CN205255921U - Flight electric automobile - Google Patents
Flight electric automobile Download PDFInfo
- Publication number
- CN205255921U CN205255921U CN201520891061.1U CN201520891061U CN205255921U CN 205255921 U CN205255921 U CN 205255921U CN 201520891061 U CN201520891061 U CN 201520891061U CN 205255921 U CN205255921 U CN 205255921U
- Authority
- CN
- China
- Prior art keywords
- wing
- electric automobile
- flight
- folding
- wheel
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 230000015572 biosynthetic process Effects 0.000 claims description 7
- 239000000725 suspension Substances 0.000 claims description 6
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 5
- 229910021389 graphene Inorganic materials 0.000 claims description 4
- 230000003014 reinforcing effect Effects 0.000 claims description 3
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical group [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims description 2
- 229910018095 Ni-MH Inorganic materials 0.000 claims description 2
- 229910018477 Ni—MH Inorganic materials 0.000 claims description 2
- 239000000446 fuel Substances 0.000 claims description 2
- 229910052744 lithium Inorganic materials 0.000 claims description 2
- 230000010354 integration Effects 0.000 abstract 1
- 239000000463 material Substances 0.000 description 6
- 238000010276 construction Methods 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 239000002828 fuel tank Substances 0.000 description 3
- 229920000049 Carbon (fiber) Polymers 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 239000004917 carbon fiber Substances 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 239000004677 Nylon Substances 0.000 description 1
- 239000004952 Polyamide Substances 0.000 description 1
- 229910001069 Ti alloy Inorganic materials 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 229920001778 nylon Polymers 0.000 description 1
- 229920002647 polyamide Polymers 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 238000010112 shell-mould casting Methods 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
Landscapes
- Seats For Vehicles (AREA)
Abstract
The utility model discloses a flight electric automobile, by frame, wheel, storage battery, timing control ware, wheel motor, propeller motor, wing, combination constitute, its characterized in that electricelectric moves the carplane by the electromotor drive wheel, and by the operation of engine driven screw, flight electric automobile can independently walk, and the wing can expand automatically and draw in in, and flight electric automobile has the totally enclosed frame, and the wing state of flight is by installing the mechanical and electrical integration control mechanism operation controls on the shell.
Description
Technical field
The utility model both related to and can aloft fly, after landing, can drive voluntarily on ground again walking, wing can before and after manipulation 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
What the general-purpose aircraft of prior art adopted is fixed-wing, aircraft relies on vertical tail control aircraft to carry out left and right turn, rely on tailplane aircraft to carry out oscilaltion, what dynamic-delta-wing aircraft adopted is movable wing, rely on horizontal rotating shaft to combine with vertical hanging hinge, utilize triangle control stick control wing to tilt and swing up and down to control aircraft left and right turn and oscilaltion with front and back, in order to alleviate flying weight, what on delta-wing aircraft slide trolley, adopt is all Unpowered wheel, take-off and landing all needs motor driven screw to move, dolly does not have the power of self, limit its range of application, in addition, after propeller-parachuting and delta-wing aircraft land, the umbrella wing cannot draw in by auto-folder, in short time, be difficult to walking, this drawback is never had to good technical scheme to be solved.
