CN205273074U - Electricelectric moves hovercar - Google Patents
Electricelectric moves hovercar Download PDFInfo
- Publication number
- CN205273074U CN205273074U CN201520891374.7U CN201520891374U CN205273074U CN 205273074 U CN205273074 U CN 205273074U CN 201520891374 U CN201520891374 U CN 201520891374U CN 205273074 U CN205273074 U CN 205273074U
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- wing
- pure electronic
- electronic flight
- folding
- wheel
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Abstract
The utility model provides a wing combines to constitute characterized by: that electricelectric moves hovercar, by wheel, frame, automobile body, screw, engine, hang hinged joint with the automobile body through the haplopore the wheel is driven by the electronic power system that dynamic electricity motivation, powered storage battery, timing control ware combine to constitute, and the wheel is set up at the hovercar rear portion by screw (22) and propeller motor (21) that the control of manual steering mechanism turns to, provides level flight power, and wing (16) constitute electricelectric moves hovercar for folding wing.
Description
Technical field
The utility model relates to and both can aloft fly, can drive voluntarily on ground again after landing walking, wing can before and after manipulate up and down, flight power truck that left and right manipulates up and down, belong to empty, two-purpose traffic tool technical field.
Background technology
What the general aircraft of prior art adopted is the fixing wing, aircraft relies on vertical fin control aircraft to carry out left and right turn, tailplane aircraft is relied on to carry out upper and lower lifting, what dynamic-delta-wing aircraft adopted is movable wing, horizontal rotating shaft is relied on to combine with vertical hanging hinge, utilize triangle control stick control wing lateral tilting tiltedly and front and back swing up and down and control aircraft left and right turn and lifting up and down, in order to alleviate flight weight, what adopt on delta-wing aircraft slide trolley is all Unpowered wheel, take-off and landing all needs engine driven water screw to move, dolly does not have the power of self, limit its range of application, in addition, after power umbrella and delta-wing aircraft land, the umbrella wing cannot draw in by auto-folder, walking it is difficult in short period of time, the technical scheme that this drawback is never good is solved.
Summary of the invention
acenaphthene Xun health Duo still quarrel shelves curtain treadle-operated tilt hammer for hulling rice closely question the fierce purine generation of comet Lei chant in a loud voice Fei Shan Hua Qiang cottonrose hibiscus fish hawk billy goat stop health Duo still quarrel shelves stare at the rampant swollen wall loess hills stalk of preparing food of the enough Ge rampant stack legendary small dragon with horns imperial decrees of Zhai loess hills prepare food send herd happiness send screen-like mountain peak dung linchpin quail plaited straw beam linchpin Zhen 19. Jiu Liang have jurisdiction over Gua a kind of scorpion and send wonderful signatures linchpin Gua Jia cangue Song larva of a tapeworm or the cercaria of a schistosome hook mulberry to prepare food to steal and simmer painting and stop that to send Meng Zhong to consider border vinegar to be worth doing be that raw meat adds and pushes away and pray horsefly Duo Zhai stewing and stop around profile shown in the high and steep of Guan or sports car profile or egg type profile; pure electronic flight automobile also can be set up journey fuel electric generator; it is finished rear emergent charging in order to power accumulator electric power in way; can not certainly arrange and set up journey fuel electric generator; pure electronic flight automobile top or front portion can arrange first aid parachute; certainly; it is possible to do not arrange first aid parachute. the motor driving machine structure that pure electronic flight automobile of the present utility model is arranged due to wheel; make it have from walking function; wing can launch and automatically draw in automatically simultaneously; flight electromobile of the present utility model can either aloft freely be circled in the air as aviette; achieving the goal can select again the road that vehicle is few to land rapidly and draw rapidly wing in behind overhead; ground; freely drive on highway as common electric car; achieve the goal ground fast. the vehicle body design letter refining of pure electronic flight automobile of the present utility model; light structure; the store battery that power cell adopts unit weight energy density big; such as various lithium cell or lithium-air battery or zinc-air battery or aluminium gas battery; nickel metal hydride battery; fuel cell; especially graphene battery; such as the graphene battery etc. of Graphenano company of Spain and the much cooperation research and development of Spain Ke Erwa; electric motor adopts portable motor, such as the drive-motor of outer rotor wheel hub motor or band differential mechanism.
