CN108944306A - Automobile aerocraft - Google Patents
Automobile aerocraft Download PDFInfo
- Publication number
- CN108944306A CN108944306A CN201810726455.XA CN201810726455A CN108944306A CN 108944306 A CN108944306 A CN 108944306A CN 201810726455 A CN201810726455 A CN 201810726455A CN 108944306 A CN108944306 A CN 108944306A
- Authority
- CN
- China
- Prior art keywords
- vehicle body
- wing
- rotor
- parachute
- rotor mechanism
- 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.)
- Pending
Links
- 230000000712 assembly Effects 0.000 claims description 2
- 238000000429 assembly Methods 0.000 claims description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000004888 barrier function Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
Classifications
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/56—Folding or collapsing to reduce overall dimensions of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D17/00—Parachutes
- B64D17/80—Parachutes in association with aircraft, e.g. for braking thereof
Abstract
The present invention relates to technical field of transportation means, more particularly, to a kind of automobile aerocraft.It include: vehicle body, wing, power device and avoiding device；The two sides of the vehicle body are collapsibly provided with the wing, and the avoiding device is arranged on the vehicle body；The power device includes the first rotor mechanism being arranged on the wing, and the wing is arranged in close to the side of the vehicle body in first rotor mechanism.To alleviate festivals or holidays traffic jam existing in the prior art, inconvenient technical problem of going on a journey.
Description
Technical field
The present invention relates to technical field of transportation means, more particularly, to a kind of automobile aerocraft.
Background technique
Currently, as the improvement of people's living standards, the incrementss of automobile increase year by year, especially in peak period on and off duty
Or festivals or holidays etc., the phenomenon that traffic jam caused by road is crowded is increasingly severe, traffic congestion, is frequent occurrence.
And many people can choose seating subway or public transport when on and off duty, but in festivals or holidays trip
When, traffic jam is often very serious, brings many troubles to people's trip.
Summary of the invention
The purpose of the present invention is to provide automobile aerocrafts, to alleviate festivals or holidays traffic jam existing in the prior art,
The inconvenient technical problem of trip.
A kind of automobile aerocraft provided by the invention, comprising: vehicle body, wing, power device and avoiding device；
The two sides of the vehicle body are collapsibly provided with the wing, and the avoiding device is arranged on the vehicle body；
The power device includes the first rotor mechanism being arranged on the wing, and the first rotor mechanism setting exists
The wing is close to the side of the vehicle body.
Further, the power device further includes preceding rotor mechanism, rear rotor mechanism and vertical rotor mechanism；
The front end of the vehicle body is arranged in the preceding rotor mechanism, after the vehicle body is arranged in the rear rotor mechanism
Lower end is arranged in the middle part of the vehicle body in end, the vertical rotor mechanism.
Further, the vertical rotor mechanism includes multiple vertical rotors, is provided in the middle part of the lower end of the vehicle body more
A mounting groove；
Multiple institute's mounting grooves are arranged in a one-to-one correspondence with multiple vertical rotors, and are provided in the mounting groove flexible
Part, the center axis connection of the extensible member and the vertical rotor；When the extensible member is shunk, the vertical rotor is contained in
In the mounting groove.
Further, multiple vertical rotors are evenly distributed in the middle part of the vehicle body lower end.
Further, the avoiding device includes four parachutes dress that the vehicle body two sides and head and the tail both ends are arranged in
It sets.
Further, the parachute assembly includes ejection mechanism, trigger mechanism and parachute；
The receiving storehouse for accommodating the parachute and the ejection mechanism is provided on the vehicle body；The receiving storehouse
Opening is provided with cover board, and the cover board is for covering or exposing the opening；
The ejection mechanism is connect with the parachute and the trigger mechanism respectively；The trigger mechanism is for controlling institute
It is mobile to expose opening to state cover board, and controls the ejection mechanism and the parachute is removed into the receiving storehouse.
