavity is closed by the spherical cavity flap of the spherical cavity upper cover (53) on top with bottom and constitutes, and fastened by screw (54) and pull bar, the outside universal spherical sleeve pipe (51) for opening through circular hole inside spherical structure is placed in spherical cavity, tubulose stick (12) passes universal spherical sleeve pipe (51).
  5. 5. According to the flight electric automobile described in claim 1 or 2 or 3, it is characterized in that: the front portion of flight electric automobile arranges wing front overhang hanger (3) backward, wing front overhang hanger (3) is that two, left and right bracing frame is constituted, rear portion arranges forward single or double joint wing rear overhang hanger (19), front overhang hanger (3) and rear overhang hanger (19) are bonded wing hanger bracket, wing hanger bracket top arranges hinge seat (17), and on wing hanger bracket, the installation umbrella wing (16), wing are connected by hinge axis between wing hanger bracket;The propeller (22) of flight electric automobile, electromotor (31) are arranged on the electromotor fixed support of body tail on (25).
  6. null6. the flight electric motor car as described in claim 1 or 2 or 3,It is characterized in that: wing (16) is made up of tapered airfoil or delta wing,Folding wings leading edge skeleton (14) front end of the right and left has folding axis hole,Wing head is fixed seat (45) both sides and is also had folding axis hole,The middle part of fixing seat (45) fastens with wing girder (15),Folding shaft (42) is arranged on folding axis hole,Folding wings leading edge skeleton (14) of the right and left can rotate around folding shaft (42),Leading edge of a wing skeleton (14) front portion arranges nut and fixes seat (38),The outer wall of nut (40) is vertically disposed with rotating shaft,Nut rotating shaft is arranged on nut and fixes the position up and down that seat (38) is internal,Folding electric machine (43) one end fastens with folding electric machine rotating seat (41),Folding electric machine rotating seat (41) bottom is provided with rotating shaft,The rotating shaft of folding electric machine rotating seat is arranged on folding electric machine and fixes on seat (44),Folding electric machine (43) passes through folding electric machine rotating seat (41) around axis of rotation,Screw mandrel (39) one end is connected with folding electric machine (43) armature spindle,Other end is socketed on nut (40),The armature spindle of folding electric machine (43) drives screw mandrel (39) to rotate forward or backwards,Foldable nose of wing skeleton (14) and wing launch or draw in.
  7. 7. the flight electric automobile as described in claim 1 or 2 or 3, it is characterized in that: auxiliary girder shaft seat (48) is fixed on leading edge of a wing skeleton (14), the inwardly protruding position of auxiliary girder shaft seat arranges axis hole, auxiliary girder (49) is connected on auxiliary girder shaft seat (48) by rotating shaft, and can rotate around the axis, auxiliary girder (49) and leading edge of a wing skeleton (14) form 90 degree of angles of cut or are formed more than 90 degree or less than 90 degree of angles, auxiliary girder (49) is in streamlined, and auxiliary girder (49) is distributed in the wing left and right sides.
  8. 8. Flight electric automobile as described in claim 1 or 2 or 3, is characterized in that: the Automatic-expanding of wing and automatic gathering mechanism are made up of the hydraulic jack extensible member of motor-driven or actuator is made up of cylinder.
  9. 9. Flight electric automobile as described in claim 1 or 2 or 3, it is characterized in that: tubulose stick (12) lower end is provided with cross bar (30), the left and right sides in cross bar (30), and being provided with the telescopic lever (13) of leading edge skeleton (14) for reinforcing wing between leading edge of a wing skeleton (14), the vehicle body of flight electric automobile is open design or totally enclosed frame structure or semiclosed shell mechanism is constituted.
  10. 10. Flight electric automobile as described in claim 1 or 2 or 3, it is characterized in that: the electrokinetic cell of flight electric automobile is by lithium battery or lithium-air battery or zinc-air battery or aluminium-air cell, Ni-MH battery, fuel cell, especially graphene battery is constituted, and flight electromobile at top or front portion can arrange first aid ejection parachute.
CN201510760599.3A 2015-11-10 2015-11-10 Flight electric car Active CN105922830B (en)

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Application Number Priority Date Filing Date Title
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Application Number Priority Date Filing Date Title
CN201510760599.3A CN105922830B (en) 2015-11-10 2015-11-10 Flight electric car

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CN105922830A true CN105922830A (en) 2016-09-07
CN105922830B CN105922830B (en) 2019-03-01

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106854853A (en) * 2017-02-28 2017-06-16 南京铝翔航空科技有限公司 A kind of helistop of detachable storage
CN107945645A (en) * 2017-11-07 2018-04-20 南昌启扬科技有限公司 Model plane driving and its control system are used in one kind teaching
CN116834487A (en) * 2021-01-30 2023-10-03 武汉发明家创新科技有限公司 Vertical take-off and landing suspension movable wing tilting flying electric automobile, take-off and landing method and lifting steering method

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Publication number Priority date Publication date Assignee Title
US20030094536A1 (en) * 2001-10-25 2003-05-22 Labiche Mitchell G. Flyable automobile
CN202357821U (en) * 2011-11-23 2012-08-01 向天立 Wing-variable micro amphibian flight vehicle
CN103692873A (en) * 2013-12-20 2014-04-02 胡新如 Amphibious aerocar
CN103770589A (en) * 2014-02-28 2014-05-07 武汉蓝天翔航空科技有限公司 Flying car
ES1135334U (en) * 2014-12-12 2015-01-14 Francisco BOSCH REIXACH Flying car (Machine-translation by Google Translate, not legally binding)
CN104723816A (en) * 2014-07-25 2015-06-24 李俊兰 Aerodynamic configuration and power allocation implement plan of air-ground sedan and service car

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030094536A1 (en) * 2001-10-25 2003-05-22 Labiche Mitchell G. Flyable automobile
CN202357821U (en) * 2011-11-23 2012-08-01 向天立 Wing-variable micro amphibian flight vehicle
CN103692873A (en) * 2013-12-20 2014-04-02 胡新如 Amphibious aerocar
CN103770589A (en) * 2014-02-28 2014-05-07 武汉蓝天翔航空科技有限公司 Flying car
CN104723816A (en) * 2014-07-25 2015-06-24 李俊兰 Aerodynamic configuration and power allocation implement plan of air-ground sedan and service car
ES1135334U (en) * 2014-12-12 2015-01-14 Francisco BOSCH REIXACH Flying car (Machine-translation by Google Translate, not legally binding)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106854853A (en) * 2017-02-28 2017-06-16 南京铝翔航空科技有限公司 A kind of helistop of detachable storage
CN106854853B (en) * 2017-02-28 2022-06-21 南京铝翔航空科技有限公司 Can dismantle helicopter air park of accomodating
CN107945645A (en) * 2017-11-07 2018-04-20 南昌启扬科技有限公司 Model plane driving and its control system are used in one kind teaching
CN116834487A (en) * 2021-01-30 2023-10-03 武汉发明家创新科技有限公司 Vertical take-off and landing suspension movable wing tilting flying electric automobile, take-off and landing method and lifting steering method

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