CN205554629U - Unmanned aerial vehicle trades battery system - Google Patents

Unmanned aerial vehicle trades battery system Download PDF

Info

Publication number
CN205554629U
CN205554629U CN201620108725.7U CN201620108725U CN205554629U CN 205554629 U CN205554629 U CN 205554629U CN 201620108725 U CN201620108725 U CN 201620108725U CN 205554629 U CN205554629 U CN 205554629U
Authority
CN
China
Prior art keywords
unmanned plane
battery
aerial vehicle
unmanned aerial
platform
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
CN201620108725.7U
Other languages
Chinese (zh)
Inventor
汪正伟
郭帅
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.)
Shandong Xiang Hong Electronic Technology Co., Ltd.
Xiang hung electronic technology (Beijing) Co., Ltd.
Xiang hung electronic technology (Shenzhen) Co., Ltd.
Original Assignee
Beijing Jueyun Electronic Co Ltd
Shenzhen Xianyun Technology Co Ltd
LINYI HI-TECH INDUSTRIAL DEVELOPMENT ZONE XIANGHONG ELECTRONIC TECHNOLOGY Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Beijing Jueyun Electronic Co Ltd, Shenzhen Xianyun Technology Co Ltd, LINYI HI-TECH INDUSTRIAL DEVELOPMENT ZONE XIANGHONG ELECTRONIC TECHNOLOGY Co Ltd filed Critical Beijing Jueyun Electronic Co Ltd
Priority to CN201620108725.7U priority Critical patent/CN205554629U/en
Application granted granted Critical
Publication of CN205554629U publication Critical patent/CN205554629U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Battery Mounting, Suspending (AREA)

Abstract

The utility model relates to an unmanned aerial vehicle system provides unmanned aerial vehicle trades battery system, including the platform that can supply unmanned aerial vehicle to descend, sets up on the platform and has marking of directionality, and the unmanned aerial vehicle below sets up image recognition system, and control unmanned aerial vehicle descends to the platform according to certain direction, unmanned aerial vehicle is last to be equipped with the group battery that the level was pegged graft, and the group battery is fixed with the unmanned aerial vehicle joint, is equipped with relative with this group battery battery device that trades on the platform, trading empty battery jar that the battery device includes that a plurality of pulls out the unmanned aerial vehicle group battery and a plurality of and being equipped with the reserve cell groove that is full of the battery, the inside push -and -pull device that is equipped with of battery jar, unmanned aerial vehicle battery are pulled out back reserve cell groove and are aimed at unmanned aerial vehicle and push the battery. The utility model discloses can utilize image recognition system to descend according to an orientation, realize the battery with trade the battery device to closing, accomplish new waste battery's change save time voluntarily, the dead weight that lightens unmanned aerial vehicle can realize quick replacement, the change process is stable, strong adaptability.

