CN208198853U - The unmanned plane that unmanned plane shuts down library, which is reformed, shuts down library with clamping device and unmanned plane - Google Patents
The unmanned plane that unmanned plane shuts down library, which is reformed, shuts down library with clamping device and unmanned plane Download PDFInfo
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- CN208198853U CN208198853U CN201820793716.5U CN201820793716U CN208198853U CN 208198853 U CN208198853 U CN 208198853U CN 201820793716 U CN201820793716 U CN 201820793716U CN 208198853 U CN208198853 U CN 208198853U
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Abstract
It reforms the utility model discloses the unmanned plane that a kind of unmanned plane shuts down library and shuts down library with clamping device and unmanned plane, it mainly includes a pair of of the X-direction push rod being arranged on airplane parking area and a pair of of Y direction push rod with clamping device that the unmanned plane, which is reformed, two push rods of a pair of of X-direction push rod are oppositely arranged and synchronizing moving, two push rods of a pair of of Y direction push rod are oppositely arranged and synchronizing moving, a pair of of X-direction push rod and a pair of of Y direction push rod are driven by power and transmission mechanism realizes movement, several claws are respectively equipped on two push rods of the pair of X-direction push rod or the pair of Y direction push rod, charging electrode is equipped at least one described claw of each push rod.The utility model can be pushed away just the unmanned plane dropped on airplane parking area by a pair of of X-direction push rod and a pair of of Y direction push rod realization automatically, and ensure that the mobile synchronism of two push rods in same group of push rod.
Description
Technical field
The utility model relates to a kind of unmanned plane landing auxiliary device, in particular to a kind of nothings with automatic charge device
Man-machine shutdown library and its unmanned plane is reformed and clamping device.
Background technique
UAV, i.e. unmanned plane are operated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft because having many advantages, such as that at low cost, efficiency-cost ratio is good, risk is low, survival ability is strong, mobility is good, and is answered extensively
It is shot for high-altitude, and there is very strong application prospect in express delivery delivery field.
Unmanned plane is usually powered by the battery for carrying on it, is limited to limited mass that can be battery-mounted, and consume
Electricity constantly increases with the increase of ancillary equipment, causes its single voyage partially short, limits its application prospect and development.
In order to extend the cruising ability of unmanned plane, a kind of nothing is disclosed in the patent document of Publication No. CN106368478A
People's distributed unmanned plane on duty charges hangar comprising hangar protect cabinet, airplane parking area, can slip lid solar panel,
Battery pack, GPS/ Beidou positioning and communicating unit, control unit and wireless charging unit, battery pack are electrically connected with solar panel
To charge to it, wireless charging unit be electrically connected with battery pack and controlled by control unit and to resting on airplane parking area
Unmanned plane charges.Unmanned plane charging hangar is arranged by distributed in the patent document, can effectively extend the continuous of unmanned plane
Boat ability, but it is wireless charging, compared with wired charging, not only charge efficiency is lower, and charging equipment high expensive.
Utility model content
The utility model, which provides a kind of unmanned plane, shuts down the unmanned plane in library and reforms and clamping device and unmanned plane shut down library.
The technical solution of the utility model is as follows:
A kind of unmanned plane in unmanned plane shutdown library is reformed and clamping device, mainly includes a pair being arranged on airplane parking area
X-direction push rod and a pair of of Y direction push rod, two push rods of a pair of of X-direction push rod are oppositely arranged and synchronize shifting
Dynamic, two push rods of a pair of of Y direction push rod are oppositely arranged and synchronizing moving, a pair of of X-direction push rod and
A pair of of Y direction push rod is driven by power and transmission mechanism and realizes movement, in the pair of X-direction push rod or the pair of
Several claws are respectively equipped on two push rods of Y direction push rod, is equipped with and fills at least one described claw of each push rod
Electrode.
