CN107471936A - Hovercar - Google Patents
Hovercar Download PDFInfo
- Publication number
- CN107471936A CN107471936A CN201710860776.4A CN201710860776A CN107471936A CN 107471936 A CN107471936 A CN 107471936A CN 201710860776 A CN201710860776 A CN 201710860776A CN 107471936 A CN107471936 A CN 107471936A
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- Prior art keywords
- auxiliary
- shaft
- main wing
- car body
- control cabinet
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
- B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
Abstract
The present invention proposes a kind of hovercar, including car body, control cabinet and battery pack are provided with car body, the bottom of car body is provided with power wheel and miniature turbofan generator, four culvert type wind energy conversion systems are respectively provided with car body, culvert type wind-force motor spindle is provided with adjustable air outlet, auxiliary control cabinet is provided with the top of car body, auxiliary control cabinet is provided with folding wing, turbofan generator is provided with the top of auxiliary control cabinet, each folding wing includes main wing and aileron, auxiliary control cabinet is connected with main wing, main wing is connected by rotating control assembly with aileron, the telescopic protection frame of circular arc is provided between two main wings, filling capsule is provided with telescopic protection frame, folding wing is effectively protected.Reliable and stable, service life the advantages of being protected when hovercar of the present invention also has stabilization rational in infrastructure, simple to operate, easily controllable, operation.
Description
Technical field
The present invention relates to automotive field, more particularly to hovercar.
Background technology
With the development of society, hovercar has been appeared in the visual field of people, current hovercar is usually to install
Fixed wing, when hovercar is travelling on highway, space-consuming is big, and wing can be to traveling of the hovercar on highway
When stability impact；There are some hovercars using two rotatable wings in top, meeting between two wings
The breach of V-arrangement is formed, in hovercar flight, wind-force can be acted directly on wing, and the service life of wing cannot protect
Barrier；The wing that is rotatable or folding of also some hovercars is arranged in the bottom plate of hovercar, can so reduce flight
The chassis height of automobile, influence traveling of the hovercar on highway.
The content of the invention
It is an object of the invention to provide a kind of hovercar, solves above-mentioned prior art problem.
The present invention proposes a kind of hovercar, including car body, and control cabinet and battery pack are provided with car body, described
The bottom of car body is provided with four power wheels and a miniature turbofan generator, is respectively provided with four angles of the car body
One culvert type wind energy conversion system, the culvert type wind-force motor spindle are provided with adjustable air outlet, can adjust air outlet and contain for controlling
The size of road formula wind energy conversion system air outlet, the car body top are provided with auxiliary control cabinet, and auxiliary control cabinet can provided with two
Folded wing, the auxiliary control cabinet top are provided with turbofan generator, and each folding wing includes a main wing and one
Individual aileron, the auxiliary control cabinet are connected with main wing, and the main wing is connected by rotating control assembly with aileron, two masters
The telescopic protection frame of circular arc is provided between the wing, filling capsule is provided with telescopic protection frame.
Wherein, the miniature turbofan generator is located on the center between four power wheels, the turbofan generator
It is located on the centre position between four culvert type wind energy conversion systems, miniature turbofan generator and turbofan generator pass through charging device
It is connected with battery pack.
Wherein, four power wheels are divided into two preceding power wheels and two rear power wheels, two preceding power wheels it
Between, between two rear power wheels be equipped with connecting shaft, each power wheel includes motor, wheel hub and tire, the electricity
Motivation connects connection assist by rotating shaft, and connection assist connects wheel hub by more spokes, and the wheel hub is provided with tire.
Further, the spoke is uniformly distributed between connection assist and wheel hub.
Wherein, the filling capsule is filled using gas, and the one end for filling capsule is connected with two-way air pump, by filling gas
Body enhancing, which expands, fills intracapsular volume of air, reaches filling telescopic protection frame, pressure in enhancing telescopic protection frame
Purpose.