Description

Unmanned plane changes battery system
Technical field
The present invention relates to UAS, be specifically related to unmanned plane and change battery system.
Background technology
Unmanned plane is extremely rapid as a kind of novel aircraft development in recent years, UAS is applied to industry-by-industry and has motility and the high advantage of efficiency.Rotor wing unmanned aerial vehicle mainly uses electric power as power at present, so that the extension of its voyage, a kind of method is to increase the carried charge of battery, and its shortcoming is the weight simultaneously adding battery, makes unmanned plane load become big.Therefore it has been proposed that use charging pile to unmanned plane during flying lands when, unmanned plane to be charged.Disadvantage of this is that and have to wait for the corresponding charging interval, cause service efficiency low.
Summary of the invention
The present invention is to solve that high capacity cell weight is big, the problem of charging pile waiting time length, it is provided that a kind of express delivery unmanned plane being convenient for changing battery entrained by unmanned plane changes battery system.
The present invention realizes by the following technical solutions, unmanned plane changes battery system, including being available for the platform that unmanned plane lands, platform is provided with the sign of directivity, arranging image identification system below unmanned plane, image identification system controls unmanned plane and drops to according to a certain direction on platform;Unmanned plane is provided with the set of cells of horizontal grafting, and set of cells connects and fixes with unmanned plane, and platform is provided with and relative with this set of cells changes cell apparatus;Changing cell apparatus and include several empty battery cases unmanned plane set of cells pulled out and several are equipped with the reserve cell groove of fully charged battery, be provided with push-pull device at fixed inside battery case, after the pull-out of unmanned plane battery, battery is pushed by reserve cell groove alignment unmanned plane.
Preferably, described in change the battery case of cell apparatus in be provided with can the gripping bar of slide anteroposterior, gripping bar is connected with unmanned plane battery pack fixing device.
Preferably, described in change cell apparatus and be divided into upper and lower 2 layers, change cell apparatus and the rotating turret being arranged on platform be rotatably connected.
Preferably, being equipped with the Spring Card of fixing unmanned plane body before and after described platform, Spring Card cross section is L-shaped, and under unmanned plane body, compacting is existing the most fixing, and Spring Card is outwards elastic connects spring assembly.
Preferably, described rotating turret oscilaltion can be arranged and be provided with charging device.
Preferably, described platform is provided with the groove matched with unmanned plane undercarriage.
Preferably, the bottom of described groove is provided with the clip of annular of fixed landing gear.
Preferably, described gripping bar is provided with the retainer slid laterally along it, detachably connectable on rear side of this retainer and set of cells.
The invention have benefit that, it is possible to utilize image identification system to land according to certain orientation, it is achieved battery with change the involutory of cell apparatus, the time is saved in the replacing being automatically performed new used batteries, alleviates the deadweight of unmanned plane, can realize quick-replaceable, Renewal process is stable, strong adaptability.
Accompanying drawing explanation
Fig. 1 overall structure of the present invention schematic diagram;
Fig. 2 present invention changes cell apparatus construction schematic diagram.
1. platform in figure, 2. Spring Card, 3. groove, 31. clips, 34 brackets, 4. change cell apparatus, 41. rotating turrets, 42. chutes, 43. gripping bars, 44. retainers.
Detailed description of the invention
The invention will be further described below in conjunction with the accompanying drawings.
As depicted in figs. 1 and 2, the present invention provides a kind of unmanned plane to change battery system, including being available for the platform 1 that unmanned plane lands, platform 1 is provided with the sign of directivity, image identification system is set below unmanned plane, utilizes sign that unmanned plane is dropped on platform 1 according to a certain direction.The afterbody of unmanned plane is provided with the set of cells of horizontal grafting, and this set of cells and unmanned plane utilize fixing fastening to be connected, and is provided with on the platform 1 and relative with this set of cells changes cell apparatus 4.
If changing empty battery case that cell apparatus 4 includes that unmanned plane set of cells pulls out by dried layer and several being equipped with the reserve cell groove of fully charged battery, empty battery case is relative with unmanned plane battery, the inside of each battery case is provided with along the movable gripping bar 43 of chute 42, gripping bar 43 is provided with the retainer 44 slid laterally along it, on rear side of this retainer 44 and set of cells detachably connectable, it is connected with unmanned plane battery and is pulled out by former unmanned plane battery, and then battery is pushed by reserve cell groove alignment unmanned plane.
In the present embodiment, this push-pull device at fixed is gripping bar 43, driving means slide anteroposterior can be utilized to connect along chute 42, and gripping bar 43 is connected with unmanned plane battery pack fixing device.Changing cell apparatus 4 and be divided into upper and lower 2 layers, entirety, in rectangular structure, is arranged over sky battery case, and lower section is provided with reserve cell groove, changes cell apparatus 4 and the rotating turret 41 being arranged on platform is rotatably connected.When unmanned plane lands, changing cell apparatus and taken out by the battery in unmanned plane, after rotating 180 °, battery is pushed and can complete to change cell process by reserve cell groove.It is highly preferred that rotating turret oscilaltion can be arranged and be provided with charging device.
For the most fixing unmanned plane position when changing battery, avoid moving forward and backward, the Spring Card 2 of fixing unmanned plane body it is equipped with before and after platform 1, Spring Card 2 cross section is L-shaped, presses under unmanned plane body lands, and a limit of Spring Card is depressed, another side slopes inwardly, realizing the fixing of unmanned plane body, when unmanned plane flies away from, the Spring Card outwards elastic spring assembly that connects makes it automatically open up.
In order to limit unmanned plane transverse shifting, platform 1 is provided with the groove 3 matched with unmanned plane undercarriage.Undercarriage is limited in bottom land after unmanned plane lands by this groove, and the bottom of groove is provided with the clip 31 of the annular of fixed landing gear, rotates and realizes fixing undercarriage.
When the present invention works, unmanned plane is according to instruction near platform, and after having directive sign above the image identification system Identification platform below unmanned plane, property is landed according to a certain direction, undercarriage drops in the groove above fixing device, and undercarriage is fixed in groove by clip.During landing body by press under the Spring Card of front and back both sides body is front and back fixed spacing.
After unmanned plane has landed, set of cells and fixing device side to change cell apparatus relative, the cell apparatus that changes of cuboid is arranged above the battery case of sky, and set of cells is taken out with the battery pack fits at unmanned plane rear, then changed cell apparatus 180 degree rotation by clamp device, reserve battery is advanced in the same way unmanned plane cabin, the battery taken out is charged, and replacing completes, and clip is opened, unmanned plane can fly away from, and i.e. completes whole to change cell process.