In the preferred embodiment, the pair of X-direction push rod is driven by independent power and transmission mechanism, described dynamic
Power and transmission mechanism include at least one power source, at least two groups belt wheel and cover the transmission belt on every group of belt wheel, it is described at least
Two groups of belt wheels are separately positioned on the opposite two sides of airplane parking area, and above-mentioned side is the shutdown vertical with the X-direction push rod
The side on level ground, the both ends of every X-direction push rod are separately fixed on the transmission belt of airplane parking area two sides, and two X-axis sides
The upper half and lower half of the side transmission belt are separately positioned on to the end positioned at same side of push rod.
In the preferred embodiment, the power of the pair of X-direction push rod and transmission mechanism include two groups of belt wheels, two
Transmission belt, the first power source, first group of belt wheel include first pulley, the second belt wheel, and second group of belt wheel includes third belt wheel, the 4th
Belt wheel, first pulley described in first power source drive, the first pulley drive second band to rotate by transmission belt
Dynamic, second belt wheel drives the third belt wheel rotation by a long axis, and the third belt wheel is driven by another transmission belt
4th belt wheel.Present embodiment designs two X-axis push rods and uses the same power source, and setting by above-mentioned drive mechanism
It sets, can be realized the synchronizing moving of two X-axis push rods.
In the preferred embodiment, the pair of Y direction push rod is driven by independent power and transmission mechanism, described
Power and transmission mechanism include at least one power source, at least two screw rods, at least two sliding blocks installed on every screw rod, institute
State the opposite two sides that airplane parking area is arranged at least two screw rods, the side is and the Y direction push rod is vertical stops
The both ends of the side on machine level ground, every Y direction push rod are separately fixed on the sliding block of two sides.
In the preferred embodiment, the power of the pair of Y direction push rod and transmission mechanism include two screw rods, four
Sliding block, the second power source, every screw rod are equipped with two sections of opposite screw threads of hand of spiral, second power source drive first
Screw rod, first screw rod rotation drive two sliding blocks mounted thereto to move towards or be away from each other movement, and described first
Realize and be driven that first screw rod drives second silk by synchronous belt in the end of the axis of root screw rod and second screw rod
Bar rotation, and then two sliding blocks on second screw rod move towards or are away from each other movement.Present embodiment designs two Y
Axis direction push rod uses the same power source, and the synchronizing moving of two Y direction push rods is realized by above-mentioned drive mechanism.
In the preferred embodiment, fixed by multiple connectors on the X-direction push rod or the Y direction push rod
There are third power source and a screw rod, meanwhile, the claw on the X-direction push rod or the Y direction push rod is set
It contacts or connects with some of connectors, the screw rod is equipped with thread segment, and the third power source drives the screw rod to turn
When dynamic, some connectors for contacting or connecting with the claw can be slided along the screw rod, and then drive the claw
It is mobile.The structure can make claw from two sides to middle propulsion, and then clamp unmanned plane undercarriage.
In the preferred embodiment, it installs and has elastic component after the claw, be compressed to preboarding in the elastic element
Microswitch is triggered when variable, the third power source stops.The structure guarantees that the charging electrode on claw rises and falls with unmanned plane
The contact force of electrode on frame realizes effectively charging.
Above-described first power source, the second power source, first, second, third in third power source are only used for area
Point, and the meaning without limitation.
The utility model also provides a kind of unmanned plane shutdown library comprising airplane parking area, and it is equipped with any of the above-described unmanned plane
It reforms and clamping device.
In the preferred embodiment, the middle part of the airplane parking area is equipped with to positive guidance mark.
In the preferred embodiment, the back side of the airplane parking area is equipped with several structural reinforcement members, and the structural reinforcement member is
Rod-shaped, the both ends of each structural reinforcement member are connected in two long sides of the airplane parking area.
Compared with prior art, the beneficial effects of the utility model are as follows:
A kind of unmanned plane provided by the utility model is reformed can be to the unmanned plane dropped on airplane parking area with clamping device
It is pushed away just, positive (groined type pushes away just) is pushed away by a pair of of X-direction push rod and a pair of of Y direction push rod realization automatically, and ensure that
The synchronism of two push rods movement in one group of push rod, while it being also provided with the vertical charging claw for clamping unmanned plane undercarriage,
Compared with existing laterally clamping, it is successfully realized another method of clamping.