Summary of the invention
The purpose of this utility model is to overcome the deficiencies in the prior art, provides one both can fly aloft, can drive voluntarily rapidly again the land and air double-used vehicles of walking after landing on ground. technical scheme of the present invention is achieved in that vehicle structure and the front-wheel foot controlled steering mechanism to delta-wing aircraft thoroughly improves, wheel is by driving force motor, power accumulator, speed setting controller provides driving force in conjunction with the electric-powered system forming, wheel is controlled and is turned to by manual steering mechanism, screw 22, engine 21 is arranged on hovercar rear portion, for hovercar provides the power of airflight level, wing 16 is for can automatically drawing in, the triangle collapse wing of Automatic-expanding or trapezoidal folded wing, between flight electric automobile vehicle body hanger bracket and wing 16, hang chain connection by single hole, it is upper and lower around hinge suspension ring 17 front and back that electronic control system is controlled wing 16 by tubulose control stick 12, the state of flight that left and right is rotated control hovercar up and down forms and can aloft fly, after landing, can drive on ground again the flight electric automobile of walking, front-wheel, on rear wheeling supporting frame, damper is set, damper also can be set, front-wheel can be set to one and take turns and also can be set to 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, on the vehicle frame of flight electric motor car, manpower pedal driving mechanism can also be set, manpower pedal driving mechanism can certainly be set, seat can be set to single seat for single, the crossbeam of vehicle frame is lengthened backward, two or three or all the people present's seat can be installed, respectively for two people or three people or four people, vehicle frame rear portion arranges engine holder, on engine holder, pacify engine, screw is fixed on engine power output shaft, screw is established safety guard around, also can not establish safety guard, engine fuel tank is arranged on vehicle frame, the front portion of car backward, rear portion arranges wing hanger bracket forward, front portion arranges wing front overhang hanger 3 backward, wing front overhang hanger 3 is that two of left and right bracing frame forms, be convenient to for before tubulose control stick 12 reserves, after, left, the space operating moves right, rear portion arranges single or double joint wing rear overhang hanger 19 forward, the front portion of car backward, rear portion front and rear suspension frame is forward combined into wing hanger bracket jointly, wing hanger bracket top arranges hinge, the umbrella wing is installed on wing hanger bracket, between wing and electric motor car, be connected through the hinge, wing hanger bracket also can be hidden in the enclosure of flight electric automobile, aerofoil material is arranged on trapezoidal skeleton or on dalta wing skeleton and forms, wing aerofoil material adopts the aerofoil material identical with prior art delta-wing aircraft, as the light weight high-strength materials such as high-strength polyamide fibre or nylon form, wing is can Automatic-expanding and the folding wing that automatically draws in, the Automatic-expanding of wing and automatically gathering mechanism be--nut--motor external member actuator by long screw, relative position between the leading edge of a wing wing middle part fixed bar that driving is connected through the hinge forms, certainly actuator can also adopt electric motor driven hydraulic jack extensible member to form, or actuator adopts cylinder to form, the reducing motor reduction gearing that can also adopt actuator directly engages hinge shaft gear and forms. wing main body is movable, manipulation wing moves by the electronic control system control of wing, the electronic control system of wing is by being fixed on the tubulose control stick of wing central shaft and the portal frame type X-Y two dimension line slideway electric drive part of tubulose control stick bottom setting in conjunction with forming, on the driving slide block of actuator, universal sleeve pipe is set, tubulose control stick is through universal sleeve pipe, tubulose control stick bottom is provided with perpendicular reinforcement cross bar, the left and right sides and the leading edge of a wing middle part of strengthening cross bar are provided with telescopic lever, be used for reinforcing the skeleton of wing, after wing draws in, wing afterbody is received and is clamped by telescopic wing collection frame, the wing of electric motor car of avoiding flying produces to jolt and causes wing skeleton metal fatigue in the time of ground running, the vehicle body of flight electric motor car is open design or is with totally-enclosed or semiclosed shell mechanism, sheathing material adopts alloy in lightweight as aluminium alloy, magnadure or employing titanium alloy or carbon fiber or Graphene form, shell moulding can adopt all fuel-engined vehicles or the electric automobile moulding of prior art, especially profile shown in Fig. 1 or sports car profile or egg shape profile, flight electric automobile top or front portion can arrange first aid parachute, certainly, first aid parachute also can be set. the motor operated driving mechanism that flight electric automobile of the present invention arranges due to wheel, make it have from walking function, wing can draw in automatic by Automatic-expanding simultaneously, flight electric automobile of the present invention can either aloft freely be circled in the air as light aerocraft, arrive at the destination and can select again the road that vehicle is few land rapidly and draw rapidly wing in behind overhead, as common electric car, on highway, freely drive, arrive at the destination fast. the vehicle body design letter of flight electric automobile of the present invention is refined, structure is light and handy, electrokinetic cell adopts the large battery of Unit Weight energy density, as various lithium batteries or lithium-air battery or zinc-air battery or aluminium-air cell, Ni-MH battery, fuel cell etc., especially graphene battery, as the graphene battery of Graphenano company of Spain and Spain Cole watt much R & D Cooperations, motor adopts portable motor, as outer rotor hub motor or the drive motors with differential mechanism.