Further, the installing port for installing the first rotor mechanism is provided on the wing, and on the installing port
It is provided with blinds window cover.
Further, it is additionally provided with the controller for controlling the blinds window cover opening and closing in the vehicle body and executes machine
Structure；
The executing agency connect with the blinds window cover, and the controller controls executing agency's work, so that
The blinds window cover is closed or is opened.
Further, there are three wheels for setting on the vehicle body.
Further, there are four wheels for setting on the vehicle body.
Automobile aerocraft provided by the invention, comprising: vehicle body, wing, power device and avoiding device；The two of the vehicle body
Side is collapsibly provided with the wing, and the avoiding device is arranged on the vehicle body；The power device includes setting
The wing is arranged in close to the side of the vehicle body in the first rotor mechanism on the wing, first rotor mechanism.
Using above-mentioned scheme, by being provided with wing on vehicle body, wing can be folded relative to vehicle body, while be arranged on wing
There is the first rotor mechanism, the first rotor mechanism takes off for vehicle body and provides power, and avoiding device is provided on vehicle body, works as automobile
When power is unbalance in the sky, the safety of vapour occupant can be ensured as far as possible, since vehicle is collapsibly arranged in wing
The two sides of body can also be such that vehicle body normally travels on road surface, to alleviate festivals or holidays traffic jam existing in the prior art, out
The inconvenient technical problem of row.
Detailed description of the invention
It, below will be to specific in order to illustrate more clearly of the specific embodiment of the invention or technical solution in the prior art
Embodiment or attached drawing needed to be used in the description of the prior art be briefly described, it should be apparent that, it is described below
Attached drawing is some embodiments of the present invention, for those of ordinary skill in the art, before not making the creative labor
It puts, is also possible to obtain other drawings based on these drawings.
Fig. 1 is top view when automobile aerocraft avoiding device provided in an embodiment of the present invention starts；
Fig. 2 is bottom view when automobile aerocraft vertical rotor provided in an embodiment of the present invention mechanism starts；
Fig. 3 is the partial schematic diagram of automobile aerocraft provided in an embodiment of the present invention；
Fig. 4 is top view when automobile aerocraft device avoiding device provided in an embodiment of the present invention is inactive.
Icon: 1- vehicle body；2- wing；3- avoiding device；The first rotor mechanism of 4-；Rotor mechanism before 5-；Gyroplane after 6-
Structure；7- vertical rotor mechanism；8- mounting groove；9- blinds window cover；201- installing port；701- vertical rotor；702- extensible member.
Specific embodiment
Technical solution of the present invention is clearly and completely described below in conjunction with attached drawing, it is clear that described implementation
Example is a part of the embodiment of the present invention, instead of all the embodiments.Based on the embodiments of the present invention, ordinary skill
Personnel's every other embodiment obtained without making creative work, shall fall within the protection scope of the present invention.
In the description of the present invention, it should be noted that such as occur term " center ", "upper", "lower", "left", "right",
"vertical", "horizontal", "inner", "outside" etc., indicated by orientation or positional relationship be orientation based on the figure or position
Relationship is merely for convenience of description of the present invention and simplification of the description, rather than the device or element of indication or suggestion meaning must have
There is specific orientation, be constructed and operated in a specific orientation, therefore is not considered as limiting the invention.In addition, as occurred
Term " first ", " second ", " third " are used for descriptive purposes only and cannot be understood as indicating or suggesting relative importance.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " peace such as occur
Dress ", " connected ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or integrally
Connection；It can be mechanical connection, be also possible to be electrically connected；Can be directly connected, can also indirectly connected through an intermediary,
It can be the connection inside two elements.For the ordinary skill in the art, above-mentioned art can be understood with concrete condition
The concrete meaning of language in the present invention.