Detailed description of the invention
Fig. 1 is that the unmanned plane of the utility model embodiment is reformed and the signal of the stereochemical structure at the positive visual angle of clamping device
Figure；
Fig. 2 reforms for the unmanned plane of the utility model embodiment to be shown with the stereochemical structure at another visual angle in front of clamping device
It is intended to；
Fig. 3 is the backside structure perspective view that the unmanned plane of the utility model embodiment is reformed with clamping device；
Fig. 4 is the backside structure front view that the unmanned plane of the utility model embodiment is reformed with clamping device；
Fig. 5 is that the unmanned plane of the utility model embodiment is reformed with the X-direction push rod of clamping device and is arranged thereon
The schematic perspective view of claw, stepper motor and screw rod；
Fig. 6 is that the unmanned plane of the utility model embodiment is reformed and configuration state of the clamping device after unmanned plane stop is shown
It is intended to；
Fig. 7 is that the unmanned plane of the utility model embodiment is reformed and clamping device is after unmanned plane stop, and claw is fixed
The configuration state schematic diagram of unmanned plane undercarriage；
Wherein, the airplane parking area 1-；2- a pair of X-direction push rod；21, two X-direction push rods of 22-；3- a pair of Y direction pushes away
Bar；31, two Y direction push rods of 32-；4- claw；The collet of 41- claw；The arc card pressure surface of 411- collet；51- first band
Wheel；The second belt wheel of 52-；53- third belt wheel；The 4th belt wheel of 54-；6- transmission belt；7- power source；8- long axis；9- sliding block；10- is same
Walk band；11- connector；13- structural reinforcement member；14- screw rod；141,142- thread segment；15- unmanned plane.
Specific embodiment
The utility model is further described below in conjunction with the drawings and specific embodiments.Following embodiment is only used for
For example, rather than the restriction protection scope of the utility model.In the examples below, identical label indicates similar
Element.
Embodiment
- Fig. 7 referring to Figure 1, a kind of unmanned plane that shutting down library for unmanned plane provided in this embodiment are reformed and clamping machine
Structure, main includes a pair of of the X-direction push rod 2 being arranged on airplane parking area 1 and a pair of of Y direction push rod 3, a pair of of X-axis
Two push rods (push rod 21, push rod 22) of direction push rod 2 are oppositely arranged and synchronizing moving, a pair of of Y direction push rod 3
Two push rods (push rod 31, push rod 32) are oppositely arranged and synchronizing moving, a pair of of X-direction push rod 2 and a pair of of Y direction
Push rod 3 is driven by power and transmission mechanism and realizes movement, the pair of X-direction push rod 2 two push rods (push rod 21,
Push rod 22) on be respectively equipped with two claws 4, each claw 4 includes a collet 41, and each collet 41 has arc card pressure surface
411, charging electrode is equipped on each arc card pressure surface.
In other alternative embodiments, claw, the quantity of claw can also be set on a pair of of Y direction push rod 3
It can also be the other quantity other than two, furthermore may be arranged as only a part claw and be equipped with charging electrode, and it is remaining
A part be not provided with charging electrode.
In the present embodiment, the power of the pair of X-direction push rod 2 and transmission mechanism include two groups of belt wheels, two biographies
Dynamic 6, power sources 7 of band, two groups of belt wheels are separately positioned on the opposite two sides of airplane parking area 1, and the side of the airplane parking area is
Perpendicular side, the both ends of every X-direction push rod are separately fixed at the two sides of airplane parking area 1 with the X-direction push rod 2
Transmission belt on, and the end positioned at same side of two X-direction push rods is separately positioned on the upper half of the side transmission belt
Portion and lower half.Wherein, first group of belt wheel includes first pulley 51, the second belt wheel 52, second group of belt wheel include third belt wheel 53,
4th belt wheel 54, the power source 7 drive the first pulley 51, and the first pulley 51 drives described the by transmission belt 6
The rotation of two belt wheels 52, second belt wheel 52 drive the third belt wheel 53 to rotate by a long axis 8, and the third belt wheel 53 is logical
It crosses another transmission belt 6 and drives the 4th belt wheel 54.In the present embodiment, two X-direction push rods use the same power source
7, and synchronizing moving is realized by the combination drive mechanism of above-mentioned belt wheel, transmission belt and long axis.Above the named first pulley,
Second belt wheel, third belt wheel, first, second, third, fourth in the 4th belt wheel are used only as distinguishing, without limitation.
In other embodiments, the power of the pair of X-direction push rod and transmission mechanism can also include being more than one
A power source is arranged in a power source, i.e. every X-direction push rod, can be according to need in the transmission mechanism of every X-direction push rod
The belt wheel of other sets of numbers and the transmission belt of other quantity covered on every group of belt wheel are set with actual conditions.
In the present embodiment, the power of the pair of Y direction push rod 3 and transmission mechanism include two screw rod 14, four
9, power sources 7 of sliding block, two screw rods 14 are arranged in the opposite two sides of airplane parking area 1, the side of the airplane parking area 1 be with
The perpendicular side of the Y direction push rod 3, the both ends of every Y direction push rod 3 are separately fixed on the sliding block of two sides；Often
Root screw rod 14 is equipped with the opposite two sections of screw threads (thread segment 141, thread segment 142) of hand of spiral, the driving of power source 7 first
Root screw rod 14, first screw rod 14 rotation then drive two sliding blocks 9 mounted thereto to move towards or be away from each other shifting
Dynamic, transmission, and then described first are realized by synchronous belt 10 in the end of the axis of first screw rod 14 and second screw rod 14
Root screw rod 14 drives second screw rod 14 to rotate, then two sliding blocks 9 on second screw rod 14 move towards or
It is away from each other movement.Make two Y direction push rods using the same power source 7, and passes through the group of above-mentioned screw rod, sliding block and synchronous belt
Drive mechanism is closed, the synchronizing moving of two Y direction push rods is realized.
In other embodiments, the power of the pair of Y direction push rod and transmission mechanism can also include being more than one
A power source is arranged in a power source, i.e. every Y direction push rod, and the quantity of screw rod and the quantity of screw rod top shoe can be according to need
It is deformed and is replaced.
In the present embodiment, the both ends of the X-direction push rod 2 by multiple connectors 11 be installed with a power source 7 and
One screw rod 14, meanwhile, the claw 4 being arranged on the X-direction push rod 2 contacts or connects with some of connectors 11
It connects, the screw rod 14 is equipped with thread segment, when above-mentioned power source 7 drives the screw rod 14 to rotate, contacts or connects with the claw 4
The some connectors 11 connect can be slided along the screw rod 14, and then the claw 4 is driven to move along X-direction push rod 2
It is dynamic.The structure can be such that two claws 4 at both ends promote from two sides to centre, to clamp unmanned plane undercarriage.
In the present embodiment, it is also equipped with elastic element (not shown), specially spring after the claw 4, described
Elastic element triggers a microswitch when being compressed to predetermined deformation quantity, so make drive claw 4 along the x axis push rod 2 promote
Power source 7 stops.The elastic element and microswitch structure guarantee the contact force of claw 4 and unmanned plane undercarriage top electrode.
In the present embodiment, multiple power sources 7 are stepper motor.
In the embodiment of other deformations, the synchronization band structure of above-described embodiment can be replaced with chain drive, tool
The structure of body is that those skilled in the art can replace according to prior art knowledge, is not detailed and is unfolded herein.
Referring to Figure 1 and Fig. 2, the present embodiment also provide a kind of unmanned plane shutdown library comprising airplane parking area, and be equipped with above-mentioned
Any unmanned plane is reformed and clamping device.
In the present embodiment, the middle part of the airplane parking area 1 is equipped with to positive guidance mark, and described includes one to positive guidance mark
Circular contour mark and the I-shaped mark in circular contour mark.
In the present embodiment, the back side of the airplane parking area 1 is equipped with several structural reinforcement members 13.
In the present embodiment, the structural reinforcement member 13 is rod-shaped, and is two reinforcing rods being parallel to each other, Mei Gejia
The both ends of strong bar are connected in two long sides of the airplane parking area 1.
In other embodiments, the shape, quantity and relative positional relationship of structural reinforcement member can also be in above structures
On the basis of deformed, or use other reinforcement structures commonly used in the art, the diagram of the utility model and above-mentioned retouch
It states and restriction is not made to the shape of structural reinforcement member, quantity and relative positional relationship.
Fig. 6 is referred to, after unmanned plane 15 is parked on airplane parking area 1, two X-direction push rods 21,22 and two Y directions
Push rod 31,32 is promoted to 1 middle position of airplane parking area, and is pressed against on the undercarriage of unmanned plane 15, and Fig. 7 is referred to, meanwhile, connection
The arc card pressure surface 411 for the claw 4 being arranged on two X-direction push rods 21,22 is against in the vertical bar of unmanned plane undercarriage,
Also, the charging structure being correspondingly arranged in the vertical bar of the charging electrode being arranged on arc card pressure surface 411 and unmanned plane undercarriage
Cooperation, charges to unmanned plane 15.
A kind of unmanned plane provided by the utility model is reformed can be to the unmanned plane dropped on airplane parking area with clamping device
It is pushed away just, positive (groined type pushes away just) is pushed away by X-direction a pair of push rods and the realization of Y direction a pair of push rods automatically, and ensure that
The synchronism of two push rods movement in one group of push rod, while the vertical charging claw for clamping unmanned plane under-chassis is additionally used, with
Existing laterally clamping is compared, and another method of clamping is successfully realized.
Disclosed above is only the preferred embodiment in the utility model.There is no all thin of detailed descriptionthe for preferred embodiment
Section, also not limiting the utility model is only the specific embodiment.Obviously, according to the content of this specification, can make very much
Modifications and variations.These embodiments are chosen and specifically described to this specification, is the original in order to preferably explain the utility model
Reason and practical application, so that one of ordinary skill in the art be enable to utilize the utility model well.The utility model is only by right
The limitation of claim and its full scope and equivalent.
Claims (10)
1. the unmanned plane that a kind of unmanned plane shuts down library is reformed and clamping device, which is characterized in that main includes being arranged in airplane parking area
On a pair of of X-direction push rod and a pair of of Y direction push rod, two push rods of a pair of of X-direction push rod be oppositely arranged
And synchronizing moving, two push rods of a pair of of Y direction push rod are oppositely arranged and synchronizing moving, a pair of of X-axis side
It is driven to push rod and a pair of of Y direction push rod by power and transmission mechanism and realizes movement, in the pair of X-direction push rod
Or several claws are respectively equipped on two push rods of the pair of Y direction push rod, at least one described card of each push rod
Pawl is equipped with charging electrode.
2. the unmanned plane that unmanned plane according to claim 1 shuts down library is reformed and clamping device, which is characterized in that described one
X-direction push rod is driven by independent power and transmission mechanism, the power and transmission mechanism include at least one power source,
At least two groups belt wheel and cover the transmission belt on every group of belt wheel；At least two groups belt wheel is separately positioned on the phase of the airplane parking area
Anti- two sides, the side of the above-mentioned airplane parking area are the sides vertical with the X-direction push rod；Every X-direction pushes away
The both ends of bar are separately fixed on the transmission belt of two sides, and the end part positioned at same side of two X-direction push rods
The upper half and lower half of the side transmission belt are not set.
3. the unmanned plane that unmanned plane according to claim 2 shuts down library is reformed and clamping device, which is characterized in that described one
Power and transmission mechanism to X-direction push rod include two groups of belt wheels, two transmission belts, the first power source, first group of belt wheel packet
Include first pulley, the second belt wheel, second group of belt wheel includes third belt wheel, the 4th belt wheel, described in first power source drive
One belt wheel, the first pulley drive second belt wheel to rotate by transmission belt, and second belt wheel is driven by a long axis
The third belt wheel rotation, the third belt wheel drive the 4th belt wheel by another transmission belt.
