CN207360602U - Unmanned plane battery gripping body - Google Patents

Unmanned plane battery gripping body Download PDF

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Publication number
CN207360602U
CN207360602U CN201721214766.5U CN201721214766U CN207360602U CN 207360602 U CN207360602 U CN 207360602U CN 201721214766 U CN201721214766 U CN 201721214766U CN 207360602 U CN207360602 U CN 207360602U
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CN
China
Prior art keywords
cylinder
clamp arm
unmanned plane
horizontal sliding
sliding table
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
Application number
CN201721214766.5U
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Chinese (zh)
Inventor
杨凌
文朋
冯小淋
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Chaonongli (Zhejiang) Intelligent Technology Co.,Ltd.
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Chengdu Tianqi Technology Co Ltd
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Publication of CN207360602U publication Critical patent/CN207360602U/en
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Classifications

    • 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
    • B64F1/02—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables
    • 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
    • A—HUMAN NECESSITIES
    • A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
    • A01M—CATCHING, TRAPPING OR SCARING OF ANIMALS; APPARATUS FOR THE DESTRUCTION OF NOXIOUS ANIMALS OR NOXIOUS PLANTS
    • A01M7/00—Special adaptations or arrangements of liquid-spraying apparatus for purposes covered by this subclass
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B60L53/80—Exchanging energy storage elements, e.g. removable batteries
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60S—SERVICING, CLEANING, REPAIRING, SUPPORTING, LIFTING, OR MANOEUVRING OF VEHICLES, NOT OTHERWISE PROVIDED FOR
    • B60S5/00—Servicing, maintaining, repairing, or refitting of vehicles
    • B60S5/06—Supplying batteries to, or removing batteries from, vehicles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/19—Propulsion using electrically powered motors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L2200/00—Type of vehicles
    • B60L2200/10—Air crafts
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/60—Other road transportation technologies with climate change mitigation effect
    • Y02T10/70—Energy storage systems for electromobility, e.g. batteries
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/60—Other road transportation technologies with climate change mitigation effect
    • Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02T90/10—Technologies relating to charging of electric vehicles
    • Y02T90/14—Plug-in electric vehicles

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Chemical & Material Sciences (AREA)
  • Transportation (AREA)
  • Zoology (AREA)
  • Environmental Sciences (AREA)
  • Power Engineering (AREA)
  • Wood Science & Technology (AREA)
  • Pest Control & Pesticides (AREA)
  • Insects & Arthropods (AREA)
  • Catching Or Destruction (AREA)
  • Battery Mounting, Suspending (AREA)
  • Manipulator (AREA)
  • Power-Operated Mechanisms For Wings (AREA)
  • Infusion, Injection, And Reservoir Apparatuses (AREA)
  • Forklifts And Lifting Vehicles (AREA)
  • Platform Screen Doors And Railroad Systems (AREA)

Abstract

It the utility model is related to unmanned plane battery gripping body, including clamping device, clamping device includes the battery case for placing battery, two grip blocks and two horizontal sliding table cylinder A for driving two grip blocks respectively, and grip block is on the slide unit of horizontal sliding table cylinder A；For the battery case between two grip blocks, each grip block is equipped with least one clamp arm, the side wall of the battery case be equipped with supply clamp arm horizontal through through hole.The utility model is simple in structure, convenient and efficient easy to which the battery of unmanned plane is extracted, and reduces the workload of operating personnel.