Fig. 1 is top view when automobile aerocraft avoiding device provided in an embodiment of the present invention starts.As shown in Figure 1, this
Invent a kind of automobile aerocraft provided, comprising: vehicle body 1, wing 2, power device and avoiding device 3；
The two sides of the vehicle body 1 are collapsibly provided with the wing 2, and the avoiding device 3 is arranged in the vehicle body 1
On；
The power device includes the first rotor mechanism 4 being arranged on the wing 2, and first rotor mechanism 4 is set
It sets in the wing 2 close to the side of the vehicle body 1.
Wherein, the angle that wing 2 is folded relative to vehicle body 1 can be 90 °.
The two sides at 1 middle part of vehicle body are arranged in wing 2, can enable automobile aerocraft more steady in flight in this way.
Automobile aerocraft provided by the invention, comprising: vehicle body 1, wing 2, power device and avoiding device 3；The vehicle body 1
Two sides be collapsibly provided with the wing 2, the avoiding device 3 is arranged on the vehicle body 1；The power device packet
The first rotor mechanism 4 being arranged on the wing 2 is included, first rotor mechanism 4 is arranged in the wing 2 close to the vehicle
The side of body 1.Using above-mentioned scheme, by being provided with wing 2 on vehicle body 1, wing 2 can be folded relative to vehicle body 1, together
When be provided with the first rotor mechanism 4 on wing 2, the first rotor mechanism 4 is that vehicle body 1 takes off and provides power, and sets on vehicle body 1
Avoiding device 3 has been set, when power is unbalance in the sky for automobile, can ensure the safety of vapour occupant as far as possible, due to
The two sides of vehicle body 1 are collapsibly arranged in wing 2, and vehicle body 1 can also be made normally to travel on road surface, to alleviate in the prior art
Existing festivals or holidays traffic jam, inconvenient technical problem of going on a journey.
Fig. 2 is bottom view when automobile aerocraft vertical rotor provided in an embodiment of the present invention mechanism starts；Fig. 3 is this hair
The partial schematic diagram for the automobile aerocraft that bright embodiment provides.As shown in Figures 2 and 3, on the basis of the above embodiments, further
Ground, the power device further include preceding rotor mechanism 5, rear rotor mechanism 6 and vertical rotor mechanism 7；
The front end of the vehicle body 1 is arranged in the preceding rotor mechanism 5, and the vehicle body 1 is arranged in the rear rotor mechanism 6
Rear end, the vertical rotor mechanism 7 are arranged in the 1 middle part lower end of vehicle body.
Wherein, preceding rotor mechanism 5 includes preceding rotor and front driving device, the power output shaft of front driving device and preceding rotor
Center axis connection, the power output shaft rotation of front driving device is with the central axis rotation of 2 rotor of wing before driving, to drive
Preceding 2 rotor rotational of wing.Rotor mechanism 6 includes rear rotor and rear drive equipment afterwards, and the power output shaft of rear drive equipment is with after
The center axis connection of rotor, the power output shaft of rear drive equipment rotates the central axis rotation to drive 2 rotor of wing, thus band
2 rotor rotational of wing after dynamic.
In the present embodiment, the setting of preceding rotor mechanism 5, rear rotor mechanism 6 and vertical rotor mechanism 7 can make vehicle body 1 exist
There is enough power when needing to take off, and vehicle body 1 can make vertical raising when raising, so as to reduce
Requirement to runway.
On the basis of the above embodiments, further, the vertical rotor mechanism 7 includes multiple vertical rotors 701, institute
It states and is provided with multiple mounting grooves 8 in the middle part of the lower end of vehicle body 1；
Multiple institute's mounting grooves 8 are arranged in a one-to-one correspondence with multiple vertical rotors 701, and are arranged in the mounting groove 8
There are extensible member 702, the center axis connection of the extensible member 702 and the vertical rotor 701；When the extensible member 702 is shunk,
The vertical rotor 701 is contained in the mounting groove 8.