4. the unmanned plane that unmanned plane according to claim 1 shuts down library is reformed and clamping device, which is characterized in that described one
Y direction push rod is driven by independent power and transmission mechanism, the power and transmission mechanism include at least one power
The phase of airplane parking area is arranged at least two sliding blocks installed on source, at least two screw rods, every screw rod, at least two screw rods
Anti- two sides, above-mentioned side are the sides vertical with the Y direction push rod, and the both ends of every Y direction push rod are solid respectively
It is scheduled on the sliding block of two sides.
5. the unmanned plane that unmanned plane according to claim 4 shuts down library is reformed and clamping device, which is characterized in that described one
Power and transmission mechanism to Y direction push rod include two screw rods, four sliding blocks, the second power source, and every screw rod is equipped with
The opposite both ends screw thread of hand of spiral, second power source drive, first screw rod, first screw rod rotation drive peace
Two sliding blocks mounted in thereon move towards or are away from each other movement, and the end of the axis of first screw rod and second screw rod is logical
It crosses synchronous belt and realizes transmission, first screw rod drives second screw rod rotation, and then makes on second screw rod
Two sliding blocks move towards or be away from each other movement.
6. the unmanned plane that unmanned plane according to claim 1 shuts down library is reformed and clamping device, which is characterized in that the X
It is installed with third power source and a screw rod by multiple connectors on axis direction push rod or the Y direction push rod, meanwhile, setting
The claw on the X-direction push rod or the Y direction push rod is contacted or is connected with some of connectors, described
Screw rod is equipped with thread segment, when the third power source drives screw rod rotation, contact or connect with the claw described in
Some connectors can be slided along the screw rod, and then drive the claw mobile.
7. the unmanned plane that unmanned plane according to claim 6 shuts down library is reformed and clamping device, which is characterized in that the card
Installation has elastic component after pawl, and microswitch, the third power are triggered when the elastic element is compressed to predetermined deformation quantity
Source stops.
8. a kind of unmanned plane shuts down library, which is characterized in that including airplane parking area, and be equipped with any nothing in claim 1-7
It is man-machine to reform and clamping device.
9. the unmanned plane that unmanned plane according to claim 8 shuts down library is reformed and clamping device, which is characterized in that described to stop
The middle part on machine level ground is equipped with to positive guidance mark.
10. the unmanned plane that unmanned plane according to claim 8 shuts down library is reformed and clamping device, which is characterized in that described
The back side of airplane parking area is equipped with several structural reinforcement members, and the structural reinforcement member is rod-shaped, the both ends difference of each structural reinforcement member
It is connected in two long sides of the airplane parking area.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820793716.5U CN208198853U (en) | 2018-05-25 | 2018-05-25 | The unmanned plane that unmanned plane shuts down library, which is reformed, shuts down library with clamping device and unmanned plane |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820793716.5U CN208198853U (en) | 2018-05-25 | 2018-05-25 | The unmanned plane that unmanned plane shuts down library, which is reformed, shuts down library with clamping device and unmanned plane |
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| CN208198853U true CN208198853U (en) | 2018-12-07 |
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| CN109778725A (en) * | 2019-03-18 | 2019-05-21 | 深圳基原中正工程建设有限公司 | Auto-folder handling can transport formula airplane parking area |
| CN110920432A (en) * | 2019-12-20 | 2020-03-27 | 国网山西省电力公司电力科学研究院 | Unmanned aerial vehicle parking device and unmanned aerial vehicle adapted to same |
| CN110979673A (en) * | 2019-12-18 | 2020-04-10 | 武汉飞流智能技术有限公司 | Unmanned aerial vehicle aligning device |
| CN111026156A (en) * | 2019-12-17 | 2020-04-17 | 北京京东乾石科技有限公司 | Inspection system, method, control device, equipment and storage medium |
| CN112144937A (en) * | 2019-06-27 | 2020-12-29 | 上海复亚智能科技有限公司 | Unmanned aerial vehicle multimachine hangar |
| CN112278309A (en) * | 2020-11-02 | 2021-01-29 | 华北电力大学（保定） | Unmanned aerial vehicle automatic station |
| CN112379683A (en) * | 2020-11-19 | 2021-02-19 | 普宙飞行器科技（深圳）有限公司 | Unmanned aerial vehicle take-off and landing control system and method |
| CN112987768A (en) * | 2021-02-08 | 2021-06-18 | 华软科技股份有限公司 | Unmanned aerial vehicle righting device and orientation righting method |
| CN113815443A (en) * | 2021-09-16 | 2021-12-21 | 星逻人工智能技术(上海)有限公司 | Automatic charging device of unmanned aerial vehicle |
| CN114109107A (en) * | 2021-11-22 | 2022-03-01 | 北京煜邦电力技术股份有限公司 | Unmanned aerial vehicle's lift mechanism and unmanned aerial vehicle hangar of returning to center |
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| CN114275179A (en) * | 2022-01-19 | 2022-04-05 | 上海航天测控通信研究所 | Automatic locking means of unmanned aerial vehicle playback |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN109778725A (en) * | 2019-03-18 | 2019-05-21 | 深圳基原中正工程建设有限公司 | Auto-folder handling can transport formula airplane parking area |
| CN112144937A (en) * | 2019-06-27 | 2020-12-29 | 上海复亚智能科技有限公司 | Unmanned aerial vehicle multimachine hangar |
| CN111026156A (en) * | 2019-12-17 | 2020-04-17 | 北京京东乾石科技有限公司 | Inspection system, method, control device, equipment and storage medium |
| CN110979673A (en) * | 2019-12-18 | 2020-04-10 | 武汉飞流智能技术有限公司 | Unmanned aerial vehicle aligning device |
| CN110920432B (en) * | 2019-12-20 | 2023-07-25 | 国网山西省电力公司电力科学研究院 | Unmanned aerial vehicle resident stop device and unmanned aerial vehicle who adapts to it |
| CN110920432A (en) * | 2019-12-20 | 2020-03-27 | 国网山西省电力公司电力科学研究院 | Unmanned aerial vehicle parking device and unmanned aerial vehicle adapted to same |
| CN112278309A (en) * | 2020-11-02 | 2021-01-29 | 华北电力大学（保定） | Unmanned aerial vehicle automatic station |
| CN112379683A (en) * | 2020-11-19 | 2021-02-19 | 普宙飞行器科技（深圳）有限公司 | Unmanned aerial vehicle take-off and landing control system and method |
| CN112987768A (en) * | 2021-02-08 | 2021-06-18 | 华软科技股份有限公司 | Unmanned aerial vehicle righting device and orientation righting method |
| CN113815443A (en) * | 2021-09-16 | 2021-12-21 | 星逻人工智能技术(上海)有限公司 | Automatic charging device of unmanned aerial vehicle |
| CN114109107A (en) * | 2021-11-22 | 2022-03-01 | 北京煜邦电力技术股份有限公司 | Unmanned aerial vehicle's lift mechanism and unmanned aerial vehicle hangar of returning to center |
| CN114228549A (en) * | 2021-12-08 | 2022-03-25 | 海宁量益智能装备有限公司 | Unmanned aerial vehicle location battery charging outfit |
| CN114228549B (en) * | 2021-12-08 | 2024-03-19 | 海宁量益智能装备有限公司 | Unmanned aerial vehicle location battery charging outfit |
| CN114275179A (en) * | 2022-01-19 | 2022-04-05 | 上海航天测控通信研究所 | Automatic locking means of unmanned aerial vehicle playback |
| CN114275179B (en) * | 2022-01-19 | 2023-11-17 | 上海航天测控通信研究所 | Unmanned aerial vehicle automatic locking means that returns to position |
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