CN108008737A - A kind of release of vehicle-mounted unmanned aerial vehicle and retracting device - Google Patents
A kind of release of vehicle-mounted unmanned aerial vehicle and retracting device Download PDFInfo
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- CN108008737A CN108008737A CN201711223110.4A CN201711223110A CN108008737A CN 108008737 A CN108008737 A CN 108008737A CN 201711223110 A CN201711223110 A CN 201711223110A CN 108008737 A CN108008737 A CN 108008737A
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- 238000012545 processing Methods 0.000 claims abstract description 11
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims abstract description 9
- 238000002604 ultrasonography Methods 0.000 claims abstract description 9
- 238000004064 recycling Methods 0.000 claims abstract description 8
- 241000251730 Chondrichthyes Species 0.000 claims description 8
- 210000004291 uterus Anatomy 0.000 claims description 7
- 238000010408 sweeping Methods 0.000 claims description 3
- 238000005516 engineering process Methods 0.000 abstract description 4
- 238000010586 diagram Methods 0.000 description 8
- 230000007704 transition Effects 0.000 description 6
- 230000007246 mechanism Effects 0.000 description 4
- 230000008859 change Effects 0.000 description 3
- 238000004891 communication Methods 0.000 description 3
- 238000013461 design Methods 0.000 description 2
- 238000001514 detection method Methods 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 239000000725 suspension Substances 0.000 description 2
- 230000000007 visual effect Effects 0.000 description 2
- 206010039203 Road traffic accident Diseases 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000003028 elevating effect Effects 0.000 description 1
- 239000000686 essence Substances 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000007373 indentation Methods 0.000 description 1
- 230000005389 magnetism Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
Classifications
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
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- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G1/00—Traffic control systems for road vehicles
- G08G1/09—Arrangements for giving variable traffic instructions
- G08G1/0962—Arrangements for giving variable traffic instructions having an indicator mounted inside the vehicle, e.g. giving voice messages
- G08G1/0967—Systems involving transmission of highway information, e.g. weather, speed limits
- G08G1/096766—Systems involving transmission of highway information, e.g. weather, speed limits where the system is characterised by the origin of the information transmission
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Abstract
The invention belongs to technical field of traffic transportation, release and retracting device more particularly to a kind of vehicle-mounted unmanned aerial vehicle, including the cabin in vehicle ceiling, nacelle top is equipped with electric folding door, ultrasonic signal transmitting module is equipped with cabin, when recycling unmanned plane, automatic flight control modules control unmanned plane to make a return voyage to vehicle up direction according to the positional information of GPS navigation module first, ultrasonic signal transmitting module interval in cabin sends ultrasonic pulse signal, the multiple ultrasound signal receipt modules set on unmanned plane receive the pulse signal and send to data processing module, the time difference that data processing module receives signal according to each ultrasound signal receipt module calculates specific location of the cabin relative to unmanned plane, automatic flight control modules control unmanned plane to fall into cabin according to the positional information.The present invention carries out precise positioning using ultrasonic technology to unmanned plane, can accurately drop in specified region, so as to fulfill the automatic recycling of vehicle-mounted unmanned aerial vehicle.
Description
Technical field
The invention belongs to technical field of traffic transportation, and in particular to a kind of release of vehicle-mounted unmanned aerial vehicle and retracting device.
Background technology
With the continuous development of society, people's living standard gradually steps up, and automobile has become most of family must can not
Few vehicles, however, being continuously increased with car ownership, urban traffic conditions are also increasingly busy, big-and-middle at some
Type city, the early, traffic congestion of evening peak is even more homely food, and for driver, road ahead is predicted in advance
Passage situation can effectively avoid congestion.With the continuous development of network technology, electronic map has had been provided with road conditions forecast
Function, it will be appreciated, however, that the road conditions advance notice of electronic map is often based on that big data is calculated as a result, therefore its is pre-
Result is accused with actual road conditions there may be discrepancy, for example, on a highway with multiple tracks, may be due to traffic thing
Therefore or the reason such as traffic control cause the more congestion of part track, and then passage rate is very fast in some tracks, in this case, electricity
Sub- map can only provide unique advance notice as a result, which the smooth bar track more congestion of which bar lane of driver can not be informed,
Driven into Deng vehicle after congested link it is difficult to remove change lane again, lane change by force easily triggers new traffic accident on the contrary.Cause
This to accurately understand front road conditions, it is also necessary to a kind of more structurally sound road conditions detection system.Present inventor designs
A kind of road conditions detection system based on unmanned plane, but this system also needs to rely on a set of reliable vehicle-mounted unmanned aerial vehicle folding and unfolding
Mechanism.
The content of the invention
The object of the present invention is to provide a kind of release for the vehicle-mounted unmanned aerial vehicle that can quickly discharge and accurately recycle unmanned plane
And retracting device.
To achieve the above object, the present invention provides following technical scheme：A kind of release of vehicle-mounted unmanned aerial vehicle and recycling dress
Put, the vehicle-mounted unmanned aerial vehicle discharges and retracting device is located at vehicle roof, including the cabin in vehicle ceiling, the cabin
Top is equipped with electric folding door, and ultrasonic signal transmitting module is equipped with the cabin, when recycling unmanned plane, oneself on unmanned plane
Dynamic flight control modules control unmanned plane to make a return voyage to vehicle up direction according to the positional information of GPS navigation module first, then
Ultrasonic signal transmitting module interval in cabin sends ultrasonic pulse signal, the multiple ultrasonic signals set on unmanned plane
Receiving module receives the pulse signal and sends to data processing module, and data processing module is according to each ultrasound signal receipt mould
The time difference that block receives signal calculates specific location of the cabin relative to unmanned plane, and automatic flight control modules are believed according to the position
Breath control unmanned plane is fallen into cabin.
Preferably, the unmanned plane is quadrotor unmanned vehicle, including chassis and upper cover, the upper cover are shark fins
Shape, the camera are installed in upper cover, and camera is set towards shark fins rear, and the camera is installed on a turntable
On, the axis horizontal of turntable is set, and enables the upper and lower sweeping of camera；Four equipped with cross distribution, the chassis is outstanding
Arm, is respectively provided with a rotor above four cantilever ends, a ultrasound signal receipt module is respectively provided with below four cantilever ends；When
When unmanned plane is deposited in cabin, the upper cover protrudes from the top face of vehicle, and the electric folding door, which is equipped with, to be used to keep away
Allow the notch of upper cover.
Preferably, the uav bottom is equipped with an inserted block, and the side of the inserted block is the inclined plane shape inwardly collapsed, described
Inserted block bottom is equipped with magnetic charging connector；The engine room inside is equipped with an engine base, and the engine base, which vertically moves back and forth, to be set
Put, the engine base is equipped with is equipped with magnetic cradle with the matched slot of the inserted block, the slot bottom surface.
Preferably, permanent magnets are correspondingly arranged on the bottom surface of the inserted block and the bottom surface of slot.
Preferably, the electric folding door includes the sliding door of two symmetrical foldings, and two sliding door joints, which are equipped with, to be used to avoid
The notch of unmanned plane upper cover, wherein a fan sliding door is equipped with cervical orifice of uterus in indentation, there, the cervical orifice of uterus is fitted to be can be by the notch
Close and can be removed from the notch.
Preferably, the chassis is equipped with lifting motor, and the main shaft of the lifting motor is connected with a vertical screw, described
Nut is fixed with upper cover, which forms thread fitting with screw, and upright guide rail, the upper cover are additionally provided with the chassis
It is interior to be equipped with and the matched guide sleeve of upright guide rail.
Preferably, the engine base side is equipped with first connecting rod and second connecting rod, in the first connecting rod and second connecting rod
Portion is hinged, and upper end and the engine base of first connecting rod are hinged at, and lower end is hinged with the sliding block set on cabin floor, and second connects
The horizontal slider that the upper end of bar is set with engine base side is hinged, and lower end is hinged with cabin floor, and the cabin floor, which is equipped with, to be risen
Motor is dropped, leading screw is connected with the main shaft of the lifting motor, the sliding block is equipped with threaded hole, and sliding block forms screw thread with leading screw and matches somebody with somebody
Close.
The technical effects of the invention are that：The present invention carries out precise positioning using ultrasonic technology to unmanned plane, can
It is enough accurately to drop in specified region, so as to fulfill the automatic recycling of vehicle-mounted unmanned aerial vehicle.
Brief description of the drawings
Fig. 1 is release and the retracting device structure diagram for the vehicle-mounted unmanned aerial vehicle that the embodiment of the present invention is provided；
Fig. 2-6 is that each station stereochemical structure of release process for the unmanned plane applying mechanism that the embodiment of the present invention is provided is shown
It is intended to；
Fig. 7 is the side view before the unmanned plane that the embodiment of the present invention is provided discharges；
Fig. 8 is the side view after the unmanned plane that the embodiment of the present invention is provided discharges；
Fig. 9 is the dimensional structure diagram for the unmanned plane that the embodiment of the present invention is provided；
Figure 10 is the dimensional structure diagram at another visual angle of unmanned plane that the embodiment of the present invention is provided；
Figure 11 is the dimensional structure diagram at the another visual angle of unmanned plane that the embodiment of the present invention is provided；
Figure 12 is the dimensional structure diagram for the unmanned plane folding state that the embodiment of the present invention is provided；
Figure 13 is the bottom view for the unmanned plane folding state that the embodiment of the present invention is provided；
Figure 14 is the folding transmission mechanism schematic diagram for the unmanned plane that the embodiment of the present invention is provided；
Figure 15 is the elevating drive mechanism schematic diagram for the unmanned plane that the embodiment of the present invention is provided；
Figure 16 is the lifting seat dimensional structure diagram that the embodiment of the present invention is provided.
Embodiment
The present invention is described in detail below in conjunction with attached drawing.
Fig. 1-16 illustrated embodiments provide release and the retracting device of a kind of vehicle-mounted unmanned aerial vehicle, including unmanned plane 10 and car
Mounted terminal 30；
The unmanned plane 10 includes camera 11, data processing module 14, GPS navigation module 12, automatic flight control mould
Block 15 and wireless communication module 16, tell that camera 11 is used to gather the road surface video information in front of traffic route, camera
The vision signal collected is sent to data processing module 14, data processing module 14 and is converted to vision signal for nothing by 11
The interim signal of line communication module transmitting-receiving, the wireless communication module remotely sends interim signal to car-mounted terminal 30, described
Car-mounted terminal 30 includes remote control module 31 and video display module 32 again, and car-mounted terminal 30 handles signal and by nothing
The video information real-time display of man-machine 10 collection is controlled on screen in the car.The present invention is certain using 10 collection vehicle of unmanned plane front
In the range of road surface pass through video, and video is sent to car-mounted terminal 30, driver in real time and just can by controlling screen in vehicle
It is clearly understood that front wagon flow situation, hides congestion to shift to an earlier date change lane, improve traffic efficiency.
Further, vehicle-mounted unmanned aerial vehicle release and retracting device are further included, the vehicle-mounted unmanned aerial vehicle discharges and retracting device
Positioned at vehicle roof, including the cabin in vehicle ceiling 20, the nacelle top is equipped with electric folding door, in the cabin
Equipped with ultrasonic signal transmitting module, the unmanned plane 10 is equipped with least three ultrasound signal receipt modules 13, and each super
Acoustic signals receiving module 13 is located remotely from each other setting on unmanned plane 10；When recycling unmanned plane 10, automatic flight control modules 15
Unmanned plane 10 is controlled to make a return voyage to vehicle up direction according to the positional information of GPS navigation module 12 first, it is then super in cabin
Acoustic signals transmitting module interval sends ultrasonic pulse signal, and each ultrasound signal receipt module 13 on unmanned plane 10 receives
The pulse signal and sending to data processing module 14, data processing module 14 is received according to each ultrasound signal receipt module 13
The time difference of signal calculates cabin relative to the specific location of unmanned plane 10, and automatic flight control modules 15 are according to the positional information
Control unmanned plane 10 is fallen into cabin.
Preferably, the unmanned plane 10 is 18 unmanned vehicle of quadrotor, including chassis 102 and upper cover 101, the upper cover
101 be shark fin-shaped, and the camera 11 is installed in upper cover 101, and camera 11 is set towards shark fins rear, described to take the photograph
As first 11 are installed on a turntable 1013, the axis horizontal of turntable 1013 is set, and enables camera sweeping about 11；The bottom
Disk 102 is equipped with four cantilevers 17 of cross distribution, and a rotor 18, four cantilevers, 17 end are respectively provided with above four cantilevers, 17 end
A ultrasound signal receipt module 13 is respectively provided with below portion；When unmanned plane 10 is deposited in cabin, the upper cover 101 is protruded
In the top face of vehicle, the electric folding door is equipped with the notch 211 for being used for avoiding upper cover 101.When unmanned plane 10 is in
During recycling state, protruding out the camera 11 on roof can make as the camera 11 of automobile data recorder or electronics rearview mirror
With the upper cover 101 of shark fin-shaped makes vehicle roof keep beautiful.
Preferably, four cantilevers 17 of the unmanned plane 10 are pivotally connected along vertical axis and chassis 102, enable four cantilevers 17
It is in Jie's font folding to the fin point direction of shark fins.
Preferably, a gear 171 is respectively equipped with the pivot of four cantilevers 17, the folding of four cantilevers 17 is by chassis 102
The folding motor driving that inside is set, the main shaft of folding motor are equipped with the first duplicate gear 103, folding motor and each pivot it
Between drive path be followed successively by：I gears in first duplicate gear 103 at the same time with the pivot gear 171 of offside rear suspension arm 17 and
First Transition gear 105 engages, and First Transition gear 105 is engaged with the pivot gear 171 of nearside rear suspension arm 17, the first duplicate gear
II gears in 103 are engaged by synchronous belt with the I gears of the second duplicate gear 104, No. II of the second duplicate gear 104
Gear is engaged with 171 and second transition gear 106 of pivot gear of right front boom 17 at the same time, the second transition gear 106 with it is left front
The pivot gear 171 of cantilever 17 engages；The wherein gearratio of the I gears of the first duplicate gear 103 and First Transition gear 105
For 1:1, the gearratio of the II gears of the second duplicate gear 104 and the second transition gear 106 is 1:1, the first duplicate gear 103
II gears and the second duplicate gear 104 I gears between gearratio be more than 1, this is because two cantilever 17 of rear is received
Stroke during folding is more than stroke during two 17 folding of cantilever of front, so to ensure both foldings at the same time in place, rear cantilever 17
Folding speed have to be larger than the folding speed of front cantilever 17, the difference of both folding speed passes through the first duplicate gear 103
II gears and the second duplicate gear 104 I gears between gearratio be controlled.
Preferably, 10 bottom of unmanned plane is equipped with an inserted block 19, and the side of the inserted block 19 is the inclined-plane inwardly collapsed
Shape, 19 bottom of inserted block are equipped with magnetic charging connector 191；The engine room inside is equipped with an engine base 24, and the engine base 24 is along perpendicular
Nogata is to setting is moved back and forth, and the engine base 24 is equipped with and the matched slot 242 of the inserted block 19,242 bottom of slot
Face is equipped with magnetic cradle 243, and landing just automatically begins to charge in place unmanned plane 10 every time, it is ensured that electricity is sufficient.Due to slot
242 and the side wall of inserted block 19 carry certain taper, therefore even if there is the certain error also can be on inclined-plane when unmanned plane 10 lands
The lower automatic capturing of effect, it is ensured that magnetic charging connector 191 smoothly docks.
Preferably, permanent magnets 192,244, permanent magnetism are correspondingly arranged on the bottom surface of the inserted block 19 and the bottom surface of slot 242
Block 192,244 can make to produce certain the suction-combining force between unmanned plane 10 and engine base 24, avoid unmanned plane 10 from producing and rock.
Preferably, the electric folding door includes the sliding door 21 of two symmetrical foldings, and two sliding doors, 21 joint, which is equipped with, to be used for
The notch 211 of 10 upper cover 101 of unmanned plane is avoided, wherein a fan sliding door 21 is equipped with cervical orifice of uterus 22,22 quilt of cervical orifice of uterus at notch 211
Assemble as that can close and can be removed the notch 211 from the notch 211.The folding of the sliding door 21 and cervical orifice of uterus 22
Mode may be referred to the open-close ways of vehicle dormer window in the prior art, the design focal point of this structure and non-invention, therefore not
It is described in detail again.
Preferably, the upper cover 101 vertically moves back and forth setting, the bottom of the upper cover 101 relative to chassis 102
Face is equipped with Gask-O-Seal.In removal process, after unmanned plane 10 falls into cabin, upper cover 101 is first lifted, then electric folding door
Closure, upper cover 101 reset still further below, the gasket on its bottom surface is close to the edge of notch 211, it is ensured that roof sealing can
Lean on.
Preferably, the chassis 102 is equipped with lifting motor 25, the main shaft of the lifting motor 25 and a vertical screw
109 are connected, and nut 1011 is fixed with the upper cover 101, which forms thread fitting, the bottom with screw 109
Upright guide rail 1021 is additionally provided with disk 102, guide sleeve 1012 matched with upright guide rail 1021 is equipped with the upper cover 101.
Preferably, 24 side of engine base is equipped with first connecting rod 29 and second connecting rod 28, the first connecting rod 29 and second
The middle part of connecting rod 28 is hinged, and upper end and the engine base 24 of first connecting rod 29 are hinged at, and lower end on cabin floor 23 with setting
Sliding block 26 it is hinged, the horizontal slider 241 that upper end and 24 side of engine base of second connecting rod 28 are set is hinged, lower end and cabin floor
23 is hinged, and the cabin floor 23 is equipped with lifting motor 25, and leading screw 27, the cunning are connected with the main shaft of the lifting motor 25
Block 26 is equipped with threaded hole, and sliding block 26 forms thread fitting with leading screw 27.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all essences in the present invention
All any modification, equivalent and improvement made within refreshing and principle etc., should all be included in the protection scope of the present invention.
Claims (8)
1. release and the retracting device of a kind of vehicle-mounted unmanned aerial vehicle, it is characterised in that：The vehicle-mounted unmanned aerial vehicle discharges and retracting device
Positioned at vehicle roof, including the cabin in vehicle ceiling (20), the nacelle top are equipped with electric folding door, the cabin
It is interior to be equipped with ultrasonic signal transmitting module；When recycling unmanned plane (10), the automatic flight control modules (15) on unmanned plane (10)
Unmanned plane (10) is controlled to make a return voyage to vehicle up direction according to the positional information of GPS navigation module (12) first, then in cabin
Ultrasonic signal transmitting module interval send ultrasonic pulse signal, the multiple ultrasonic signals set on unmanned plane (10) connect
Receive module (13) to receive the pulse signal and send to data processing module (14), data processing module (14) is according to each ultrasonic wave
The time difference that signal receiving module (13) receives signal calculates specific location of the cabin relative to unmanned plane (10), automatic flight
Control module (15) controls unmanned plane (10) to fall into cabin according to the positional information.
2. release and the retracting device of vehicle-mounted unmanned aerial vehicle according to claim 2, it is characterised in that：The unmanned plane (10)
For quadrotor unmanned vehicle, including chassis (102) and upper cover (101), the upper cover (101) is shark fin-shaped, the shooting
Head (11) is installed in upper cover (101), and camera (11) is set towards shark fins rear, and the camera (11) is installed on one
On turntable (1013), the axis horizontal of turntable (1013) is set, and makes camera (11) being capable of upper and lower sweeping；The chassis (102)
Four cantilevers (17) of cross distribution are equipped with, a rotor (18), four cantilevers are respectively provided with above four cantilevers (17) end
(17) a ultrasound signal receipt module (13) is respectively provided with below end；It is described when unmanned plane (10) is deposited in cabin
Upper cover (101) protrudes from the top face of vehicle, and the electric folding door is equipped with the notch for being used for avoiding upper cover (101)
(211)。
3. release and the retracting device of vehicle-mounted unmanned aerial vehicle according to claim 2, it is characterised in that：The unmanned plane (10)
Bottom is equipped with an inserted block (19), and the side of the inserted block (19) is the inclined plane shape inwardly collapsed, and inserted block (19) bottom is equipped with
Magnetic charging connector (191)；The engine room inside is equipped with an engine base (24), and the engine base (24) vertically moves back and forth and sets
Put, the engine base (24) is equipped with is equipped with magnetic with the inserted block (19) matched slot (242), slot (242) bottom surface
Inhale cradle (243).