Below in conjunction with the drawings and specific embodiments, the utility model is described in further detail.
Accompanying drawing illustrates:
1. front-wheel in figure, 2. front hub, 3. wing hangs front frame, 4. totally-enclosed car shell, 5. cab windshield, 6. car door, 7. electric drive part Y guide rail, 8. electric drive part permanent seat, 9. tubulose joystick driver car, 10. the universal sliding cylinder of twin shaft, 11. electric drive part X guide rails, 12. tubulose control sticks, 13. flexible pull bars, 14. wing leading edge 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. water screw protective frame, 21. engines, 22. water screws, 23. water screw retaining plates, 24. engine power output shafts, support fixed by 25. engines, 26. vapor pipes, 27. fuel containers, 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, 41. folding electric machine rotary seats, 42. folding shaft, 43. folding electric machines, 44. folding electric machine permanent seats, 45. wing head permanent seats, 46. girder F strain ropes, 47. nose cones, 48. auxiliary girder shaft seats, 49. auxiliary girders, 50. spherical chambeies, 51. universal spherical sleeve pipes, 52. universal spherical sleeve pipe cylindrical cavities, 53. spherical chamber upper covers, 54. spherical chamber upper cover fixing threaded holes.
Fig. 1 is the structural representation of the practical electronic flight automobile of Novel pure of book;
Fig. 2 is the practical Novel pure electronic flight automobile folded wing structural representation of book;
Fig. 3 is the practical Novel pure electronic flight automobile wing folded state structural representation of book;
Fig. 4 is the driving bassinet structure schematic diagram being provided with tubulose control stick;
Fig. 5 pushes away view before tubulose joystick driver car;
Fig. 6 is that folded wing actuator always becomes vertical view;
Fig. 7 is that folded wing actuator always becomes front view.
Embodiment:
Pure electronic flight automobile shown in Fig. 1, by vehicle frame, front-wheel 1, trailing wheel 28, seat, wheel electric motor, power accumulator, speed regulating control device, turning device, brake mechanism, water screw electric motor 21, water screw 22, fuel tank 27, wing 16, the electronic control system in wing course is bonded the pure electronic flight automobile that can certainly walk, front-wheel, trailing wheel arranges vibroshock, and front-wheel can be set to take turns and also can be set to two wheel constructions, and trailing wheel can arrange two and take turns or a wheel construction, arranges the power truck with prior art and arranges substantially identical, arrange seat in power truck in car, driving force motor, power accumulator, speed regulating control device, turning device, brake mechanism, seat is individual seat or many people seat, and car end arranges the fixing support 25 of engine, engine 21 installed by the fixing support of engine, water screw 22 is fixed on engine power output shaft, or water screw 22 is fixed on the speed-changing wheel disc being connected with engine, water screw 22 can fixed sturcture water screw or folding structure water screw, the front portion of pure electronic flight automobile arranges wing front overhang hanger 3 backward, wing front overhang hanger 3 is that two bracing frames in left and right are formed, and is convenient to as before tubulose control stick 12 reserves, after, left, moving right the space of operation, rear portion arranges hanger bracket 19 after single root or double joint wing forward, and front overhang hanger 3 and rear hanger bracket 19 are bonded wing hanger bracket, and wing hanger bracket top arranges hinge suspension ring 17, and wing hanger bracket is installed the umbrella wing 16, it is connected by hinge suspension ring between wing with wing hanger bracket, wing 16 is made up of tapered airfoil or dalta wing, wing is the collapsible wing that can automatically launch and automatically draw in,--nut--electric motor external member actuator is arranged on folding electric machine permanent seat 44 and wing leading edge skeleton 15 to form respectively by long screw for the automatic expansion of wing and automatic gathering mechanism, is used for driving wing leading edge skeleton launch and draw in. the flexible part of the hydraulic ram that the actuator of certain folded wing can also adopt electric motor to drive is formed or the actuator of folded wing adopts the flexible part of cylinder to form. after wing gathering, wing afterbody is received by the wing collection frame 18 that stretches and is clamped, the wing of flight power truck is avoided to produce when ground running to jolt to cause wing skeleton metal fatigue, wing main body is movable, manipulation wing about 16, what moved in left and right is by the electronic control system control of wing, by being fixed on, the portal frame type X-Y two dimension line slideway electric drive part arranged bottom the tubulose control stick of wing central shaft and tubulose control