Claims (8)

1. unmanned plane changes battery system, including the platform being available for unmanned plane landing, it is characterised in that be provided with the sign of directivity on described platform, arranging image identification system below unmanned plane, image identification system controls unmanned plane and drops to according to a certain direction on platform;Unmanned plane is provided with the set of cells of horizontal grafting, and set of cells connects and fixes with unmanned plane, and platform is provided with and relative with this set of cells changes cell apparatus;Changing cell apparatus and include several empty battery cases unmanned plane set of cells pulled out and several are equipped with the reserve cell groove of fully charged battery, be provided with push-pull device at fixed inside battery case, after the pull-out of unmanned plane battery, battery is pushed by reserve cell groove alignment unmanned plane.
Unmanned plane the most according to claim 1 changes battery system, it is characterised in that described in change the battery case of cell apparatus in be provided with can the gripping bar of slide anteroposterior, gripping bar is connected with unmanned plane battery pack fixing device.
Unmanned plane the most according to claim 1 and 2 changes battery system, it is characterised in that described in change cell apparatus and be divided into upper and lower 2 layers, change cell apparatus and the rotating turret being arranged on platform be rotatably connected.
Unmanned plane the most according to claim 3 changes battery system, it is characterized in that, being equipped with the Spring Card of fixing unmanned plane body before and after described platform, Spring Card cross section is L-shaped, under unmanned plane body, compacting is existing the most fixing, and Spring Card is outwards elastic connects spring assembly.
Unmanned plane the most according to claim 3 changes battery system, it is characterised in that described rotating turret oscilaltion can be arranged and be provided with charging device.
Unmanned plane the most according to claim 1 changes battery system, it is characterised in that described platform is provided with the groove matched with unmanned plane undercarriage.
Unmanned plane the most according to claim 6 changes battery system, it is characterised in that the bottom of described groove is provided with the clip of the annular of fixed landing gear.
Unmanned plane the most according to claim 2 changes battery system, it is characterised in that described gripping bar is provided with the retainer slid laterally along it, detachably connectable on rear side of this retainer and set of cells.
CN201620108725.7U 2016-02-03 2016-02-03 Unmanned aerial vehicle trades battery system Active CN205554629U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620108725.7U CN205554629U (en) 2016-02-03 2016-02-03 Unmanned aerial vehicle trades battery system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620108725.7U CN205554629U (en) 2016-02-03 2016-02-03 Unmanned aerial vehicle trades battery system

Publications (1)

Publication Number Publication Date
CN205554629U true CN205554629U (en) 2016-09-07

Family

ID=56821664

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620108725.7U Active CN205554629U (en) 2016-02-03 2016-02-03 Unmanned aerial vehicle trades battery system

Country Status (1)

Country Link
CN (1) CN205554629U (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106483979A (en) * 2016-12-19 2017-03-08 重庆信首科技有限公司 A kind of unmanned aerial vehicle control system for land for growing field crops bird repellent
CN106516138A (en) * 2016-11-16 2017-03-22 华南理工大学广州学院 Automatic battery replacing device for four-rotor aircraft
CN107891991A (en) * 2017-05-11 2018-04-10 天宇科技有限公司 Unmanned plane
CN109733234A (en) * 2019-01-25 2019-05-10 吴清槐 A kind of convenient charging pile that battery is protected of unmanned plane