4. release and the retracting device of vehicle-mounted unmanned aerial vehicle according to claim 3, it is characterised in that：The inserted block (19)
Permanent magnets (192,244) are correspondingly arranged on bottom surface and the bottom surface of slot (242).
5. release and the retracting device of vehicle-mounted unmanned aerial vehicle according to claim 3, it is characterised in that：The electric folding door
Include the sliding door (21) of two symmetrical foldings, two sliding doors (21) joint, which is equipped with, to be used to avoid unmanned plane (10) upper cover (101)
Notch (211), wherein a fan sliding door (21) is equipped with cervical orifice of uterus (22) at notch (211) place, the cervical orifice of uterus (22) fitted to be can
The notch (211) is closed and can removed from the notch (211).
6. release and the retracting device of vehicle-mounted unmanned aerial vehicle according to claim 5, it is characterised in that：The upper cover (101)
Vertically move back and forth and set relative to chassis (102), the bottom surface of the upper cover (101) is equipped with Gask-O-Seal.
7. release and the retracting device of vehicle-mounted unmanned aerial vehicle according to claim 6, it is characterised in that：The chassis (102)
Lifting motor (108) is equipped with, the main shaft of the lifting motor (108) is connected with a vertical screw (109), the upper cover
(101) nut (1011) is fixed with, which forms thread fitting with screw (109), and the chassis (102) is interior
Upright guide rail (1021) is additionally provided with, is equipped with and upright guide rail (1021) matched guide sleeve (1012) in the upper cover (101).
8. release and the retracting device of vehicle-mounted unmanned aerial vehicle according to claim 3, it is characterised in that：Engine base (24) side
Face is equipped with first connecting rod (29) and second connecting rod (28), and the middle part of the first connecting rod (29) and second connecting rod (28) is mutually cut with scissors
Connect, upper end and the engine base (24) of first connecting rod (29) are hinged at, and lower end is cut with scissors with the sliding block (26) set on cabin floor (23)
Connect, the horizontal slider (241) that upper end and engine base (24) side of second connecting rod (28) are set is hinged, lower end and cabin floor (23)
Hinged, the cabin floor (23) is equipped with lifting motor (25), and leading screw (27) is connected with the main shaft of the lifting motor (25),
The sliding block (26) is equipped with threaded hole, and sliding block (26) forms thread fitting with leading screw (27).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711223110.4A CN108008737A (en) | 2017-11-29 | 2017-11-29 | A kind of release of vehicle-mounted unmanned aerial vehicle and retracting device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711223110.4A CN108008737A (en) | 2017-11-29 | 2017-11-29 | A kind of release of vehicle-mounted unmanned aerial vehicle and retracting device |
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| CN108008737A true CN108008737A (en) | 2018-05-08 |
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ID=62054445
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|---|---|---|---|
| CN201711223110.4A Pending CN108008737A (en) | 2017-11-29 | 2017-11-29 | A kind of release of vehicle-mounted unmanned aerial vehicle and retracting device |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN108725812A (en) * | 2018-05-10 | 2018-11-02 | 送飞实业集团有限公司 | A kind of sound wave is to just guiding landing system |
| CN109515640A (en) * | 2018-11-22 | 2019-03-26 | 深圳市海斯比船艇科技股份有限公司 | Unmanned boat folding and unfolding unmanned plane device and control method based on electroactive polymer |
| CN111324140A (en) * | 2018-12-14 | 2020-06-23 | 北京宝沃汽车有限公司 | Method, system and device for controlling return flight of unmanned aerial vehicle and unmanned aerial vehicle |
| CN111942266A (en) * | 2020-09-11 | 2020-11-17 | 中国人民解放军陆军炮兵防空兵学院 | Unmanned aerial vehicle take-off and landing platform |
| CN112130583A (en) * | 2020-09-14 | 2020-12-25 | 国网天津市电力公司 | Method and device for detecting partial discharge of unmanned aerial vehicle during night patrol |
| CN112821935A (en) * | 2020-12-30 | 2021-05-18 | 嘉兴安步信息科技有限公司 | Information acquisition system based on unmanned aerial vehicle platform |
| CN112888630A (en) * | 2018-08-24 | 2021-06-01 | 周鹏跃 | Method for transferring goods between unmanned aerial vehicle and automatic driving vehicle |
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