CN208630283U - Automobile aerocraft - Google Patents
Automobile aerocraft Download PDFInfo
- Publication number
- CN208630283U CN208630283U CN201821063487.8U CN201821063487U CN208630283U CN 208630283 U CN208630283 U CN 208630283U CN 201821063487 U CN201821063487 U CN 201821063487U CN 208630283 U CN208630283 U CN 208630283U
- Authority
- CN
- China
- Prior art keywords
- vehicle body
- wing
- rotor
- parachute
- automobile aerocraft
- 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.)
- Active
Links
Abstract
The utility model 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 power device includes the bispin wing mechanism that wing one end is arranged in, and the other end of the wing is arranged on the vehicle body for being connected to the vehicle body, the avoiding device；The wing can be folded to the direction close to the vehicle body, and the bispin wing mechanism can be to the direction folding close to wing.To alleviate festivals or holidays traffic jam existing in the prior art, inconvenient technical problem of going on a journey.
Description
Technical field
The utility model 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.
Utility model content
The purpose of this utility model is to provide automobile aerocrafts, stifled to alleviate festivals or holidays traffic existing in the prior art
Plug, inconvenient technical problem of going on a journey.
A kind of automobile aerocraft provided by the utility model, comprising: vehicle body, wing, power device and avoiding device；
The power device includes the bispin wing mechanism that wing one end is arranged in, and the other end of the wing is for being connected to
On the vehicle body, the avoiding device is arranged on the vehicle body；
The wing can be folded to the direction close to the vehicle body, and the bispin wing mechanism can be to close to wing
Direction folding.
Further, the bispin wing mechanism includes Dual-output shaft motor, the first rotor and the second rotor；The dual output
The one end of wing far from the vehicle body is arranged in spindle motor, and first rotor sets second rotor and is symmetricly set on described pair
Export the both ends of spindle motor.
Further, first rotor includes the first fixed frame and two the first blades；
First fixed frame is fixedly connected with the Dual-output shaft motor, and there are two for setting on first fixed frame
One mounting groove, two first blades are separately positioned in two first mounting grooves, and first blade being capable of phase
First mounting groove is rotated, first blade is folded.
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, 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 utility model, comprising: vehicle body, wing, power device and avoiding device；The power
Device includes the bispin wing mechanism that wing one end is arranged in, and the other end of the wing is described for being connected to the vehicle body
Avoiding device is arranged on the vehicle body；The wing can be folded to the direction close to the vehicle body, and the DCB Specimen machine
Structure can be to the direction folding close to wing.Using above-mentioned scheme, DCB Specimen machine is provided with far from one end of vehicle body in wing
Structure, and wing can be folded to the side of vehicle body, meanwhile, bispin wing mechanism can folding, in this way, automobile need to take off when
Wing is unfolded time, while by DCB Specimen mechanism opening, power device is started to work, and to provide lift for vehicle body, makes vehicle body liter
Sky, while avoiding device is mounted on vehicle body, in this way when automobile runs out of steam in the sky, avoiding device can be good at dropping
The case where low personnel cause danger, to alleviate festivals or holidays traffic jam existing in the prior art, inconvenient technical problem of going on a journey.
Detailed description of the invention
It, below will be right in order to illustrate more clearly of specific embodiment of the present invention or technical solution in the prior art
Specific embodiment or attached drawing needed to be used in the description of the prior art are briefly described, it should be apparent that, it is described below
In attached drawing be that some embodiments of the utility model are not paying creativeness for those of ordinary skill in the art
Under the premise of labour, it is also possible to obtain other drawings based on these drawings.
Fig. 1 is top view when automobile aerocraft avoiding device provided by the embodiment of the utility model is opened；
Fig. 2 is bottom view when automobile aerocraft vertical rotor provided by the embodiment of the utility model mechanism works；
Fig. 3 is the partial schematic diagram of automobile aerocraft provided by the embodiment of the utility model；
Side view when Fig. 4 is automobile aerocraft wing provided by the embodiment of the utility model and bispin wing mechanism folding.
Icon: 1- vehicle body；2- wing；3- avoiding device；The first rotor of 4-；Rotor mechanism before 5-；Rotor mechanism after 6-；7-
Vertical rotor mechanism；8- mounting groove；The first blade of 401-；The first fixed frame of 402-；701- vertical rotor；702- extensible member.
Specific embodiment
The technical solution of the utility model is clearly and completely described below in conjunction with attached drawing, it is clear that described
Embodiment is the utility model a part of the embodiment, instead of all the embodiments.Based on the embodiments of the present invention, originally
Field those of ordinary skill every other embodiment obtained without making creative work belongs to practical
Novel protected range.
In the description of the present invention, it should be noted that such as occur term " center ", "upper", "lower", " left side ",
" right side ", "vertical", "horizontal", "inner", "outside" etc., indicated by orientation or positional relationship be orientation based on the figure or
Positional relationship is merely for convenience of describing the present invention and simplifying the description, rather than the device or member of indication or suggestion meaning
Part must have a particular orientation, be constructed and operated in a specific orientation, therefore should not be understood as limiting the present invention.