Below in conjunction with the drawings and specific embodiments, the utility model is described in further detail.
Brief description of the drawings:
1. front-wheels in figure, 2. front hub, 3. wing hangs side arm, 4. totally-enclosed car shell, 5. driver's cabin windshield, 6. car door, 7. electric drive part Y guide rail, 8. electric drive part holder, 9. tubulose joystick driver car, 10. the universal slide cartridge of twin shaft, 11. electric drive part X guide rails, 12. tubulose control sticks, 13. telescopic levers, 14. leading edge of a wing skeletons, 15. wing girders, 16. wings, wing collection frame hinge suspension ring, 17. hinge suspension ring, 18. wing collection frames, 19. wings hang after-frame, 20. screw protective frame, 21. engines, 22. screws, 23. screw fixed heads, 24. engine power output shafts, 25. engine fixed supports, 26. blast pipes, 27. fuel tanks, 28. trailing wheels, 29. rear-wheel hubs, 30. cross bars, 32. tubulose operating handle fixed seats, 33. ball-type hinges, 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, 41. folding electric machine rotating seats, 42. folding shaft, 43. folding electric machines, 44. folding electric machine holders, 45. wing head holders, 46. girder forward pull ropes, 47. radome fairings, 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 the utility model flight electric automobile;
Fig. 2 is the utility model flight electric automobile folded wing structural representation;
Fig. 3 is the utility model flight electric automobile wing-folding structural representation;
Fig. 4 is the driving bassinet structure schematic diagram that tubulose control stick is installed;
Fig. 5 is push mode schematic diagram before tubulose joystick driver car.
Fig. 6 is folded wing actuator assembly top view;
Fig. 7 is folded wing actuator assembly front view.
Detailed description of the invention:
Flight 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, engine 21, screw 22, fuel tank 27, wing 16, wing control system can be from the flight electric automobile of walking, front-wheel in conjunction with forming, trailing wheel arranges damper, and front-wheel can be set to one and take turns and also can be set to two wheel constructions, and trailing wheel can arrange two-wheeled or a wheel construction, arranges and arrange basic identically with the electric motor car of prior art in car, and 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 engine fixed support 25, engine 21 is installed on engine fixed support, screw 22 is fixed on engine power output shaft, or screw 22 is fixed on the speed-changing wheel disc being connected with engine, screw 22 can fixed structure screw or folding structure screw, the front portion of flight electric automobile arranges wing front overhang hanger 3 backward, wing front overhang hanger 3 is that two bracing frames in left and right form, and is convenient to for before tubulose control stick 12 reserves, after, left, the move right space of operation, rear portion arranges single or double joint wing rear overhang hanger 19 forward, and front overhang hanger 3 is with rear overhang hanger 19 in conjunction with forming wing hanger brackets, and wing hanger bracket top arranges hinge seat 17, and the umbrella wing 16 is installed on wing hanger bracket, between wing and wing hanger bracket, be connected by hinge axis, wing 16 is made up of tapered airfoil or dalta wing, wing is can Automatic-expanding and the folding wing that automatically draws in,--nut--motor external member actuator is arranged on respectively on folding electric machine holder 44 and leading edge of a wing skeleton 15 and forms by long screw for the Automatic-expanding of wing and automatically gathering mechanism, is used for driving machine nose of wing skeleton launch and draw in. certainly the actuator of folded wing can also adopt the actuator of electric motor driven hydraulic jack extensible member formation or folded wing to adopt Telescopic-cylinder part to form. after wing draws in, wing afterbody is received and is clamped by telescopic wing collection frame 18, the wing of electric motor car of avoiding flying produces to jolt and causes wing skeleton metal fatigue in the time of ground running, wing main body is movable, manipulation wing 16 is upper and lower, side-to-side movement be by the electronic control system control of wing, the electronic control system of wing is by being fixed on the tubulose control stick of wing central shaft and the portal frame type X-Y two dimension line slideway electric drive part of tubulose control stick bottom setting in conjunction with forming, on electric drive part Y guide rail 7, Y-direction drive motor is set, the X guide rail 11 that driving is arranged on Y guide rail moves along Y guide rail, on electric drive part X guide rail, X is set to drive motor, the tubulose joystick driver car 9 that driving is arranged on X guide rail moves along X guide rail, on tubulose joystick driver car 9, spherical cavity 50 is set, spherical cavity is closed and forms with the spherical cavity flap of bottom by the spherical cavity upper cover 53 on top, and fastening by screw 54 and pull bar, in spherical cavity, place outside for driving the universal spherical sleeve pipe 51 that connects circular hole in spherical structure inside, tubulose control stick 12 is through universal spherical sleeve pipe 51. the spherical cavity 50 universal spherical sleeve pipes of portal frame type X-Y two dimension line slideway electric drive part can also be with forming in the mutual tubular cavity that vertically has axle dicyclo sleeve pipe to be arranged on tubulose joystick driver car 9. the left and right sides of the crossbeam 30 arranging in tubulose control stick 12 lower ends, and between leading edge of a wing skeleton 14, be provided with telescopic lever 13, be 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 formation, and flight electric automobile top or front portion can arrange first aid parachute first aid parachute also can be set.
Figure 2 shows that the utility model flight electric automobile folded wing structural representation, Fig. 3 is the utility model flight electric automobile wing-folding structural representation, in Fig. 2 and Fig. 3, folding wings leading edge skeleton 14 front ends of the right and left have folding axis hole, wing head holder 45 both sides also have folding axis hole, the middle part of holder 45 and wing girder 15 are fastening, 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 portions arrange nut holder 38, the outer wall of nut 40 is setting up and down rotating shaft, nut rotating shaft is arranged on the position up and down of nut holder 38 inside, folding electric machine 43 one end and folding electric machine rotating seat 41 are fastening, folding electric machine rotating seat 41 bottoms are provided with rotating shaft, the rotating shaft of folding electric machine rotating seat is arranged on folding electric machine holder 44, folding electric machine 43 is enclosed and is rotated around the axis by folding electric machine rotating seat 41, screw mandrel 39 one end are connected with folding electric machine 43 armature spindles, one end is socketed on nut 40 in addition, 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-wing towards upper bending pulling force 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 auxiliary girder shaft seat inwardly protruding position 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 forms the 90 degree angles of cut with leading edge of a wing skeleton 14 or formation is greater than 90 degree or is less than 90 degree angles, and auxiliary girder 49 is streamlined, and auxiliary girder 49 is distributed in the wing left and right sides.
Fig. 4 is the structural representation that the driving car of tubulose control stick is installed, and Fig. 5 is push mode schematic diagram before tubulose joystick driver car. the electronic control system of wing is by being fixed on the tubulose control stick of wing central shaft and the portal frame type X-Y two dimension line slideway electric drive part of tubulose control stick bottom setting in conjunction with forming, on electric drive part Y guide rail 7, Y-direction drive motor is set, the X guide rail 11 that driving is arranged on Y guide rail moves along Y guide rail, on electric drive part X guide rail, X is set to drive motor, the tubulose joystick driver car 9 that driving is arranged on X guide rail moves along X guide rail, on tubulose joystick driver car 9, spherical cavity 50 is set, spherical cavity is closed and forms with the spherical cavity flap of bottom by the spherical cavity upper cover 53 on top, and fastening by screw 54 and pull bar, in spherical cavity, place outside for driving the universal spherical sleeve pipe 51 that connects circular hole in spherical structure inside, tubulose control stick 12 is through universal spherical sleeve pipe 51. the spherical cavity 50 universal spherical sleeve pipes of portal frame type X-Y two dimension line slideway electric drive part can also be with forming in the mutual tubular cavity that vertically has axle dicyclo sleeve pipe to be arranged on tubulose joystick driver car 9.