stick is bonded the electronic control system of wing, electric drive part Y guide rail 7 arranges Y-direction drive motor, the X guide rail 11 being arranged in Y guide rail is driven to move along Y guide rail, electric drive part X guide rail arranges X to drive motor, the tubulose joystick driver car 9 being arranged on X guide rail is driven to move along X guide rail, tubulose joystick driver car 9 arranges spherical chamber 50, spherical chamber is covered by the spherical chamber seat of the spherical chamber upper cover 53 on top with bottom and forms, and it is fastening by screw 54 and pull bar, the outside universal spherical sleeve pipe 51 opening through circular hole for globosity is inner is placed in spherical chamber, tubulose control stick 12 is through universal spherical sleeve pipe 51. the spherical chamber 50 universal spherical sleeve pipe of portal frame type X-Y two dimension line slideway electric drive part can also with mutually vertically there being the two ring set pipe of axle to be arranged in the tubular cavity of tubulose joystick driver car 9 to form. in the left and right sides of the crossbeam 30 that tubulose control stick 12 times ends are arranged, and it is provided with flexible pull bar 13 between wing leading edge skeleton 14, it is used for reinforcing the leading edge skeleton 14 of wing, the vehicle body of pure electronic flight automobile is open design or band totally enclosed frame or semiclosed containment structure, sheating material is alloy in lightweight as titanium alloy or aluminium alloy or magnalium or carbon fiber or Graphene are formed, and pure electronic flight automobile top or front portion can arrange first aid parachute also can not arrange first aid parachute.
Fig. 2 show the pure electronic flight automobile folded wing structural representation of the utility model, Fig. 3 is the pure electronic flight automobile wing pleated sheet structure schematic diagram of the utility model, in figs. 2 and 3, folding wings leading edge skeleton 14 front end of the right and left has folding axis hole, wing head permanent seat 45 both sides also have folding axis hole, middle part and the wing girder 15 of permanent seat 45 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, wing leading edge skeleton 14 front portion arranges nut permanent seat 38, the outer wall of nut 40 is vertically disposed with rotating shaft, nut rotating shaft is arranged on the position up and down of nut permanent seat 38 inside, folding electric machine 43 one end and folding electric machine rotary seat 41 are fastening, it is provided with rotating shaft bottom folding electric machine rotary seat 41, the rotating shaft of folding electric machine rotary seat is arranged on folding electric machine permanent seat 44, folding electric machine 43 passes through folding electric machine rotary seat 41 around axis of rotation, screw mandrel 39 one end is connected with folding electric machine 43 rotor spindle, one end is socketed on nut 40 in addition, the rotor spindle of folding electric machine 43 drives screw mandrel 39 to rotate forward or backwards, Foldable wing leading edge skeleton 14, wing launches or draws in, 46 is girder F strain rope, and 37 is girder backward pull rope, by tension ropes before and after girder for girder 15 provides anti-airfoil bending pulling force upwards, 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 wing leading edge 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 and wing leading edge skeleton 14 form 90 degree of angles of cut or formation is greater 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 of the driving car being provided with tubulose control stick, and Fig. 5 pushes away view before tubulose joystick driver car. by being fixed on, the portal frame type X-Y two dimension line slideway electric drive part arranged bottom the tubulose control stick of wing central shaft and tubulose control stick is bonded the electronic control system of wing, electric drive part Y guide rail 7 arranges Y-direction drive motor, the X guide rail 11 being arranged in Y guide rail is driven to move along Y guide rail, electric drive part X guide rail arranges X to drive motor, the tubulose joystick driver car 9 being arranged on X guide rail is driven to move along X guide rail, tubulose joystick driver car 9 arranges spherical chamber 50, spherical chamber is covered by the spherical chamber seat of the spherical chamber upper cover 53 on top with bottom and forms, and it is fastening by screw 54 and pull bar, the outside universal spherical sleeve pipe 51 opening through circular hole for globosity is inner is placed in spherical chamber, tubulose control stick 12 is through universal spherical sleeve pipe 51. the spherical chamber 50 universal spherical sleeve pipe of portal frame type X-Y two dimension line slideway electric drive part can also with mutually vertically there being the two ring set pipe of axle to be arranged in the tubular cavity of tubulose joystick driver car 9 to form.
Fig. 6 is that folded wing actuator always becomes vertical view, Fig. 7 is that folded wing actuator always becomes front view, 38 is nut permanent seat, the outer wall of nut 40 is vertically disposed with rotating shaft 55, nut rotating shaft 55 is arranged on the position up and down of nut permanent seat 38 inside, folding electric machine 43 one end and folding electric machine rotary seat 41 are fastening, it is provided with rotating shaft 56 bottom folding electric machine permanent seat 41, the rotating shaft 56 of folding electric machine permanent seat is arranged on folding electric machine permanent seat 44, folding electric machine 43 is rotated around rotating shaft 56 by folding electric machine permanent seat 41, screw mandrel 39 one end is connected with folding electric machine 43 rotor spindle, one end is socketed on nut 40 in addition, the rotor spindle of folding electric machine 43 drives screw mandrel 39 to rotate forward or backwards, Foldable wing leading edge skeleton 14, wing launches or draws in.
Claims (10)
1. a pure electronic flight automobile, by wheel, vehicle frame, vehicle body, water screw, engine, the wing hanging chain connection by single hole with vehicle body is bonded, it is characterized in that: wheel is by driving force motor, power accumulator, the electric-powered system that speed regulating control device is bonded drives, wheel is turned to by the control of manual turning device, water screw (22) and the water screw electric motor (21) of horizontal flight power is provided to be arranged on flight automobile rear, wing (16) is for can automatically draw in, automatically the triangle collapse wing launched or trapezoidal folded wing are formed, electronic control system is by tubulose control stick (12) control wing (16) around hinge suspension ring (17) front and back up and down, the flight state that left and right rotates the pure electronic flight automobile of control up and down forms and can aloft fly, the pure electronic flight automobile of walking can be driven again on ground after landing.
2. pure electronic flight automobile according to claim 1, it is characterized in that: the front-wheel (1) of pure electronic flight automobile is taken turns by one or two taken turns and form, trailing wheel (28) is taken turns by two or one is taken turns and form, the manual turning device of pure electronic flight automobile is made up of bearing circle or tap, the wheel of pure electronic flight automobile drives driving force motor to be wheel hub motor or differential speed motor, wheel hub motor is arranged on front-wheel wheel hub or is arranged on trailing wheel wheel hub, after differential speed motor is arranged on, two take turns on coupling shaft, the wheel electric motor of pure electronic flight automobile and water screw electric motor can share the speed regulating control device of a convertible speed governing, or each speed regulation controller is set separately, wheel electric motor and water screw electric motor arrange the power accumulator of independent use separately, or it is shared to arrange one group of power accumulator, independent or the power cell that shares is by lithium cell or lithium-air battery or zinc-air battery or aluminium gas battery, nickel metal hydride battery, fuel cell, graphene battery is formed.
3. pure electronic flight automobile according to claim 1, is characterized in that: by being fixed on, the portal frame type X-Y two dimension line slideway electric drive part arranged bottom the tubulose control stick (12) of wing central shaft and tubulose control stick is bonded the electronic control system of wing.
4. pure electronic flight automobile according to claim 1 or 3, it is characterized in that: electric drive part Y guide rail (7) of portal frame type X-Y two dimension line slideway electric drive part arranges Y-direction drive motor, the X guide rail 11 being arranged in Y guide rail is driven to move along Y guide rail, electric drive part X guide rail arranges X to drive motor, tubulose joystick driver car (9) being arranged on X guide rail is driven to move along X guide rail, tubulose joystick driver car (9) arranges spherical chamber (50), spherical chamber is covered by the spherical chamber seat in spherical chamber upper cover (53) on top Yu bottom and forms, and it is fastening by screw (54) and pull bar, the outside universal spherical sleeve pipe (51) opening through circular hole for globosity is inner is placed in spherical chamber, tubulose control stick (12) is through universal spherical sleeve pipe (51).
5. pure electronic flight automobile according to claim 1 or 2 or 3, it is characterized in that: the front portion of pure electronic flight automobile arranges wing front overhang hanger (3) backward, wing front overhang hanger (3) is two, left and right bracing frame formation, rear portion arranges hanger bracket (19) after single root or double joint wing forward, front overhang hanger (3) and rear hanger bracket (19) are bonded wing hanger bracket, wing hanger bracket top arranges hinge suspension ring (17), wing hanger bracket is installed and is connected by single hole hinge axis between wing (16), wing and wing hanger bracket; The water screw (22) of flight electromobile, engine (31) are arranged on the fixing support of engine at vehicle body rear portion on (25).
6. by the pure electronic flight 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 permanent seat (45) both sides also have folding axis hole, middle part and the wing girder (15) of permanent seat (45) are fastening, folding shaft (42) is arranged on folding axis hole, folding wings leading edge skeleton (14) of the right and left can be rotated around folding shaft (42), wing leading edge skeleton (14) front portion arranges nut permanent seat (38), the outer wall upper and lower of nut (40) is provided with rotating shaft, nut rotating shaft is arranged on the inner position up and down of nut permanent seat (38), folding electric machine (43) one end and folding electric machine rotary seat (41) are fastening, folding electric machine rotary seat (41) bottom is provided with rotating shaft, the rotating shaft of folding electric machine rotary seat is arranged on folding electric machine permanent seat (44), folding electric machine (43) by folding electric machine rotary seat (41) around axis of rotation, screw mandrel (39) one end is connected with folding electric machine (43) rotor spindle, one end is socketed on nut (40) in addition, the rotor spindle of folding electric machine (43) drives screw mandrel (39) to rotate forward or backwards, Foldable wing leading edge skeleton (14) and wing launch or draw in.
7. by the pure electronic flight automobile described in claim 1 or 2 or 3, it is characterized in that: auxiliary girder shaft seat (48) is fixed on wing leading edge skeleton (14), auxiliary girder (49) is connected by rotating shaft with auxiliary girder shaft seat (48), and can rotate around the axis, auxiliary girder (49) and wing leading edge skeleton (14) form 90 degree of angles of cut or formation is greater than 90 degree or be 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. by the pure electronic flight automobile described in claim 1 or 2 or 3, it is characterized in that: the flexible part of the hydraulic ram that the automatic expansion of folded wing and automatic gathering mechanism are driven by electric motor forms or actuator is made up of cylinder.
9. by the pure electronic flight automobile described in claim 1 or 2 or 3, it is characterized in that: tubulose control stick (12) lower end is provided with crossbeam (30), in the left and right sides of crossbeam (30), and being provided with the flexible pull bar (13) of leading edge skeleton (14) for reinforcing wing between wing leading edge skeleton (14), the vehicle body of pure electronic flight automobile is that open design or totally enclosed frame structure or semiclosed containment structure are formed.
10. by the pure electronic flight automobile described in claim 1 or 2 or 3, it is characterized in that: establishing on pure electronic flight automobile and increase journey fuel electric generator, top or the front portion of pure electronic flight automobile can arrange first aid ejection parachute.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201520891374.7U CN205273074U (en) | 2015-11-10 | 2015-11-10 | Electricelectric moves hovercar |
Applications Claiming Priority (1)
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CN201520891374.7U CN205273074U (en) | 2015-11-10 | 2015-11-10 | Electricelectric moves hovercar |
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CN205273074U true CN205273074U (en) | 2016-06-01 |
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CN201520891374.7U Expired - Fee Related CN205273074U (en) | 2015-11-10 | 2015-11-10 | Electricelectric moves hovercar |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106218333A (en) * | 2015-11-10 | 2016-12-14 | 刘思佳 | Pure electronic hovercar |
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 |
-
2015
- 2015-11-10 CN CN201520891374.7U patent/CN205273074U/en not_active Expired - Fee Related
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106218333A (en) * | 2015-11-10 | 2016-12-14 | 刘思佳 | Pure electronic hovercar |
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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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: 20160601 Termination date: 20201110 |
|
CF01 | Termination of patent right due to non-payment of annual fee |