Wherein, auxiliary motor and power transmission mechanism, the power transmission mechanism bag are provided with the auxiliary control cabinet
Including an auxiliary driven shaft and two asessory shafts, the auxiliary motor are provided with reversing box, reversing box is provided with driving shaft,
Toothed disc is equipped with driving shaft, auxiliary driven shaft and asessory shaft, toothed disc and auxiliary on one of them described asessory shaft
Toothed disc on driven shaft is meshed, and the toothed disc on another described asessory shaft is meshed with the toothed disc on driving shaft, institute
The toothed disc stated on auxiliary driven shaft is meshed with the toothed disc on driving shaft, and the toothed disc on the asessory shaft connects with main wing
Connect, asessory shaft corresponds with folding wing.
Wherein, the rotating control assembly includes electric rotating motivation, auxiliary reversing box, rotary shaft, rotation gear, driven tooth
Wheel and driven shaft, the driven gear be connected with aileron, the driven gear is enclosed on driven shaft, the electric rotating motivation and
Aid in reversing box connection, the auxiliary reversing box is provided with rotary shaft, and rotary shaft is provided with rotation gear, the rotation gear and
Driven gear is meshed.
Wherein, first hydraulic cylinder and second hydraulic cylinder, the first hydraulic cylinder and the first hydraulic press are provided with the main wing
Connection, the first hydraulic cylinder are provided with the first expansion link, and the second hydraulic cylinder is connected with the second hydraulic press, second liquid
Cylinder pressure is provided with the second expansion link, is provided with the first via hole and the second via hole in the aileron, first via hole it is big
Small shape and position are corresponding with the size shape of the first expansion link and position, the size shape of second via hole with
And position is corresponding with the size shape of the second expansion link and position.First expansion link and the second expansion link are used to strengthen
Bonding strength between main wing and aileron, the further service life for strengthening folding wing.
Wherein, the car body is provided with outside track groove and inner orbit groove, the thickness and inner orbit of the outside track groove
The thickness of groove is equal, and outside track groove and inner orbit groove are respectively provided on two different concentric circles of diameter, the outside track groove
Both ends and the both ends of inner orbit groove are respectively provided with a fixed block, fixed block bottom connection hydraulic means, and hydraulic means is located at automobile
In main body, fixed block can be controlled to lift using hydraulic means, the bottom of the main wing is provided with two auxiliary sliding shoes, and two auxiliary
Help the position of sliding shoe corresponding with the position of outside track groove and inner orbit groove respectively, two auxiliary sliding shoes pass through auxiliary
Contiguous block is connected with main wing, and two auxiliary sliding shoes are each passed through the housing of main wing and outside track groove and inner orbit groove connect
Connect.
Wherein, the hovercar has two kinds of operational modes to be respectively：Its road-driving mode and offline mode.
A kind of the advantages of hovercar of the present invention is：Stabilization rational in infrastructure, easy to operate, easily controllable, function
Practicality, reliable and stable during operation, folding wing is small on being influenceed caused by the traveling of hovercar during its road-driving mode, can roll over
Folded wing is effectively protected, and the service life of hovercar of the present invention has also obtained effective guarantee.
Brief description of the drawings
Fig. 1 is front view of the hovercar in its road-driving mode in one embodiment of the present invention；
Fig. 2 is the enlarged drawing of A-a parts in Fig. 1；
Fig. 3 is top view of the hovercar in its road-driving mode in one embodiment of the present invention；
Fig. 4 is top view of the hovercar in offline mode in one embodiment of the present invention；
Fig. 5 is the cross-sectional view of folding wing in one embodiment of the present invention；
Fig. 6 is the structural representation of power transmission mechanism in one embodiment of the present invention；
Fig. 7 is upward view of the hovercar in its road-driving mode in one embodiment of the present invention；
Fig. 8 is the front view of power wheel in one embodiment of the present invention.