Wherein, vertical rotor mechanism 7 includes vertical rotor 701 and vertical drive, and the power of vertical drive is defeated
The power output shaft of the center axis connection of shaft and vertical rotor 701, vertical drive is rotated to drive vertical rotor 701
Central axis rotation, so that vertical rotor 701 be driven to rotate.
Wherein, extensible member 702 can be telescopic rod.In use, when automobile aerocraft needs raising, user
Telescopic rod is extended, so that vertical rotor 701 be enabled to stretch out mounting groove 8；When automobile aerocraft needs to land, user will stretch
Bar shortens, so that vertical rotor 701 be enabled to withdraw in mounting groove 8.
When vertical rotor 701 is multiple, extensible member 702 further includes connection frame, connection frame respectively with multiple vertical rotors
701 connections, telescopic rod are connect to drive connection frame flexible with connection frame, and the setting of connection frame can enable multiple vertical rotors 701
Synchronizing moving.
In the present embodiment, in use, when automobile aerocraft needs raising, user extends extensible member 702,
It is rotated to enable vertical rotor 701 stretch out mounting groove 8, when automobile aerocraft needs to land, user is by extensible member 702
Shorten, so that vertical rotor 701 be enabled to withdraw in mounting groove 8.When automobile aerocraft on the ground when driving, due to the barrier on ground
Hinder object more, may collide with and be damaged to vertical rotor 701, it is vertical that the setting of extensible member 702 and mounting groove 8 can play protection
The effect of rotor 701.
On the basis of the above embodiments, further, multiple vertical rotors 701 are evenly distributed on the vehicle body 1
In the middle part of lower end.
Wherein, multiple vertical rotors 701 are spaced setting in same level.
Multiple vertical rotors 701 can be arranged along the length extending direction interval of vehicle body 1, or prolong along the width of vehicle body 1
Stretch the setting of direction interval.
In the present embodiment, multiple settings can further increase vertical raising power, enable the speed of automobile aerocraft raising
Degree is faster, more efficient.
On the basis of the above embodiments, further, the avoiding device 3 include setting in 1 two sides of vehicle body and
Four parachute assemblies at head and the tail both ends.
In the present embodiment, it is respectively arranged with parachute assembly in the head and the tail of vehicle body 1 and side,
On the basis of the above embodiments, further, the parachute assembly include ejection mechanism, trigger mechanism and
Parachute；
The receiving storehouse for accommodating the parachute and the ejection mechanism is provided on the vehicle body 1；The receiving storehouse
Opening be provided with cover board, the cover board is for covering or exposing the opening；
The ejection mechanism is connect with the parachute and the trigger mechanism respectively；The trigger mechanism is for controlling institute
It is mobile to expose opening to state cover board, and controls the ejection mechanism and the parachute is removed into the receiving storehouse.
Wherein, the middle part of 1 side of vehicle body should be arranged in opening, in this way when two parachutes pop up, can enable vehicle body 1 more
Add stabilization.
The two sides of vehicle body 1 are also relatively set with wing 2, and opening should be arranged in the top of wing 2, work as parachute assembly in this way
When starting, parachute will not generate interference, the damage for preventing wing 2 and parachute from being impacted by the two with wing 2.
Ejection mechanism may include cylinder and push rod, and push rod is arranged between cylinder and parachute, trigger mechanism and cylinder
Connection.In use, user controls cover board by trigger mechanism and opens to expose opening, then controls cylinder drive and pushes away
Bar, which releases parachute, accommodates storehouse, and the movement of parachute relative atmospheric is inflating expanded, to slow down 1 lapse rate of vehicle body.
In the present embodiment, in automobile aerocraft normally travel or flight, parachute is located in accommodating storehouse；Work as automobile
When aircraft is fallen at high speeds, user controls cover board movement by operation trigger mechanism and is open with exposing, then trigger mechanism
It controls ejection mechanism and removes parachute and accommodate storehouse, the movement of parachute relative atmospheric is inflating expanded, drops speed to slow down vehicle body 1
Degree, and then improve the safety of automobile aerocraft.The setting for accommodating storehouse and cover board can be played the role of protecting parachute, and
Can also prevent parachute without using when error starting, hinder automobile aerocraft normal use.