Description

Unmanned plane battery gripping body
Technical field
It the utility model is related to unmanned air vehicle technique field, more particularly to unmanned plane battery gripping body.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself Not manned aircraft, without cockpit on machine, but the equipment such as automatic pilot, presetting apparatus are installed；It is widely used in aerial Scouting, monitoring, communication, antisubmarine, electronic interferences etc..
With the continuous development of scientific technology, unmanned plane is in an increasingly wide range of applications, such as plant protection unmanned plane, cares for name It is the UAV for agriculture and forestry plant protection operation to think justice, which has flying platform (fixed-wing, Dan Xuan The wing, more rotors), GPS fly control, spraying mechanism three parts composition, fly to control by ground remote control or GPS, can to realize spraying operation To spray medicament, seed, pulvis etc., bring great convenience for live and work.
Existing unmanned plane recycling so can usually use auxiliary often frequently with the mode of block landing or ground landing Instrument needs special messenger to recycle, inefficient.
Unmanned plane needs lasting power supply during plant protection, and unmanned plane maiden takeoff simultaneously detects not enough power supply When, it is necessary to back to charging on base station.Because battery is mounted in the battery compartment of unmanned plane, battery is extracted very manually Trouble, increases the workload of operating personnel.
Utility model content
The utility model aims to provide unmanned plane battery gripping body, automatically can extract the battery of unmanned plane, convenient fast It is prompt.
To reach above-mentioned purpose, the technical solution adopted in the utility model is as follows：
Unmanned plane battery gripping body, including clamping device, clamping device include for placing battery battery case, two Grip block and two horizontal sliding table cylinder A for driving two grip blocks respectively, grip block are installed on the cunning of horizontal sliding table cylinder A On platform；
For the battery case between two grip blocks, each grip block is equipped with least one clamp arm, the battery case Side wall be equipped with for clamp arm horizontal through through hole.
Further, there are two clamp arm on each grip block, two clamp arm are matched with same battery case.
Alternatively, the battery case there are two, there are two clamp arm on each grip block, two clamp arm on same grip block Matched respectively with two battery cases.
Further, clamping device further includes the 4th installing plate, and battery case is installed on the 4th installation plate top surface, horizontal sliding table Cylinder A is located at the lower section of the 4th installing plate, and clamp arm is located at the top of the 4th installing plate, has on the 4th installing plate and grip block The sliding slot of adaptation.
It is further preferred that clamping device further includes movement device, movement device includes horizontal sliding table cylinder B and for dividing Not Dai Dong two horizontal sliding table cylinder A vertical shifts two vertical slider cylinder A, the vertical slider cylinder A is installed on water On the slide unit of somoothing board cylinder B, two vertical slider cylinder A are respectively arranged on the both sides of horizontal sliding table cylinder B slide units.
Further, movement device further includes vertical slider cylinder B, is respectively mounted on the slide unit of two vertical slider cylinder A There are vertical slider cylinder B, two horizontal sliding table cylinder A to be separately mounted on two vertical slider cylinder B.
Wherein, clamp arm is cylinder, and the axis of clamp arm is parallel with horizontal plane.
Compared with prior art, the utility model has the advantages that：
The utility model is simple in structure, automatically can extract the battery of unmanned plane, convenient and efficient, reduces the work of operating personnel Measure.
Brief description of the drawings
Fig. 1 is the structure diagram of embodiment 1；
Fig. 2 is the structure diagram of gripping body；
Fig. 3 is the structure diagram of gripping body when battery case is not shown；
Fig. 4 is the structure diagram of gripping body when battery case is not shown；
Fig. 5 is schematic diagram when horizontal sliding table cylinder B is installed on the 3rd installing plate；
Fig. 6 is the structure diagram of clamping device in embodiment 2；
In figure：The first vertical translations of 1- mechanism, the second vertical translations of 2- mechanism, 4- batteries, 5- landing platforms, 11- first Installing plate, the second installing plates of 12-, the first vertical guide posts of 13-, 14- rectangle frames, the first cylinders of 15-, the 3rd installing plates of 21-, 22- Vertical slider cylinder B, 34- the 4th of second vertical guide post, vertical slider cylinder A, 33- of 31- horizontal sliding table cylinder B, 32- is installed Plate, 35- battery cases, 36- grip blocks, 37- clamp arm, 38- sliding slots.
Embodiment
In order to make the purpose of the utility model, technical solutions and advantages more clearly understood, below in conjunction with attached drawing, to this reality It is further elaborated with new.
As shown in Figure 1, 2, unmanned plane battery gripping body disclosed in the utility model, including clamping device and action fill Put, clamping device two grip blocks 36 of driving including 35, two grip blocks 36 of battery case for placing battery and respectively Two horizontal sliding table cylinder A, grip block 36 is on the slide unit of horizontal sliding table cylinder A；Battery case 35 is located at two grip blocks Between 36, each grip block 36 is equipped with least one clamp arm 37, the side wall of battery case 35 be equipped with for clamp arm 37 horizontal through Through hole.There are two clamp arm 37 on grip block 36, two clamp arm 37 are matched with same battery case 35.Clamp arm 37 is cylinder, is pressed from both sides The axis of arm 37 is parallel with horizontal plane.
Clamping device further includes the 4th installing plate 34, and battery case 35 is installed on 34 top surface of the 4th installing plate, horizontal sliding table gas Cylinder A is located at the lower section of the 4th installing plate 34, and clamp arm 37 is located at the top of the 4th installing plate 34, has and clamp on the 4th installing plate 34 The sliding slot 38 that block 36 is adapted to.
Movement device includes horizontal sliding table cylinder B31, vertical slider cylinder A32 and vertical slider cylinder B33, vertical slide unit Cylinder A32 is on the slide unit of horizontal sliding table cylinder B31, and vertical slider cylinder A32 has two, two vertical slider cylinders A32 is respectively arranged on the both sides of horizontal sliding table cylinder B31 slide units；It is vertical to be mounted on the slide unit of two vertical slider cylinder A32 Slider cylinder B33, two horizontal sliding table cylinder A are separately mounted on two vertical slider cylinder B33.The movement side of grip block 36 It is vertical to the direction of motion of the slide unit with first level slider cylinder 31.
Horizontal sliding table cylinder B31 is installed on lifting gear.As shown in Figure 3,4, lifting gear includes the first vertical translation 1 and second vertical translation mechanism 2 of mechanism, the second vertical translation mechanism 2 are installed in the first vertical translation mechanism 1.First is vertical Translation mechanism 1 includes the first installing plate 11, the second installing plate 12, the first vertical guide post 13 and rectangle frame 14, the first vertical guide post 13 lower ends and the first installing plate 11 are affixed, there is the through hole of 13 clearance fit of guide post vertical with first on the second installing plate 12, and first Vertical 13 upper end of guide post is affixed through the through hole on the second installing plate 12 and rectangle frame 14, and the first vertical guide post 13 has 4,4 First vertical guide post 13 is separately positioned on four vertex of same rectangle, and two the first cylinders 15 are installed on the first installing plate On 11, the output terminal of the first cylinder 15 is connected with the second installing plate 12.Second vertical translation mechanism 2 is installed on the second installing plate 12 On, 4 first vertical guide posts 13 and rectangle frame 14 are located at the periphery of the second vertical translation mechanism 2, under the action of the first cylinder 15, Second vertical translation mechanism 2 is moved up and down with the second installing plate 12 along the first vertical guide post 13, realizes the first order of lifting gear Lifting.
Second vertical translation mechanism 2 includes the 3rd installing plate 21 and the second vertical guide post 22, the second vertical 22 upper end of guide post It is affixed with the 3rd installing plate 21, there is the through hole of 22 clearance fit of guide post vertical with second on the second installing plate 12, second vertically leads 22 lower end of column passes through the through hole, and the second vertical guide post 22 has 4, and 4 second vertical guide posts 22 are separately positioned on same rectangle Four vertex on, two the second cylinders, which are installed on the second installing plate 12, to be used to drive the 3rd installing plate 21 to move up and down.
Second cylinder is located at the lower section of the second installing plate 12, and the output terminal of the second cylinder passes through the second installing plate 12 and the 3rd Installing plate 21 connects, and under the action of the second cylinder, the 3rd installing plate 21 is moved up and down relative to the first vertical guide post 13, realizes The second level lifting of lifting gear.As shown in figure 4, horizontal sliding table cylinder B31 is installed on the 3rd installing plate 21.
As shown in figure 5, being reserved with the convenient window for taking battery 4 away from below on the landing platform 5 of unmanned plane landing gear, make Used time, lifting gear make clamp device 3 rise to certain altitude, and then horizontal sliding table cylinder B31, which starts action, makes vertical slide unit Cylinder A32, vertical slider cylinder B33 and clamping device integral level are moved to the underface of the window of landing platform 5, then perpendicular Straight slider cylinder A32 and vertical slider cylinder B33 successively actions make under the 4th installing plate 34 of clamping device rises to battery 4 just Side, at this time, 4 bottom of battery is located in battery case 35, and two grip blocks 36 are placed exactly in the both sides of battery 4；Then, horizontal sliding table Cylinder A drives 36 clamping of grip block, and clamp arm 37 is inserted into the blind hole of battery 4, then vertical slider cylinder B33 and vertical slide unit gas Cylinder A32 successively actions make clamping device drop to the lower section of landing platform 5 and extract battery 4.
Embodiment 2
As shown in fig. 6, clamping device includes two battery cases 35 in the present embodiment, there are two clamp arm 37 on grip block 36, Two clamp arm 37 on same grip block 36 are matched with two battery cases 35 respectively.When battery is charging on charging rack, side Just two pieces of batteries are disposably taken.
Certainly, the utility model can also have other numerous embodiments, without departing substantially from the utility model spirit and its essence In the case of, those skilled in the art can make various corresponding changes and deformation, but these according to the utility model It is corresponding to change and deform the scope of the claims that all belong to appended by the utility model.

Claims (7)

1. unmanned plane battery gripping body, it is characterised in that:Including clamping device, clamping device includes the electricity for placing battery Pond box (35), two grip blocks (36) and two horizontal sliding table cylinder A for driving two grip blocks (36) respectively, grip block (36) on the slide unit of horizontal sliding table cylinder A；The battery case (35) is between two grip blocks (36), each clamping Block (36) is equipped with least one clamp arm (37), the side wall of the battery case (35) be equipped with for clamp arm (37) horizontal through it is logical Hole.
2. unmanned plane battery gripping body according to claim 1, it is characterised in that：There are two on each grip block (36) Clamp arm (37).
3. unmanned plane battery gripping body according to claim 1, it is characterised in that：The battery case (35) has two, Have two clamp arm (37) on each grip block (36), two clamp arm (37) on same grip block (36) respectively with two batteries Box (35) matches.
4. unmanned plane battery gripping body according to claim 1, it is characterised in that：Clamping device further includes the 4th installation Plate (34), battery case (35) are installed on the 4th installing plate (34) top surface, and horizontal sliding table cylinder A is located under the 4th installing plate (34) Side, clamp arm (37) are located at the top of the 4th installing plate (34), have what is be adapted to grip block (36) on the 4th installing plate (34) Sliding slot (38).
5. unmanned plane battery gripping body according to claim 1, it is characterised in that：Further include movement device, action dress Put including horizontal sliding table cylinder B (31) and for driving two vertical slide units of two horizontal sliding table cylinder A vertical shifts respectively Cylinder A (32), the vertical slider cylinder A (32) is on the slide unit of horizontal sliding table cylinder B (31), two vertical slide unit gas Cylinder A (32) is respectively arranged on the both sides of horizontal sliding table cylinder B (31) slide unit.
6. unmanned plane battery gripping body according to claim 5, it is characterised in that：Movement device further includes vertical slide unit Cylinder B (33), is mounted on vertical slider cylinder B (33), two horizontal sliding tables on the slide unit of two vertical slider cylinder A (32) Cylinder A is separately mounted on two vertical slider cylinder B (33).
7. unmanned plane battery gripping body according to claim 1, it is characterised in that：Clamp arm (37) is cylindrical, clamp arm (37) axis is parallel with horizontal plane.
CN201721214766.5U 2017-05-19 2017-09-20 Unmanned plane battery gripping body Active CN207360602U (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN2017103595169 2017-05-19
CN201710359516 2017-05-19

Publications (1)

Publication Number Publication Date
CN207360602U true CN207360602U (en) 2018-05-15

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ID=61114025

Family Applications (10)

Application Number Title Priority Date Filing Date
CN201721211872.8U Active CN207360600U (en) 2017-05-19 2017-09-20 Unmanned plane battery grips mechanism action device
CN201721205974.9U Active CN207141422U (en) 2017-05-19 2017-09-20 A kind of unmanned plane landing platform
CN201710851248.2A Expired - Fee Related CN107697314B (en) 2017-05-19 2017-09-20 Unmanned aerial vehicle take-off and landing device
CN201721214696.3U Active CN207360291U (en) 2017-05-19 2017-09-20 Unmanned plane takes battery system
CN201721214766.5U Active CN207360602U (en) 2017-05-19 2017-09-20 Unmanned plane battery gripping body
CN201710855244.1A Active CN107640079B (en) 2017-05-19 2017-09-20 Unmanned aerial vehicle endurance guarantee method
CN201721205975.3U Active CN207243451U (en) 2017-05-19 2017-09-20 A kind of medicine-filling device
CN201721208723.6U Active CN207355319U (en) 2017-05-19 2017-09-20 A kind of automatic liquid medicine injection system
CN201710857322.1A Active CN107651205B (en) 2017-05-19 2017-09-20 Unmanned aerial vehicle location battery system
CN201710851229.XA Active CN107719329B (en) 2017-05-19 2017-09-20 Unmanned aerial vehicle support system

Family Applications Before (4)

Application Number Title Priority Date Filing Date
CN201721211872.8U Active CN207360600U (en) 2017-05-19 2017-09-20 Unmanned plane battery grips mechanism action device
CN201721205974.9U Active CN207141422U (en) 2017-05-19 2017-09-20 A kind of unmanned plane landing platform
CN201710851248.2A Expired - Fee Related CN107697314B (en) 2017-05-19 2017-09-20 Unmanned aerial vehicle take-off and landing device
CN201721214696.3U Active CN207360291U (en) 2017-05-19 2017-09-20 Unmanned plane takes battery system

Family Applications After (5)

Application Number Title Priority Date Filing Date
CN201710855244.1A Active CN107640079B (en) 2017-05-19 2017-09-20 Unmanned aerial vehicle endurance guarantee method
CN201721205975.3U Active CN207243451U (en) 2017-05-19 2017-09-20 A kind of medicine-filling device
CN201721208723.6U Active CN207355319U (en) 2017-05-19 2017-09-20 A kind of automatic liquid medicine injection system
CN201710857322.1A Active CN107651205B (en) 2017-05-19 2017-09-20 Unmanned aerial vehicle location battery system
CN201710851229.XA Active CN107719329B (en) 2017-05-19 2017-09-20 Unmanned aerial vehicle support system

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CN (10) CN207360600U (en)

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CN112666965A (en) * 2019-10-15 2021-04-16 应急管理部上海消防研究所 A positioner that is used for unmanned aerial vehicle to trade electricity automatically
CN110733663B (en) * 2019-10-29 2024-02-02 华软科技股份有限公司 Automatic battery replacing device and method for unmanned aerial vehicle
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