Embodiment
As shown in Figures 1 to 8, the present invention proposes a kind of hovercar, including car body 1, and control is provided with car body 1
Case processed and battery pack, the bottom of the car body 1 are provided with four power wheels 13 and a miniature turbofan generator 14, the vapour
A culvert type wind energy conversion system 12 is respectively provided with four angles of vehicle main body 1, the bottom of culvert type wind energy conversion system 12 is provided with and can adjust out
Air port 15, adjustable air outlet 15 are used for the size for controlling the air outlet of culvert type wind energy conversion system 12, and the top of car body 1 is provided with
Control cabinet is aided in, auxiliary control cabinet is provided with two folding wings, turbofan generator 2 is provided with the top of the auxiliary control cabinet,
Each folding wing includes a main wing 8 and an aileron 3, and the auxiliary control cabinet is connected with main wing 8, the main wing
8 are connected by rotating control assembly with aileron 3, and the telescopic protection frame 6 of circular arc is provided between two main wings 8, can be stretched
Filling capsule is provided with contracting fender bracket 6.
As the preferred of the present embodiment, the miniature turbofan generator 14 is located at the center between four power wheels 13
On, the turbofan generator 2 is located on the centre position between four culvert type wind energy conversion systems 12, can effectively reduce turbofan hair
On influence, the miniature He of turbofan generator 14 caused by the degree of balance of hovercar when motor 2 and miniature turbofan generator 14 work
Turbofan generator 2 is connected by charging device with battery pack, is easy to charge to battery pack.
As the preferred of the present embodiment, four power wheels 13 are divided to for two preceding power wheels and two rear power wheels, and two
Connecting shaft 30 is equipped between the individual preceding power wheel, between two rear power wheels, each power wheel 13 includes motor
29th, wheel hub and tire 32, the motor 29 connect connection assist 28 by rotating shaft, and connection assist 28 passes through more spokes
Bar 31 connects wheel hub, and the wheel hub is provided with tire 32.
As the preferred of the present embodiment, the spoke 31 is uniformly distributed between connection assist 28 and wheel hub.
As the preferred of the present embodiment, it is described filling capsule filled using gas, fill capsule one end be connected with it is two-way
Air pump, strengthen to expand by filling gas and fill intracapsular volume of air, it is scalable to reach filling telescopic protection frame 6, enhancing
The purpose of pressure in fender bracket 6.
As the preferred of the present embodiment, auxiliary motor and power transmission mechanism are provided with the auxiliary control cabinet, it is described
Power transmission mechanism includes an auxiliary driven shaft 17 and two asessory shafts 26, the auxiliary motor are provided with reversing box,
Reversing box is provided with driving shaft 27, toothed disc 11 is equipped with driving shaft 27, auxiliary driven shaft 17 and asessory shaft 26, wherein one
Toothed disc 11 on the individual asessory shaft 26 is meshed with the toothed disc 11 on auxiliary driven shaft 17, another described asessory shaft 26
On toothed disc 11 be meshed with the toothed disc 11 on driving shaft 27, it is described auxiliary driven shaft 17 on toothed disc 11 and driving shaft
Toothed disc 11 on 27 is meshed, and the toothed disc 11 on the asessory shaft 26 is connected with main wing 8, asessory shaft 26 and folding wing
Correspond.
Auxiliary motor can control driving shaft 27 by reversing box, then drive power transmission mechanism by driving shaft 27
The entrance open configuration of two folding wings of control closes up state.
As the preferred of the present embodiment, the rotating control assembly includes electric rotating motivation 21, auxiliary reversing box, rotation
Axle, rotation gear 20, driven gear 19 and driven shaft 18, the driven gear 19 are connected with aileron 3, the driven gear 19
It is enclosed on driven shaft 18, the electric rotating motivation 21 is connected with auxiliary reversing box, and the auxiliary reversing box is provided with rotary shaft, revolves
Rotating shaft is provided with rotation gear 20, and the rotation gear 20 is meshed with driven gear 19.