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106516138A (en) * 2016-11-16 2017-03-22 华南理工大学广州学院 Automatic battery replacing device for four-rotor aircraft
CN106516138B (en) * 2016-11-16 2018-12-11 华南理工大学广州学院 A kind of quadrotor automatic battery replacement device
CN106483979A (en) * 2016-12-19 2017-03-08 重庆信首科技有限公司 A kind of unmanned aerial vehicle control system for land for growing field crops bird repellent
CN107891991A (en) * 2017-05-11 2018-04-10 天宇科技有限公司 Unmanned plane
CN109733234A (en) * 2019-01-25 2019-05-10 吴清槐 A kind of convenient charging pile that battery is protected of unmanned plane
CN109733234B (en) * 2019-01-25 2021-04-20 吴清槐 Unmanned aerial vehicle is with filling electric pile that conveniently protects battery

Similar Documents

Publication Publication Date Title
CN205554629U (en) Unmanned aerial vehicle trades battery system
Suzuki et al. Automatic battery replacement system for UAVs: Analysis and design
CN110770129A (en) Base station and vehicle with same
CN107221972A (en) Mobile charging method and apparatus
CN110785352A (en) System and method for air cargo transportation
CN108945500B (en) Movable landing platform of quad-rotor unmanned aerial vehicle and automatic battery replacement method
EP3705343A1 (en) Quick battery swap system, vehicle-mounted battery transfer method, and vehicle-mounted battery operating platform
CN112389262B (en) Battery changing station and method for changing power battery
CN105691617A (en) Unmanned aerial vehicle express system
CN106130108A (en) A kind of wireless charging stake for unmanned plane GPS fixed point continuation of the journey
CN108033031A (en) Field unmanned flight's platform with solar charging device
CN104943845A (en) Hydrogen energy source airship
CN201998780U (en) Drawing electric vehicle battery rack
CN109229077A (en) The automatic change station of accumulator of electric car
Kocer et al. Uav control in close proximities-ceiling effect on battery lifetime
CN105217057B (en) Intersatellite energy transmission device based on tethered docking
CN205335873U (en) Rotor unmanned aerial vehicle fills electric pile
CN108454806A (en) A kind of self-service rescue storehouse of power lifebuoy
CN207932022U (en) A kind of full-automatic plant protection drone movement depot
CN106516138A (en) Automatic battery replacing device for four-rotor aircraft
CN104714546A (en) Automatic AGV power supply replacement system and control method thereof
CN204481527U (en) The stake of rotor wing unmanned aerial vehicle recharging
RU2696632C1 (en) Station for automatic replacement of accumulators for uncrewed aerial vehicle (uav) and method of its use
CN113043903A (en) Unmanned aerial vehicle battery changes device, unmanned aerial vehicle and system
CN207060418U (en) Unmanned plane charging device

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
C56 Change in the name or address of the patentee
CP01 Change in the name or title of a patent holder

Address after: 276000 Shandong city of Linyi province high tech Zone Technology Park B block road bimonthly

Patentee after: Shandong Xiang Hong Electronic Technology Co., Ltd.

Patentee after: BEIJING JUEYUN ELECTRONIC CO., LTD.

Patentee after: SHENZHEN XIANYUN TECHNOLOGY CO., LTD.

Address before: 276000 Shandong city of Linyi province high tech Zone Technology Park B block road bimonthly

Patentee before: LINYI HI-TECH INDUSTRIAL DEVELOPMENT ZONE XIANGHONG ELECTRONIC TECHNOLOGY CO., LTD.

Patentee before: BEIJING JUEYUN ELECTRONIC CO., LTD.

Patentee before: SHENZHEN XIANYUN TECHNOLOGY CO., LTD.

CB03 Change of inventor or designer information
CB03 Change of inventor or designer information

Inventor after: Mao Youbin

Inventor before: Wang Zhengwei

Inventor before: Guo Shuai

CP01 Change in the name or title of a patent holder
CP01 Change in the name or title of a patent holder

Address after: 276000 Shandong city of Linyi province high tech Zone Technology Park B block road bimonthly

Co-patentee after: Xiang hung electronic technology (Beijing) Co., Ltd.

Patentee after: Shandong Xiang Hong Electronic Technology Co., Ltd.

Co-patentee after: Xiang hung electronic technology (Shenzhen) Co., Ltd.

Address before: 276000 Shandong city of Linyi province high tech Zone Technology Park B block road bimonthly

Co-patentee before: BEIJING JUEYUN ELECTRONIC CO., LTD.

Patentee before: Shandong Xiang Hong Electronic Technology Co., Ltd.

Co-patentee before: SHENZHEN XIANYUN TECHNOLOGY CO., LTD.