Fig. 4 is top view when automobile aerocraft device avoiding device provided in an embodiment of the present invention is inactive.Such as Fig. 4 institute
Show, on the basis of the above embodiments, further, the installation for installing the first rotor mechanism 4 is provided on the wing 2
Mouth 201, and blinds window cover 9 is provided on the installing port 201.
Wherein, the quantity of installing port 201 can be two either three, and be provided with first in each installing port 201
The lift of wing 2 can be improved in rotor mechanism 4 in this way, vehicle body 1 can be made quickly to go up to the air, additionally it is possible to improve vehicle body 1 and fly
Security performance in the process.
In the present embodiment, the installing port 201 of the first rotor mechanism 4 of installation is provided on wing 2, and in installing port 201
Upper and lower opening end is provided with blinds window cover 9, and blinds window cover 9 is the state closed when wing 2 is in folding state, works as vapour
When vehicle needs to go up to the air, blinds window cover 9 is in the state opened, at this point, the rotor mechanism being arranged in installing port 201 starts work
Make, by the setting of blinds window cover 9, rotor mechanism can be protected, improve the service life of rotor mechanism.
On the basis of the above embodiments, further, it is additionally provided in the vehicle body 1 for controlling the blinds window cover
The controller and executing agency that plate 9 is opened and closed；
The executing agency connect with the blinds window cover 9, and the controller controls executing agency's work, so that
The blinds window cover 9 is closed or is opened.
In the present embodiment, one end of executing agency is connect with blinds window cover 9, and executing agency is electrically connected with the controller, when
When automobile needs flight, controller is operated, controller issues executing agency and instructs, and actuating mechanism controls blinds window cover 9 is beaten
It opens.
On the basis of the above embodiments, further, there are three wheels for setting on the vehicle body 1.
Further, there are four wheels for setting on the vehicle body 1.
It is settable there are four wheel either three wheels on vehicle body 1 in the present embodiment, it needs to be used according to specific
It needs to be adjusted.
Finally, it should be noted that the above embodiments are only used to illustrate the technical solution of the present invention., rather than its limitations；To the greatest extent
Pipe present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that: its according to
So be possible to modify the technical solutions described in the foregoing embodiments, or to some or all of the technical features into
Row equivalent replacement；And these are modified or replaceed, various embodiments of the present invention technology that it does not separate the essence of the corresponding technical solution
The range of scheme.
Claims (10)
1. a kind of automobile aerocraft characterized by comprising vehicle body, wing, power device and avoiding device；
The two sides of the vehicle body are collapsibly provided with the wing, and the avoiding device is arranged on the vehicle body；
The power device includes the first rotor mechanism being arranged on the wing, and first rotor mechanism is arranged described
Wing is close to the side of the vehicle body.
2. automobile aerocraft according to claim 1, which is characterized in that the power device further include preceding rotor mechanism,
Rotor mechanism and vertical rotor mechanism afterwards；
The front end of the vehicle body is arranged in the preceding rotor mechanism, and the rear end of the vehicle body, institute is arranged in the rear rotor mechanism
It states vertical rotor mechanism and lower end is set in the middle part of the vehicle body.
3. automobile aerocraft according to claim 2, which is characterized in that the vertical rotor mechanism includes multiple vertical rotations
The lower end middle part of the wing, the vehicle body is provided with multiple mounting grooves；
Multiple institute's mounting grooves are arranged in a one-to-one correspondence with multiple vertical rotors, and are provided with extensible member in the mounting groove,
The center axis connection of the extensible member and the vertical rotor；When the extensible member is shunk, the vertical rotor is contained in institute
It states in mounting groove.