Fig. 6 is folded wing actuator assembly top view, Fig. 7 is folded wing actuator assembly front view, 38 is nut holder, the outer wall of nut 40 is setting up and down rotating shaft 55, nut rotating shaft 55 is arranged on the position up and down of nut holder 38 inside, folding electric machine 43 one end and folding electric machine rotating seat 41 are fastening, folding electric machine holder 41 bottoms are provided with rotating shaft 56, the rotating shaft 56 of folding electric machine holder is arranged on folding electric machine holder 44, folding electric machine 43 rotates around rotating shaft 56 by folding electric machine holder 41, screw mandrel 39 one end are connected with folding electric machine 43 armature spindles, one end is socketed on nut 40 in addition, 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. a flight electric automobile, by wheel, vehicle frame, vehicle body, screw, engine, be combined formation with vehicle body by the hinged wing of single hole, it is characterized in that: wheel is by driving force motor, power accumulator, speed setting controller provides driving force in conjunction with the electric-powered system forming, wheel is controlled and is turned to by manual steering mechanism, provide screw (22) and the airscrew engine (21) of horizontal flight power to be arranged on hovercar rear portion, wing (16) is for can automatically drawing in, the triangle collapse wing of Automatic-expanding or trapezoidal folded wing, it is upper and lower around hinge suspension ring (17) front and back that electronic control system is controlled wing (16) by tubulose control stick (12), left and right is rotated up and down and is formed and can aloft fly, after landing, can drive on ground again the flight electric automobile of walking.
2. flight electric automobile according to claim 1, it is characterized in that: the front-wheel (1) of flight electric automobile is taken turns by one or two-wheeled forms, trailing wheel (28) is taken turns and is formed by two-wheeled or, the manual steering mechanism of flight electric motor car is made up of steering wheel or tap, it is wheel hub motor or differential speed motor that the wheel of flight electric automobile drives driving force motor, wheel hub motor is arranged on front-wheel hub place or is arranged on rear-wheel hub place, and differential speed motor is arranged on rear two-wheeled connecting axle.
3. flight electric automobile according to claim 1, is characterized in that: the electronic control system of wing is by being fixed on the tubulose control stick of wing central shaft and the portal frame type X-Y two dimension line slideway electric drive part of tubulose control stick bottom setting in conjunction with forming.
4. according to the flight electric automobile described in claim 1 or 3, it is characterized in that: on the electric drive part Y guide rail (7) of portal frame type X-Y two dimension line slideway electric drive part, Y-direction drive motor is set, the X guide rail 11 that driving is arranged on Y guide rail moves along Y guide rail, on electric drive part X guide rail, X is set to drive motor, the tubulose joystick driver car (9) that driving is arranged on X guide rail moves along X guide rail, spherical cavity (50) is set on tubulose joystick driver car (9), spherical cavity closes formation by the spherical cavity upper cover (53) on top and the spherical cavity flap of bottom, and fastening by screw (54) and pull bar, in spherical cavity, place outside for driving the universal spherical sleeve pipe (51) that connects circular hole in spherical structure inside, tubulose control stick (12) is through universal spherical sleeve pipe (51).
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 of left and right bracing frame forms, rear portion arranges single or double joint wing rear overhang hanger (19) forward, front overhang hanger (3) forms wing hanger bracket with rear overhang hanger (19) combination, wing hanger bracket top arranges hinge suspension ring (17), installs between wing (16), wing and wing hanger bracket and be connected by hinge axis on wing hanger bracket; On the screw (22) of flight electric automobile, engine fixed support that engine (21) is arranged on body tail on (25).
6. by the flight electric automobile described in claim 1 or 2 or 3, it is characterized in that: wing (16) is made up of tapered airfoil or dalta wing, folding wings leading edge skeleton (14) front end of the right and left has folding axis hole, wing head holder (45) both sides also have folding axis hole, the middle part of holder (45) and wing girder (15) are fastening, 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 holder (38), the outer wall of nut (40) is setting up and down rotating shaft, nut rotating shaft is arranged on the inner position up and down of nut holder (38), folding electric machine (43) one end and folding electric machine rotating seat (41) are fastening, 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 holder (44), folding electric machine (43) is enclosed and is rotated around the axis by folding electric machine rotating seat (41), screw mandrel (39) one end is connected with folding electric machine (43) armature spindle, one end is socketed on nut (40) in addition, 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. by the flight electric automobile 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), auxiliary girder shaft seat inwardly protruding position 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) forms the 90 degree angles of cut with leading edge of a wing skeleton (14) or formation is greater than 90 degree or is less than 90 degree angles, auxiliary girder (49) is streamlined, and auxiliary girder (49) is distributed in the wing left and right sides.