Using electric rotating motivation 21 control rotary shaft drive rotation gear 20 rotate, then using rotate gear 20 with it is driven
The position relationship that gear 19 is meshed, driven gear 19 is driven to rotate by rotating gear 20, so as to reach drive driven gear
On the purpose that rotates of aileron 3, the direction of rotation of rotating shaft can be changed by reversing box, so as to reach the rotation for changing aileron 3
The purpose in direction.
Auxiliary control cabinet and rotating control assembly in the present embodiment are set using multi-gear, simple in construction, are easy to control
System, easy to maintenance, cost is low.
It is provided with first hydraulic cylinder 24 and second hydraulic cylinder 22 as the preferred of the present embodiment, in the main wing 8, described first
Hydraulic cylinder 24 is connected with the first hydraulic press, and the first hydraulic cylinder 24 is provided with the first expansion link 25, the second hydraulic cylinder 22
It is connected with the second hydraulic press, the second hydraulic cylinder 22 is provided with the second expansion link 23, and the first via hole is provided with the aileron 3
With the second via hole, the size shape and position of the size shape of first via hole and position with the first expansion link 25
Corresponding, the size shape of second via hole and position are relative with the size shape of the second expansion link 23 and position
Should.The expansion link 23 of first expansion link 25 and second is used to strengthen the bonding strength between main wing 8 and aileron 3, further
Strengthen the service life of folding wing.
As the preferred of the present embodiment, the car body 1 is provided with outside track groove 4 and inner orbit groove 7, the outside track
The thickness of groove 4 is equal with the thickness of inner orbit groove 7, and outside track groove 4 and inner orbit groove 7 are respectively provided at different concentric of two diameters
On circle, the both ends of the outside track groove 4 and the both ends of inner orbit groove 7 are respectively provided with a fixed block 5, the bottom of fixed block 5 connection liquid
Pressure device, hydraulic means are located in car body 1, using hydraulic means fixed block 5 can be controlled to lift, the bottom of the main wing 8
Portion is provided with two auxiliary sliding shoes 10, the position position with outside track groove 4 and inner orbit groove 7 respectively of two auxiliary sliding shoes 10
Corresponding, by aiding in contiguous block 9 to be connected with main wing 8, two auxiliary sliding shoes 10 divide two auxiliary sliding shoes 10
Not Chuan Guo the housing of main wing 8 be connected with outside track groove 4 and inner orbit groove 7, auxiliary contiguous block 9 be used to expanding auxiliary sliding shoe 10 with
Connection area between wing 3, will auxiliary contiguous block 9 be arranged in the housing of main wing 8 can effectively reduce traveling process by
The resistance of the wind arrived, sliding shoe 10 and the collective effect of fixed block 5 is aided in aid in fixing main wing 8 so that main wing 8 is in flight vapour
It is more stable during the state of flight of car.
Hovercar described in the present embodiment includes A its road-driving modes：Miniature turbofan generator 14, turbofan generator 2
And four culvert type wind energy conversion systems 12 are in state out of service, the aileron 3 in folding wing is folded on main wing 8,
Two folding wings, which are in, closes up state, directly carries out vehicle drive mode using car body 1；B offline mode：1)
Gliding is taken off pattern, aids in the auxiliary motor in control cabinet to drive driving shaft 27 to rotate, then driving shaft 27 can by its from
Toothed disc 11 with it drives the toothed disc 11 being meshed to rotate so that two folding wings open, and treat two foldable machines
When auxiliary sliding shoe 10 on the wing slides into the top of outside track groove 4 and inner orbit groove 7, auxiliary motor is stopped, hydraulic pressure
Device control fixed block 5 rises to be connected as the bottom of main wing 8, and hydraulic means is stopped, and auxiliary sliding shoe 10 enters fixing shape
State, then electric rotating motivation 21 start working, electric rotating motivation 21 drives the rotation gear 20 in rotary shaft and rotary shaft to rotate,
Rotation gear 20 drives driven gear 19 to rotate, and aileron 3 is rotated down under the drive of driven gear 19, until aileron 3 and master
The wing 8 combines, and electric rotating motivation 21 is stopped with reference to after the completion of, and then the first hydraulic press can be by first hydraulic cylinder 24 by first
Expansion link 25 is pushed into the first via hole, and it is auxiliary that the second expansion link 23 can be pushed into second by the second hydraulic press by second hydraulic cylinder 22
Help in hole, after band push-in completion formation is fixed, the first hydraulic press and the second hydraulic press are stopped, and then motor 29 starts work
Make, motor 29 can drive power wheel 13 to start Accelerating running, provide power-assisted for taking off for hovercar, then culvert type wind-force
Machine 12 is started working, and the rotating speed of culvert type wind energy conversion system 12 gradually strengthens, and hovercar enters gliding under such circumstances
Takeoff phase, after hovercar takes off, motor 29 is stopped, and miniature turbofan generator 14 and turbofan generator 2 start
Work, the turn up of air outlet 15 and culvert type wind energy conversion system 12 can be can adjust by adjusting during hovercar flies
To adjustment direction and the purpose of flying speed；2) take off vertically pattern, aids in the auxiliary motor in control cabinet to drive driving shaft
27 rotate, and then driving shaft 27 can drive the toothed disc 11 being meshed rotate by the toothed disc 11 on its own so that two
Folding wing opens, and treats that the auxiliary sliding shoe 10 on two folding wings slides into the top of outside track groove 4 and inner orbit groove 7
During end, auxiliary motor is stopped, and hydraulic means control fixed block 5 rises to be connected as the bottom of main wing 8, and hydraulic means stops
Work, auxiliary sliding shoe 10 enter stationary state, and then electric rotating motivation 21 is started working, and electric rotating motivation 21 drives rotary shaft
Rotated with the rotation gear 20 in rotary shaft, rotation gear 20 drives driven gear 19 to rotate, band of the aileron 3 in driven gear 19
It is rotated down under dynamic, until aileron 3 is combined with main wing 8, electric rotating motivation 21 is stopped with reference to after the completion of, then the first hydraulic pressure
First expansion link 25 is pushed into the first via hole by chance by first hydraulic cylinder 24, and the second hydraulic press can pass through second hydraulic cylinder
22 are pushed into the second expansion link 23 in second via hole, after band push-in completion formation is fixed, the first hydraulic press and the second hydraulic press
It is stopped, then culvert type wind energy conversion system 12, miniature turbofan generator 14 and turbofan generator 2 are started working, and culvert type wind
The rotating speed of power machine 12 gradually strengthens, and hovercar enters and taken off vertically the stage under such circumstances, and hovercar takes off
Adjustment direction and the mesh of flying speed can be reached by adjusting the rotating speed of adjustable air outlet 15 and culvert type wind energy conversion system 12 afterwards
's.
The stabilization rational in infrastructure of the hovercar, easy to operate, practical function is reliable and stable during operation, on hovercar
Folding wing be able to can also be closed to after main wing 8 folds between aileron 3 together with, space-consuming is few, reduces
Resistance of the folding wing in its road-driving mode, telescopic protection frame 6, and scalable guarantor are set between two main wings 8
Filling capsule is provided with retaining frame 6, wind-force directly acts on shape between two main wings 8 when can effectively avoid hovercar flight
Into V-shaped part in phenomenon, further protection main wing 8 so that the service life of main wing 8 is protected, so as to further
The service life that ensure that hovercar.
Described above is only the preferred embodiment of the present invention, it is noted that to those skilled in the art, not
On the premise of departing from the invention design, some similar modification and improvement can also be made, these also should be regarded as the present invention
Protection domain within.
Claims (8)
1. a kind of hovercar, it is characterised in that including car body (1), control cabinet and battery are provided with car body (1)
Group, the bottom of the car body (1) are provided with four power wheels (13) and a miniature turbofan generator (14), the automobile primary
A culvert type wind energy conversion system (12) is respectively provided with four angles of body (1), culvert type wind energy conversion system (12) bottom is provided with adjustable
Air outlet (15), car body (1) top are provided with auxiliary control cabinet, and auxiliary control cabinet is provided with two folding wings,
Turbofan generator (2) is provided with the top of the auxiliary control cabinet, each folding wing includes a main wing (8) and a pair
The wing (3), the auxiliary control cabinet are connected with main wing (8), and the main wing (8) is connected by rotating control assembly with aileron (3), and two
The telescopic protection frame (6) of circular arc is provided between the individual main wing (8), filling capsule is provided with telescopic protection frame (6).
2. hovercar according to claim 1, it is characterised in that the miniature turbofan generator (14) is located at four and moved
On center between wheels (13), the turbofan generator (2) is located at the centre between four culvert type wind energy conversion systems (12)
On position, the miniature turbofan generator (14) and turbofan generator (2) are connected by charging device with battery pack.
3. hovercar according to claim 1, it is characterised in that four power wheels (13) are divided into two preceding power
Wheel and two rear power wheels, connecting shaft (30), Mei Gesuo are equipped between two preceding power wheels, between two rear power wheels
Stating power wheel (13) includes motor (29), wheel hub and tire (32), and the motor (29) connects auxiliary by rotating shaft and connected
Fitting (28), connection assist (28) connect wheel hub by more spokes (31), and the wheel hub is provided with tire (32).
4. hovercar according to claim 1, it is characterised in that the filling capsule is filled using gas, described
One end of filling capsule is connected with two-way air pump.
5. hovercar according to claim 1, it is characterised in that it is described auxiliary control cabinet in be provided with auxiliary motor and
Power transmission mechanism, the power transmission mechanism includes an auxiliary driven shaft (17) and two asessory shafts (26), described auxiliary
Motor is helped to be provided with reversing box, reversing box is provided with driving shaft (27), driving shaft (27), auxiliary driven shaft (17) and auxiliary
Toothed disc (11) is equipped with axle (26), the toothed disc (11) on one of them described asessory shaft (26) and auxiliary driven shaft (17)
On toothed disc (11) be meshed, the toothed disc on the toothed disc (11) on another described asessory shaft (26) and driving shaft (27)
(11) it is meshed, the toothed disc (11) on the auxiliary driven shaft (17) is meshed with the toothed disc (11) on driving shaft (27),
Toothed disc (11) on the asessory shaft (26) is connected with main wing (8), and asessory shaft (26) corresponds with folding wing.
6. hovercar according to claim 1, it is characterised in that the rotating control assembly includes electric rotating motivation
(21) reversing box, rotary shaft, rotation gear (20), driven gear (19) and driven shaft (18), the driven gear, are aided in
(19) it is connected with aileron (3), the driven gear (19) is enclosed on driven shaft (18), and the electric rotating motivation (21) is changed with auxiliary
Connected to case, the auxiliary reversing box is provided with rotary shaft, and rotary shaft is provided with rotation gear (20), the rotation gear (20)
It is meshed with driven gear (19).
7. hovercar according to claim 1, it is characterised in that be provided with first hydraulic cylinder (24) in the main wing (8)
With second hydraulic cylinder (22), the first hydraulic cylinder (24) is connected with the first hydraulic press, and the first hydraulic cylinder (24) is provided with
First expansion link (25), the second hydraulic cylinder (22) are connected with the second hydraulic press, and the second hydraulic cylinder (22) is provided with the
Two expansion links (23), the aileron (3) is interior to be provided with the first via hole and the second via hole, the size shape of first via hole
And position is corresponding with the size shape of the first expansion link (25) and position, the size shape of second via hole and
Position is corresponding with the size shape of the second expansion link (23) and position.
8. hovercar according to claim 1, it is characterised in that the car body (1) is provided with outside track groove (4)
With inner orbit groove (7), the thickness of the outside track groove (4) is equal with the thickness of inner orbit groove (7), outside track groove (4) and interior rail
Road groove (7) is respectively provided on two different concentric circles of diameter, the both ends of the outside track groove (4) and the two of inner orbit groove (7)
End is respectively provided with a fixed block (5), fixed block (5) bottom connection hydraulic means, and hydraulic means is located in car body (1), profit
With hydraulic means fixed block (5) can be controlled to lift, the bottom of the main wing (8) is provided with two auxiliary sliding shoes (10), two
Aid in the position of sliding shoe (10) corresponding with the position of outside track groove (4) and inner orbit groove (7) respectively, two auxiliary are slided
For motion block (10) by aiding in contiguous block (9) to be connected with main wing (8), two auxiliary sliding shoes (10) are each passed through main wing (8)
Housing be connected with outside track groove (4) and inner orbit groove (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710860776.4A CN107471936A (en) | 2017-09-21 | 2017-09-21 | Hovercar |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710860776.4A CN107471936A (en) | 2017-09-21 | 2017-09-21 | Hovercar |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107471936A true CN107471936A (en) | 2017-12-15 |
Family
ID=60587280
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710860776.4A Withdrawn CN107471936A (en) | 2017-09-21 | 2017-09-21 | Hovercar |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107471936A (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102673787A (en) * | 2012-04-24 | 2012-09-19 | 北京航空航天大学 | Small-sized combined type air vehicle adopting layout combining disk swing with variable wings and airbag |
| CN103496305A (en) * | 2012-04-24 | 2014-01-08 | 赵辉 | Hovercar |
| US20150102155A1 (en) * | 2012-06-07 | 2015-04-16 | Ivan Krastev | Road-and-air transport vehicle |
| CN105711811A (en) * | 2016-01-27 | 2016-06-29 | 北京航空航天大学 | Wing folding mechanism |
| CN105799911A (en) * | 2016-05-10 | 2016-07-27 | 仲松梅 | Folding-wing unmanned plane for energy-saving and environment-friendly constructional engineering |
| CN106240800A (en) * | 2016-08-17 | 2016-12-21 | 四川精诚至强科技有限公司 | A kind of unmanned plane folding wing |
| CN205854477U (en) * | 2016-07-22 | 2017-01-04 | 中国人民解放军火箭军工程大学 | The fold type folding wing after a kind of rotation |
| CN106827993A (en) * | 2017-03-28 | 2017-06-13 | 刘宾 | A kind of four culvert vertical take-off and landing hovercars |
-
2017
- 2017-09-21 CN CN201710860776.4A patent/CN107471936A/en not_active Withdrawn
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102673787A (en) * | 2012-04-24 | 2012-09-19 | 北京航空航天大学 | Small-sized combined type air vehicle adopting layout combining disk swing with variable wings and airbag |
| CN103496305A (en) * | 2012-04-24 | 2014-01-08 | 赵辉 | Hovercar |
| US20150102155A1 (en) * | 2012-06-07 | 2015-04-16 | Ivan Krastev | Road-and-air transport vehicle |
| CN105711811A (en) * | 2016-01-27 | 2016-06-29 | 北京航空航天大学 | Wing folding mechanism |
| CN105799911A (en) * | 2016-05-10 | 2016-07-27 | 仲松梅 | Folding-wing unmanned plane for energy-saving and environment-friendly constructional engineering |
| CN205854477U (en) * | 2016-07-22 | 2017-01-04 | 中国人民解放军火箭军工程大学 | The fold type folding wing after a kind of rotation |
| CN106240800A (en) * | 2016-08-17 | 2016-12-21 | 四川精诚至强科技有限公司 | A kind of unmanned plane folding wing |
| CN106827993A (en) * | 2017-03-28 | 2017-06-13 | 刘宾 | A kind of four culvert vertical take-off and landing hovercars |
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Application publication date: 20171215 |
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