4. automobile aerocraft according to claim 3, which is characterized in that multiple vertical rotors are evenly distributed on described
In the middle part of vehicle body lower end.
5. automobile aerocraft according to claim 1, which is characterized in that the avoiding device includes being arranged in the vehicle body
Four parachute assemblies of two sides and head and the tail both ends.
6. automobile aerocraft according to claim 5, which is characterized in that the parachute assembly includes ejection mechanism, touching
Send out mechanism and parachute；
The receiving storehouse for accommodating the parachute and the ejection mechanism is provided on the vehicle body；The opening for accommodating storehouse
Place is provided with cover board, and the cover board is for covering or exposing the opening；
The ejection mechanism is connect with the parachute and the trigger mechanism respectively；The trigger mechanism is for controlling the lid
Plate is mobile to expose opening, and controls the ejection mechanism and the parachute is removed the receiving storehouse.
7. automobile aerocraft according to claim 6, which is characterized in that be provided on the wing for installing the first rotation
The installing port of wing mechanism, and blinds window cover is provided on the installing port.
8. automobile aerocraft according to claim 7, which is characterized in that be additionally provided in the vehicle body described for controlling
The controller of blinds window cover opening and closing and executing agency；
The executing agency connect with the blinds window cover, and the controller controls executing agency's work, so that described
Blinds window cover is closed or is opened.
9. automobile aerocraft according to claim 1-8, which is characterized in that there are three vehicles for setting on the vehicle body
Wheel.
10. automobile aerocraft according to claim 1-8, which is characterized in that on the vehicle body there are four settings
Wheel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810726455.XA CN108944306A (en) | 2018-07-04 | 2018-07-04 | Automobile aerocraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810726455.XA CN108944306A (en) | 2018-07-04 | 2018-07-04 | Automobile aerocraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108944306A true CN108944306A (en) | 2018-12-07 |
Family
ID=64485712
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810726455.XA Pending CN108944306A (en) | 2018-07-04 | 2018-07-04 | Automobile aerocraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108944306A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TW420622B (en) * | 1999-08-23 | 2001-02-01 | Fuji Ya Entpr Co Ltd | Lose-control safety device for remote controlled model flight vehicle |
| CN202863052U (en) * | 2012-11-13 | 2013-04-10 | 湖南航天机电设备与特种材料研究所 | Multifunctional flying vehicle |
| CN106827993A (en) * | 2017-03-28 | 2017-06-13 | 刘宾 | A kind of four culvert vertical take-off and landing hovercars |
| CN206288237U (en) * | 2016-12-09 | 2017-06-30 | 西安通飞航空科技有限责任公司 | Can VTOL Fixed Wing AirVehicle |
| CN108177491A (en) * | 2018-01-08 | 2018-06-19 | 杨中震 | One kind can vertical take-off and landing flying car |
| CN208630282U (en) * | 2018-07-04 | 2019-03-22 | 天津超算科技有限公司 | Automobile aerocraft |
-
2018
- 2018-07-04 CN CN201810726455.XA patent/CN108944306A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TW420622B (en) * | 1999-08-23 | 2001-02-01 | Fuji Ya Entpr Co Ltd | Lose-control safety device for remote controlled model flight vehicle |
| CN202863052U (en) * | 2012-11-13 | 2013-04-10 | 湖南航天机电设备与特种材料研究所 | Multifunctional flying vehicle |
| CN206288237U (en) * | 2016-12-09 | 2017-06-30 | 西安通飞航空科技有限责任公司 | Can VTOL Fixed Wing AirVehicle |
| CN106827993A (en) * | 2017-03-28 | 2017-06-13 | 刘宾 | A kind of four culvert vertical take-off and landing hovercars |
| CN108177491A (en) * | 2018-01-08 | 2018-06-19 | 杨中震 | One kind can vertical take-off and landing flying car |
| CN208630282U (en) * | 2018-07-04 | 2019-03-22 | 天津超算科技有限公司 | Automobile aerocraft |
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