8. by the flight electric automobile described in claim 1 or 2 or 3, it is characterized in that: the Automatic-expanding of wing and automatically gathering mechanism are made up of electric motor driven hydraulic jack extensible member or actuator is made up of cylinder or actuator directly engages hinge shaft gear by reducing motor reduction gearing and forms.
9. by the flight electric automobile described in claim 1 or 2 or 3, it is characterized in that: tubulose control stick (12) lower end is provided with cross bar (30), in the left and right sides of cross bar (30), and between leading edge of a wing skeleton (14), be provided with the telescopic lever (13) of the leading edge skeleton (14) for reinforcing wing, the vehicle body of flight electric automobile is open design or totally enclosed frame structure or semiclosed shell mechanism formation.
10. by the flight electric automobile described in claim 1 or 2 or 3, it is characterized in that: the electrokinetic cell of flight electric automobile is lithium battery or lithium-air battery or zinc-air battery or aluminium-air cell, Ni-MH battery, fuel cell, graphene battery, and flight electric automobile top or front portion can arrange first aid ejection parachute.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520891061.1U CN205255921U (en) | 2015-11-10 | 2015-11-10 | Flight electric automobile |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520891061.1U CN205255921U (en) | 2015-11-10 | 2015-11-10 | Flight electric automobile |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205255921U true CN205255921U (en) | 2016-05-25 |
Family
ID=55997469
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520891061.1U Expired - Fee Related CN205255921U (en) | 2015-11-10 | 2015-11-10 | Flight electric automobile |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205255921U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106926655A (en) * | 2017-03-15 | 2017-07-07 | 上海工程技术大学 | A kind of four rotor intelligent automobiles |
| CN107792343A (en) * | 2016-09-03 | 2018-03-13 | 及兰平 | The optimization of folding wing |
| CN114393964A (en) * | 2022-01-25 | 2022-04-26 | 广东汇天航空航天科技有限公司 | Flying automobile control method and system and flying automobile |
-
2015
- 2015-11-10 CN CN201520891061.1U patent/CN205255921U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107792343A (en) * | 2016-09-03 | 2018-03-13 | 及兰平 | The optimization of folding wing |
| CN106926655A (en) * | 2017-03-15 | 2017-07-07 | 上海工程技术大学 | A kind of four rotor intelligent automobiles |
| CN114393964A (en) * | 2022-01-25 | 2022-04-26 | 广东汇天航空航天科技有限公司 | Flying automobile control method and system and flying automobile |
| CN114393964B (en) * | 2022-01-25 | 2024-02-20 | 广东汇天航空航天科技有限公司 | Method and system for controlling aerocar and aerocar |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US7815144B2 (en) | Ground air water craft | |
| US12077027B2 (en) | Personal auto-craft having automobile and vertical take-off configurations | |
| CN107757273A (en) | A kind of hovercar | |
| CN101559702A (en) | Tandem double-duct vertical take-off and landing land-air vehicle | |
| CN103213466A (en) | Flying wheel system and flying vehicle applying same | |
| CN101885295A (en) | Land and air double-used aircraft | |
| CN105922830B (en) | Flight electric car | |
| CN205255921U (en) | Flight electric automobile | |
| US2156288A (en) | Flying automobile | |
| CN113071276A (en) | Flying automobile | |
| CN110281719A (en) | Flight vehicle and its mode conversion method | |
| CN205255922U (en) | Electricelectric moves carplane | |
| CN114084344A (en) | A multi-axis rotorcraft with powered wheeled landing gear | |
| CN206218213U (en) | A kind of culvert type bionic Aircraft | |
| CN119428029A (en) | A helicopter flying car | |
| CN115091905B (en) | An electric flying car | |
| CN218229407U (en) | Multi-rotor electric manned aircraft | |
| CN106218333B (en) | Pure electric vehicle hovercar | |
| CN114852331A (en) | A manned flying car with morphological intelligence | |
| CN205273074U (en) | Electricelectric moves hovercar | |
| CN201824819U (en) | Automobile helicopter | |
| CN205326726U (en) | Flight electric motor car | |
| CN108437728B (en) | A flying car and method of using the same | |
| CN2467345Y (en) | Flying vehicle | |
| CN106671712A (en) | Flight electric vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160525 Termination date: 20201110 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |