CN207360291U - Unmanned plane takes battery system - Google Patents

Unmanned plane takes battery system Download PDF

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Publication number
CN207360291U
CN207360291U CN201721214696.3U CN201721214696U CN207360291U CN 207360291 U CN207360291 U CN 207360291U CN 201721214696 U CN201721214696 U CN 201721214696U CN 207360291 U CN207360291 U CN 207360291U
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CN
China
Prior art keywords
vertical
unmanned plane
clamping device
battery system
battery
Prior art date
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Active
Application number
CN201721214696.3U
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Chinese (zh)
Inventor
杨凌
文朋
冯小淋
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Chaonongli (Zhejiang) Intelligent Technology Co.,Ltd.
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Chengdu Tianqi Technology Co Ltd
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND 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
    • B64F1/00Ground or aircraft-carrier-deck installations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND 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
    • B64F1/00Ground or aircraft-carrier-deck installations
    • B64F1/02Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables
    • AHUMAN NECESSITIES
    • A01AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
    • A01MCATCHING, TRAPPING OR SCARING OF ANIMALS; APPARATUS FOR THE DESTRUCTION OF NOXIOUS ANIMALS OR NOXIOUS PLANTS
    • A01M7/00Special adaptations or arrangements of liquid-spraying apparatus for purposes covered by this subclass
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60LPROPULSION 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
    • B60L53/00Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B60L53/80Exchanging energy storage elements, e.g. removable batteries
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60SSERVICING, CLEANING, REPAIRING, SUPPORTING, LIFTING, OR MANOEUVRING OF VEHICLES, NOT OTHERWISE PROVIDED FOR
    • B60S5/00Servicing, maintaining, repairing, or refitting of vehicles
    • B60S5/06Supplying batteries to, or removing batteries from, vehicles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00Propulsion; Power supply
    • B64U50/10Propulsion
    • B64U50/19Propulsion using electrically powered motors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60LPROPULSION 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
    • B60L2200/00Type of vehicles
    • B60L2200/10Air crafts
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/60Other road transportation technologies with climate change mitigation effect
    • Y02T10/70Energy storage systems for electromobility, e.g. batteries
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/60Other road transportation technologies with climate change mitigation effect
    • Y02T10/7072Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T90/00Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02T90/10Technologies relating to charging of electric vehicles
    • Y02T90/14Plug-in electric vehicles

Landscapes

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

Abstract

It the utility model is related to unmanned plane and take battery system, including gripping body and the lifting gear for moving up and down gripping body, the gripping body includes horizontal mobile mechanism, vertical shift mechanism and the clamping device for clamping battery, the horizontal mobile mechanism is installed on lifting gear, the vertical shift mechanism is installed on horizontal mobile mechanism, and the clamping device is installed in vertical shift mechanism.The utility model is simple in structure, automatically can extract the battery of unmanned plane, convenient and efficient, reduces the workload of operating personnel.

Description

Unmanned plane takes battery system
Technical field
Unmanned air vehicle technique field is the utility model is related to, more particularly to unmanned plane takes battery system.
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 and takes battery system, automatically can extract the battery of unmanned plane, convenient and efficient.
To reach above-mentioned purpose, the technical solution adopted in the utility model is as follows:
Unmanned plane takes battery system, including gripping body and the lifting gear for moving up and down gripping body, institute Stating gripping body includes horizontal mobile mechanism, vertical shift mechanism and the clamping device for clamping battery, described to move horizontally Mechanism is installed on lifting gear, and the vertical shift mechanism, which is installed on horizontal mobile mechanism, makes vertical shift mechanism can be relative to Lifting gear moves horizontally, and the clamping device, which is installed in vertical shift mechanism, makes clamping device can be relative to moving horizontally machine Structure moves up and down.
Further, the lifting gear includes Liang Ge vertical translations mechanism, one installed therein of the gripping body In vertical translation mechanism, the vertical translation mechanism for being provided with gripping body is installed in another vertical translation mechanism.
Further, the stroke of vertical translation mechanism is more than the stroke of vertical shift mechanism.
Further, the clamping device includes horizontally movable two grip blocks, the direction of motion of two grip blocks Conversely to grip or loosen battery.
Further, the clamping device further includes the battery case for placing battery, and the battery case is positioned at two folders Between holding block, each grip block is equipped with least one clamp arm, the side wall of the battery case be equipped with for clamp arm horizontal through it is logical Hole, the grip block can be moved horizontally relative to battery case.
It is further preferred that the clamping device includes two battery cases, there are two clamp arm on each grip block, it is same Two clamp arm on grip block are matched with two battery cases respectively.
Wherein, the direction of motion of the grip block and the direction of motion of horizontal mobile mechanism are vertical.
Wherein, the vertical translation mechanism, horizontal mobile mechanism, vertical shift mechanism and clamping device drive by cylinder It is dynamic.
Further, the horizontal mobile mechanism, vertical shift mechanism and clamping device are slider cylinder.
It is further preferred that the vertical shift mechanism includes two vertical slider cylinders, one of them vertical slide unit gas Cylinder is installed on the slide unit of another vertical slider cylinder.
Wherein, the vertical shift mechanism has two.
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 lifting gear;
Fig. 3 is the partial schematic diagram of lifting gear;
Fig. 4 is the structure diagram of gripping body;
Fig. 5 is the structure diagram of gripping body when battery case is not shown;
Fig. 6 is schematic diagram when first level slider cylinder is installed on the 3rd installing plate;
Fig. 7 is the structure diagram of unmanned plane landing gear;
Fig. 8 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, 3- gripping bodies, 4- batteries, 5- landing are flat Platform, the first installing plates of 11-, the second installing plates of 12-, the first vertical guide posts of 13-, 14- rectangle frames, the first cylinders of 15-, 16- first Bearing, the 3rd installing plates of 21-, the second vertical guide posts of 22-, the second cylinders of 23-, 24- second bearings, lower plate, 31- first in 25- Vertical the 4th installing plate of slider cylinder B, 34- of vertical slider cylinder A, 33- of horizontal sliding table cylinder, 32-, 35- battery cases, 36- folders Hold block, 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.
Embodiment 1
As shown in Figure 1, unmanned plane disclosed in the present embodiment takes battery system, including gripping body 3 and for making gripping The lifting gear that mechanism 3 moves up and down, the gripping body 3 include horizontal mobile mechanism, vertical shift mechanism and for clamping The clamping device of battery, the horizontal mobile mechanism are installed on lifting gear, and the vertical shift mechanism is installed on horizontal move Motivation Gou Shi vertical shifts mechanism can be moved horizontally relative to lifting gear, and the clamping device is installed in vertical shift mechanism Clamping device is set to be moved up and down relative to horizontal mobile mechanism.
To increase path increment, lifting gear includes Liang Ge vertical translations mechanism, one installed therein of the gripping body In vertical translation mechanism, the vertical translation mechanism for being provided with gripping body is installed in another vertical translation mechanism.
As shown in Figure 1, 2, lifting gear includes the first vertical translation mechanism 1 and the second vertical translation mechanism 2, and first is vertical Translation mechanism 1 include the first installing plate 11, the second installing plate 12, rectangle frame 14, for drive the second installing plate 12 vertically move The first cylinder 15 and four first vertical guide posts 13, first vertical 13 lower end of guide post and the first installing plate 11 are affixed, There is the through hole A of 13 clearance fit of guide post vertical with first on two installing plates 12, and guide post vertical with first is installed at through hole A The clutch shaft bearing 16 of 13 adaptations, the first vertical 13 upper end of guide post is affixed through clutch shaft bearing 16 and rectangle frame 14, and four first hang down Straight guide post 13 is separately positioned on four vertex of same rectangle, and the first cylinder 15 is installed on the first installing plate 11, and first The output terminal of cylinder 15 is connected with the second installing plate 12, and the second vertical translation mechanism 2 is installed on the second installing plate 12, four pieces the One vertical guide post 13 and rectangle frame 14 is located at the periphery of the second vertical translation mechanism 2.
Second vertical translation mechanism 2 includes the 3rd installing plate 21, vertically moved for the 3rd installing plate 21 of driving second Cylinder 23 and four second vertical guide posts 22, the second vertical 22 upper end of guide post and the 3rd installing plate 21 are affixed, the second installing plate 12 On have the through hole B of 22 clearance fit of guide post vertical with second, and that guide post 22 vertical with second is adapted to is installed at through hole B Two bearings 24, the second vertical 22 lower end of guide post pass through second bearing 24, and four second vertical guide posts 22 are separately positioned on same On four vertex of rectangle, the second cylinder 23 is installed on the second installing plate 12.Second cylinder 23 is located at the second installing plate 12 Lower section, the output terminal of the second cylinder 23 pass perpendicularly through the second installing plate 12 and are connected with the 3rd installing plate 21, the work of the second cylinder 23 Stopper rod (not shown in figure can) is directly connected with the 3rd installing plate 21, can also pass through push rod (not shown) and the 3rd installing plate 21 connections.As shown in figure 3, the lower section of the second installing plate 12 is interval with interior lower plate 25, second bearing 24 and interior lower plate 25 are affixed, the Two bearings, 24 lower end passes through interior lower plate 25.
Wherein, the first cylinder 15 has two, and the second cylinder 23 has two, the first installing plate 11, the second installing plate 12 and Three installing plates 21 are rectangular slab.
Gripping body 3 is installed on the 3rd installing plate 21, under the action of the first cylinder 15, the second vertical translation mechanism 2 Moved up and down with gripping body 3 with the second installing plate 12 along the first vertical guide post 13, realize the first order lifting of lifting gear. Under the action of second cylinder 23, the 3rd installing plate 21 and gripping body 3 are moved up and down relative to the first vertical translation mechanism 1, real The second level lifting of existing lifting gear.
As shown in Figure 4,5, 6, horizontal mobile mechanism is installed on the 3rd installing plate 21, and horizontal mobile mechanism includes the first water Somoothing board cylinder 31, vertical shift mechanism include vertical slider cylinder A32 and vertical slider cylinder B33, first level slide unit gas Cylinder 31 is installed on the 3rd installing plate 21, and vertical slider cylinder A32 is installed on the slide unit of first level slider cylinder 31, vertically Moving mechanism has two, and Liang Ge vertical shifts mechanism is respectively arranged on the both sides of 31 slide unit of first level slider cylinder.Vertical slide unit Cylinder B33 is on the slide unit of vertical slider cylinder A32, and clamping device is on the slide unit of vertical slider cylinder B33.
Clamping device includes the 4th installing plate 34,35, two grip blocks 36 of battery case for placing battery and difference Two horizontal sliding table cylinder A of two grip blocks 36 are driven, grip block 36 is on the slide unit of horizontal sliding table cylinder A;It is described Battery case 35 is installed on the 4th installing plate 34, and the 4th installing plate 34 is installed on the slide unit of two vertical slider cylinder B33, and two A second horizontal sliding table cylinder is separately mounted on the slide unit of two vertical slider cylinder B33.The battery case 35 is located at two Between grip block 36, each grip block 36 is equipped with least one clamp arm 37, and the side wall of the battery case 35, which is equipped with, supplies clamp arm 37 Horizontal through through hole, the direction of motion of two grip blocks 36 is conversely to grip or loosen battery.Clamp arm 37 is cylinder, its Axis is parallel with horizontal plane.
Second horizontal sliding table cylinder 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, There is the sliding slot 38 being adapted to grip block 36 on 4th installing plate 34.The direction of motion of grip block and first level slider cylinder The sliding motion direction of 31 slide unit is vertical.
As shown in fig. 7, 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 gripping body 3 rise to certain altitude, then horizontal sliding table cylinder B31, vertical slider cylinder A32 and Vertical slider cylinder B33 successively actions make the 4th installing plate 34 of clamping device be moved to immediately below battery 4, at this time, 4 bottom of battery Portion 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 grip block 36 clampings, clamp arm 37 are inserted into the blind hole of battery 4, and then vertical slider cylinder B33 and vertical slider cylinder A32 successively pull out by action Go out battery 4.
Embodiment 2
As shown in figure 8, 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.
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.
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 (10)

1. unmanned plane takes battery system, it is characterised in that:Including gripping body and the liter for moving up and down gripping body Falling unit, the gripping body includes horizontal mobile mechanism, vertical shift mechanism and the clamping device for clamping battery, described Horizontal mobile mechanism is installed on lifting gear, and the vertical shift mechanism, which is installed on horizontal mobile mechanism, makes vertical shift mechanism It can be moved horizontally relative to lifting gear, the clamping device, which is installed in vertical shift mechanism, makes clamping device can be relative to water Flat moving mechanism moves up and down.
2. unmanned plane according to claim 1 takes battery system, it is characterised in that:The lifting gear includes two vertically Translation mechanism, in a gripping body vertical translation mechanism installed therein, is provided with the vertical translation machine of gripping body Structure is installed in another vertical translation mechanism.
3. unmanned plane according to claim 2 takes battery system, it is characterised in that:The stroke of vertical translation mechanism is more than perpendicular The stroke of straight moving mechanism.
4. unmanned plane according to claim 1 takes battery system, it is characterised in that:The clamping device includes horizontal moving Two dynamic grip blocks, the direction of motion of two grip blocks is conversely to grip or loosen battery.
5. unmanned plane according to claim 4 takes battery system, it is characterised in that:The clamping device is further included for putting The battery case of battery is put, for the battery case between two grip blocks, each grip block is equipped with least one clamp arm, described The side wall of battery case be equipped with for clamp arm horizontal through through hole, the grip block can move horizontally relative to battery case.
6. unmanned plane according to claim 5 takes battery system, it is characterised in that:The clamping device includes two batteries Box, there is two clamp arm on each grip block, and two clamp arm on same grip block are matched with two battery cases respectively.
7. unmanned plane according to claim 3 takes battery system, it is characterised in that:The vertical translation mechanism, horizontal shifting Motivation structure, vertical shift mechanism and clamping device are driven by the cylinder.
8. unmanned plane according to claim 7 takes battery system, it is characterised in that:The horizontal mobile mechanism, vertical shifting Motivation structure and clamping device are slider cylinder.
9. unmanned plane according to claim 8 takes battery system, it is characterised in that:The vertical shift mechanism includes two Vertical slider cylinder, one of them vertical slider cylinder are installed on the slide unit of another vertical slider cylinder.
10. the unmanned plane according to claim 1 or 9 takes battery system, it is characterised in that:The vertical shift mechanism has two It is a.
CN201721214696.3U 2017-05-19 2017-09-20 Unmanned plane takes battery system Active CN207360291U (en)