In addition, such as there is term " first ", " second ", " third " are used for description purposes only, be not understood to indicate or imply opposite
Importance.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, such as there is term
" installation ", " connected ", " connection " shall be understood in a broad sense, for example, it may be fixedly connected, may be a detachable connection or one
Connect to body；It can be mechanical connection, be also possible to be electrically connected；It can be directly connected, it can also be indirect by intermediary
It is connected, can be the connection inside two elements.For the ordinary skill in the art, on being understood with concrete condition
State the concrete meaning of term in the present invention.
Fig. 1 is top view when automobile aerocraft avoiding device provided by the embodiment of the utility model is opened；Fig. 4 is this reality
Side view when the automobile aerocraft wing provided with new embodiment and bispin wing mechanism folding.As shown in figs. 1 and 4, this reality
With a kind of automobile aerocraft of novel offer, comprising: vehicle body 1, wing 2, power device and avoiding device 3；
The power device includes the bispin wing mechanism that 2 one end of wing is arranged in, and the other end of the wing 2 is for connecting
On the vehicle body 1, the avoiding device 3 is arranged on the vehicle body 1；
The wing 2 can be folded to the direction close to the vehicle body 1, and the bispin wing mechanism can be to close to wing
2 direction folding.
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 utility model, comprising: vehicle body 1, wing 2, power device and avoiding device 3；It is described
Power device includes the bispin wing mechanism that 2 one end of wing is arranged in, and the other end of the wing 2 is for being connected to the vehicle body 1
On, the avoiding device 3 is arranged on the vehicle body 1；The wing 2 can be folded to the direction close to the vehicle body 1, and institute
Stating bispin wing mechanism can be to the direction folding close to wing 2.Using above-mentioned scheme, set in wing 2 far from one end of vehicle body 1
Set bispin wing mechanism, and wing 2 can be folded to the side of vehicle body 1, meanwhile, bispin wing mechanism can folding, in this way, vapour
Wing 2 is unfolded when vehicle needs to take off, while by DCB Specimen mechanism opening, power device is started to work, to mention for vehicle body 1
For lift, vehicle body 1 is made to go up to the air, while being mounted with avoiding device 3 on vehicle body 1, in this way when automobile runs out of steam in the sky, kept away
Dangerous device 3 can be good at the case where reduction personnel cause danger, to alleviate festivals or holidays traffic jam existing in the prior art,
The inconvenient technical problem of trip.
On the basis of the above embodiments, further, the bispin wing mechanism includes Dual-output shaft motor, the first rotor
4 and second rotor；The one end of wing 2 far from the vehicle body 1 is arranged in the Dual-output shaft motor, and first rotor 4 sets institute
State the both ends that the second rotor is symmetricly set on the Dual-output shaft motor.
Wherein, Dual-output shaft motor drives the first rotor 4 and the second rotor to rotate synchronously, and the first rotor 4 and the second rotation
Wing rotation direction is identical.
Wherein, the quantity of wing 2 is even number, can be two or four etc..
In the present embodiment, the first rotor 4 and the second rotor are worked at the same time, so that vehicle body 1 has enough lift to be risen,
Vehicle body 1 can complete in situ raising, so that automobile aerocraft can be risen in different environment, the width of road pavement
It is required that lower.Big to alleviate the horizontal space that flight trolley existing in the prior art occupies, in road traveling inconvenience, inconvenience is risen
The technical issues of rising.
On the basis of the above embodiments, further, first rotor 4 includes the first fixed frame 402 and two the
One blade 401；
First fixed frame 402 is fixedly connected with the Dual-output shaft motor, is provided on first fixed frame 402
Two the first mounting grooves 8, two first blades 401 are separately positioned in two first mounting grooves 8, and described first
Blade 401 can be rotated relative to first mounting groove 8, and first blade 401 is folded.
Wherein, when vehicle body 1 needs raising, two the first blades 401 are in the state of expansion, and two the first blades
401 on the same line, and in vehicle body 1 in road traveling, two the first blades 401 need to withdraw, two blades withdraw when,
It is arranged in parallel between two blades, relative friction will not be generated between two blades to ensure, that improves blade uses the longevity
Life, reduces the maintenance cost of single unit system.
In the present embodiment, two the first mounting grooves 8 are provided on the first fixed frame 402, two the first mounting grooves 8 are set relatively
It sets, two the first blades 401 are separately positioned in two the first mounting grooves 8, and two the first blades 401 can be with respect to
First blade 401 can be retracted to and wing 2 by the rotation of one mounting groove 8 in this way, needing when road traveling in vehicle body 1
The applicability of automobile aerocraft is improved to reduce the space that the transverse direction of vehicle body 1 is occupied in parallel position.