Applications Claiming Priority (2)

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

Publications (1)

Publication Number Publication Date
CN207360291U true CN207360291U (en) 2018-05-15

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ID=61114025

Family Applications (10)

Application Number Title Priority Date Filing Date
CN201721214696.3U Active CN207360291U (en) 2017-05-19 2017-09-20 Unmanned plane takes battery system
CN201710851229.XA Active CN107719329B (en) 2017-05-19 2017-09-20 Unmanned aerial vehicle support system
CN201721205974.9U Active CN207141422U (en) 2017-05-19 2017-09-20 A kind of unmanned plane landing platform
CN201721205975.3U Active CN207243451U (en) 2017-05-19 2017-09-20 A kind of medicine-filling device
CN201710851248.2A Expired - Fee Related CN107697314B (en) 2017-05-19 2017-09-20 Unmanned aerial vehicle take-off and landing 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
CN201721211872.8U Active CN207360600U (en) 2017-05-19 2017-09-20 Unmanned plane battery grips mechanism action device
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

Family Applications After (9)

Application Number Title Priority Date Filing Date
CN201710851229.XA Active CN107719329B (en) 2017-05-19 2017-09-20 Unmanned aerial vehicle support system
CN201721205974.9U Active CN207141422U (en) 2017-05-19 2017-09-20 A kind of unmanned plane landing platform
CN201721205975.3U Active CN207243451U (en) 2017-05-19 2017-09-20 A kind of medicine-filling device
CN201710851248.2A Expired - Fee Related CN107697314B (en) 2017-05-19 2017-09-20 Unmanned aerial vehicle take-off and landing 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
CN201721211872.8U Active CN207360600U (en) 2017-05-19 2017-09-20 Unmanned plane battery grips mechanism action device
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

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CN (10) CN207360291U (en)

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CN208344548U (en) * 2018-03-14 2019-01-08 深圳市大疆创新科技有限公司 A kind of positioning mechanism and unmanned plane landing platform
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CN108631403A (en) * 2018-05-28 2018-10-09 天津大学 A kind of storage battery storehouse system that wireless charging can be carried out to battery
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CN108725245B (en) * 2018-05-30 2023-06-23 西安工业大学 Battery replacement system and replacement method of aircraft
CN108482697B (en) * 2018-06-06 2023-09-19 深圳草莓创新技术有限公司 Unmanned aerial vehicle automatic positioning charging device and method thereof
CN108569262A (en) * 2018-06-21 2018-09-25 长春草莓科技有限公司 A kind of unmanned plane replaces battery, Wrap device automatically
CN110673625B (en) * 2018-07-02 2023-05-23 中光电智能机器人股份有限公司 Unmanned aerial vehicle monitoring system, base station and control method
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CN109050293A (en) * 2018-07-28 2018-12-21 深圳市烽焌信息科技有限公司 A kind of continuation of the journey base station applied to unmanned plane
CN211223917U (en) * 2018-07-30 2020-08-11 魏荣亮 Landing device for vertical lifting aircraft and ship
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