Fig. 2 is bottom view when automobile aerocraft vertical rotor provided by the embodiment of the utility model mechanism works；Fig. 3 is
The partial schematic diagram of automobile aerocraft provided by the embodiment of the utility model.As shown in Figures 2 and 3, on the basis of above-described embodiment
On, further, the power device further includes 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, 701 mechanism 7 of vertical rotor includes multiple vertical rotors
701, the lower end middle part of the vehicle body 1 is provided with multiple mounting grooves 8；
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.
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 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.
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 various embodiments is only to illustrate the technical solution of the utility model, rather than it is limited
System；Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should
Understand: it is still possible to modify the technical solutions described in the foregoing embodiments, or to some or all of
Technical characteristic is equivalently replaced；And these are modified or replaceed, it does not separate the essence of the corresponding technical solution, and this is practical new
The range of each embodiment technical solution of type.
Claims (10)
1. a kind of automobile aerocraft characterized by comprising vehicle body, wing, power device and avoiding device；
The power device includes the bispin wing mechanism that wing one end is arranged in, and the other end of the wing is described for being connected to
On vehicle body, the avoiding device is arranged on the vehicle body；
The wing can be folded to the direction close to the vehicle body, and the bispin wing mechanism can be to the direction close to wing
Folding.
2. automobile aerocraft according to claim 1, which is characterized in that the bispin wing mechanism includes double output shaft electricity
Machine, the first rotor and the second rotor；The one end of wing far from the vehicle body, first rotation is arranged in the Dual-output shaft motor
The wing sets the both ends that second rotor is symmetricly set on the Dual-output shaft motor.
3. automobile aerocraft according to claim 2, which is characterized in that first rotor includes the first fixed frame and two
A first blade；
First fixed frame is fixedly connected with the Dual-output shaft motor, and there are two the first peaces for setting on first fixed frame
Tankage, two first blades are separately positioned in two first mounting grooves, and first blade can be with respect to institute
The rotation of the first mounting groove is stated, first blade is folded.
4. 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.
5. automobile aerocraft according to claim 4, 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.
6. automobile aerocraft according to claim 5, which is characterized in that multiple vertical rotors are evenly distributed on described
In the middle part of vehicle body lower end.
7. 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.
8. automobile aerocraft according to claim 7, 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.
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 |
|---|---|---|---|
| CN201821063487.8U CN208630283U (en) | 2018-07-04 | 2018-07-04 | Automobile aerocraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821063487.8U CN208630283U (en) | 2018-07-04 | 2018-07-04 | Automobile aerocraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208630283U true CN208630283U (en) | 2019-03-22 |
Family
ID=65736772
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821063487.8U Active CN208630283U (en) | 2018-07-04 | 2018-07-04 | Automobile aerocraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208630283U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108556579A (en) * | 2018-07-04 | 2018-09-21 | 天津超算科技有限公司 | Automobile aerocraft |
-
2018
- 2018-07-04 CN CN201821063487.8U patent/CN208630283U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108556579A (en) * | 2018-07-04 | 2018-09-21 | 天津超算科技有限公司 | Automobile aerocraft |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN108146169B (en) | Wing rear-folding type air-ground dual-purpose carrier | |
| CN113370730B (en) | Flying car | |
| CN205273843U (en) | Many rotor unmanned aerial vehicle's multi -functional undercarriage | |
| CN102649391B (en) | Ground-effect type extreme low-altitude dual-purpose aerocar or dual-purpose aircraft | |
| CN104149971B (en) | A kind of unmanned plane | |
| CN105291737A (en) | Rotor car | |
| CN113071276B (en) | Flying car | |
| CN208630283U (en) | Automobile aerocraft | |
| CN109455051A (en) | A kind of 4 wheel driven hovercar | |
| CN201525255U (en) | Gyroplane landing ship capable of driving on land and water | |
| CN108177491A (en) | One kind can vertical take-off and landing flying car | |
| CN112659830A (en) | Self-rotary wing aerocar | |
| CN109911185B (en) | High-speed single-rotor tailless-rotor helicopter | |
| AU2022315399A1 (en) | Wing-and-rotary-wing mixed folding and unfolding system of flying vehicle, and flying vehicle | |
| CN208630282U (en) | Automobile aerocraft | |
| CN106799942A (en) | A kind of air-ground amphibious manned loading aircraft | |
| CN213168519U (en) | Air-ground dual-purpose unmanned aerial vehicle | |
| CN108357313B (en) | Flying car | |
| RU2385807C2 (en) | Aeromobile | |
| CN108556579A (en) | Automobile aerocraft | |
| CN109250082A (en) | A kind of multiaxis low latitude manned vehicle | |
| CN110774848A (en) | Four-duct air-ground dual-purpose vehicle with telescopic wings | |
| CN106275415A (en) | The aircraft that a kind of fixed-wing and many rotors can automatically switch | |
| CN108284722A (en) | A kind of hovercar | |
| CN108501638A (en) | A kind of hovercar of foldable rotor |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |