CN206163564U - Battery quick assembly disassembly positioning locking device - Google Patents

Battery quick assembly disassembly positioning locking device Download PDF

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Publication number
CN206163564U
CN206163564U CN201621121453.0U CN201621121453U CN206163564U CN 206163564 U CN206163564 U CN 206163564U CN 201621121453 U CN201621121453 U CN 201621121453U CN 206163564 U CN206163564 U CN 206163564U
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CN
China
Prior art keywords
battery
deckle board
screw
briquetting
locking device
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Application number
CN201621121453.0U
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Chinese (zh)
Inventor
兰望娇
王伟
陈心刚
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.)
BEIJING HANGJINGCHUANGXIN TECHNOLOGY Co Ltd
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BEIJING HANGJINGCHUANGXIN TECHNOLOGY Co Ltd
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Priority to CN201621121453.0U priority Critical patent/CN206163564U/en
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    • 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
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/10Energy storage using batteries

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  • Battery Mounting, Suspending (AREA)

Abstract

The utility model discloses a battery quick assembly disassembly positioning locking device belongs to zero technical field of unmanned aerial vehicle, including fixed locking mechanism and battery installation mechanism, fixed locking mechanism includes the bottom plate, and bottom plate upper surface middle part is seted up flutedly, installs unable adjustment base on four angles of bottom plate upper surface respectively, and the last fixed mounting of unable adjustment base has the shell fragment, and the shell fragment upper end is connected with the briquetting, is provided with locking screw on the briquetting, battery installation mechanism includes the screw, go up deckle board and deckle board down, goes up and is provided with the guide block on deckle board and four angles between the deckle board down, and the guide block passes through screw and last deckle board to be connected with deckle board down, upward installs the battery between deckle board and the lower deckle board, and battery installation mechanism passes through the recess and installs in fixing locking mechanism. It has solved the heavy and complicated problem of current unmanned aerial vehicle battery dismouting, makes the dismouting become simple swift to descend in the twinkling of an eye at unmanned aerial vehicle, play effectual guard action to the battery, can satisfy people well to the many -sided requirement of unmanned aerial vehicle battery pack.

Description

A kind of battery fast assembling-disassembling positioning and locking device
Technical field
This utility model belongs to unmanned plane parts technical field, and in particular to a kind of battery fast assembling-disassembling positioning and locking dress Put.
Background technology
UAV referred to as " unmanned plane ", english abbreviation is " UAV ", using radio robot and is provided for oneself The not manned aircraft that presetting apparatus is manipulated.Can be divided into from technical standpoint definition:Unmanned fixed-wing aircraft, unmanned VTOL Machine, unmanned airship, depopulated helicopter, unmanned multi-rotor aerocraft, unmanned parasol etc..With the development of technology, unmanned plane Using increasingly wider, and battery component is the highly important part of unmanned plane, and the fast quick-detach of battery and safety assurance are very It is important.At present, unmanned plane battery holding mechanism is most is fixed using the binding of magic band, and this mode was both unstable or inconvenient Victory, older to fail, it is easy to cause accident due to magic band short life, for SUAV, operation is empty Between it is extremely limited, cause battery to install loaded down with trivial details and be difficult to be installed in place.
Utility model content
This utility model purpose is:A kind of battery fast assembling-disassembling positioning and locking device is aimed to provide, to solve existing nothing The complicated problem of man-machine battery disassembly and assembly, makes dismounting become simple and fast, and lands moment in unmanned plane, and battery is played effectively Protective effect, it is to avoid unnecessary resource waste and pollution, can well meet people many to unmanned plane battery component The requirement of aspect.
To realize above-mentioned technical purpose, the technical solution adopted in the utility model is as follows:
A kind of battery fast assembling-disassembling positioning and locking device, including fixing and locking mechanism and battery holding mechanism, the fixation Retaining mechanism includes base plate, and the base plate is cuboid platy structure, and the plate upper surface middle part opens up fluted, the bottom Plate upper surface is separately installed with firm banking on four angles, and shell fragment, the shell fragment upper end are installed with the firm banking Briquetting is connected with, lock-screw is provided with the briquetting, the briquetting is connected by lock-screw with shell fragment;The battery peace Mounting mechanism includes screw, upper deckle board and lower frame plate, and the upper deckle board and lower frame plate are provided with guide block between four relative angles, institute State guide block to be connected with upper deckle board, lower frame plate by screw, battery, the battery peace are installed between the upper deckle board and lower frame plate Mounting mechanism is arranged in groove and is fixed by fixing and locking mechanism locking.
Using the utility model of the technical program, battery holding mechanism is integral type structure, during installation, by fixed locking machine Shell fragment in structure is strutted laterally respectively, then makes the corresponding notch alignment shell fragment of guide block, and battery holding mechanism press-in is fixed Retaining mechanism, then unclamps shell fragment, and shell fragment drives briquetting to rebound normal position, and briquetting is pushed down battery holding mechanism, installed; During dismounting, shell fragment is strutted laterally respectively, then battery holding mechanism is moved up into taking-up, dismounting is finished.Such knot Structure is designed, and solves the problems, such as that existing unmanned plane battery disassembly and assembly is complicated, makes dismounting become simple and fast, and in unmanned plane landing Moment, the effect of being effectively protected is played to battery, it is to avoid unnecessary resource waste and pollution, can well meet people To many requirements of unmanned plane battery component.
Further limit, briquetting edge rounding.Such structure design, can avoid briquetting from scratching battery.
Further limit, the groove is rectangle.Such structure design, facilitates battery holding mechanism to be fixedly mounted on Determine in retaining mechanism.
Further limit, the screw is interior hexagonal round head screw.Such structure design, has screw and is easy to tightly Gu, dismounting, it is not easy to the advantages of sliding angle.
Further limit, the battery is lithium battery.Such structure design, makes battery have small volume, lightweight, appearance Amount is big, voltage stabilization the advantages of.
Description of the drawings
The nonlimiting examples that this utility model can be given by accompanying drawing are further illustrated;
Fig. 1 is a kind of structural representation of battery fast assembling-disassembling positioning and locking device embodiment of this utility model;
Fig. 2 is the structural representation of fixing and locking mechanism in Fig. 1;
Fig. 3 is the structural representation of battery holding mechanism in Fig. 1;
Main element symbol description is as follows:
1st, firm banking;2nd, briquetting;3rd, lock-screw;4th, base plate;5th, shell fragment;6th, guide block;7th, battery;8th, upper deckle board;9、 Screw;10th, lower frame plate.
Specific embodiment
In order that those skilled in the art may be better understood this utility model, it is right with reference to the accompanying drawings and examples Technical solutions of the utility model are further illustrated.
As shown in Figure 1, Figure 2 and Figure 3, a kind of battery fast assembling-disassembling positioning and locking device of the present utility model, including fixation Retaining mechanism and battery holding mechanism, fixing and locking mechanism include base plate 4, base plate 4 be cuboid platy structure, the upper table of base plate 4 Middle face opens up fluted, and 4 upper surface of base plate is separately installed with firm banking 1 on four angles, is installed with firm banking 1 Shell fragment 5, the upper end of shell fragment 5 is connected with briquetting 2, and lock-screw 3 is provided with briquetting 2, and briquetting 2 is connected by lock-screw 3 with shell fragment 5 Connect;Battery holding mechanism includes screw 9, upper deckle board 8 and lower frame plate 10, between four relative angles of upper deckle board 8 and lower frame plate 10 Guide block 6 is provided with, guide block 6 is connected with upper deckle board 8, lower frame plate 10 by screw 9, is provided between upper deckle board 8 and lower frame plate 10 Battery 7, battery holding mechanism is arranged in groove and is fixed by fixing and locking mechanism locking.
In the present embodiment, battery holding mechanism is integral type structure, during installation, by 5 points of shell fragment in fixing and locking mechanism Do not strut laterally, then make the corresponding notch alignment shell fragment 5 of guide block 6, battery holding mechanism is pressed into into fixing and locking mechanism, connect Release shell fragment 5, shell fragment 5 drives briquetting 2 to rebound normal position, briquetting 2 is pushed down battery holding mechanism, installed;During dismounting, Shell fragment 5 is strutted laterally respectively, then battery holding mechanism taking-up is moved up into, dismounting is finished.Such structure design, Solve the problems, such as that existing unmanned plane battery disassembly and assembly is complicated, make dismounting become simple and fast, and land moment in unmanned plane, it is right Battery plays the effect of being effectively protected, it is to avoid unnecessary resource waste and pollution, can well meet people to nobody The many requirements of machine battery component.
It is preferred that the edge rounding of briquetting 2.Such structure design, can avoid briquetting 2 from scratching battery.In fact, also may be used In the way of selecting others to avoid briquetting 2 from scratching battery 7 as the case may be, such as resilient sleeve etc..
It is preferred that groove is rectangle.Such structure design, facilitates battery holding mechanism to be fixedly mounted on fixing and locking mechanism It is interior.In fact, the shape of groove can also be specifically considered according to the shape of lower frame plate 10, to facilitate lower frame plate 10 to be arranged on groove It is interior.
It is preferred that screw 9 is interior hexagonal round head screw.Such structure design, has screw 9 and is easy to fasten, dismantles, no Easily the advantages of sliding angle.In fact, the species of screw 9 can also specifically be considered as the case may be.
Preferred battery 7 is lithium battery.Such structure design, small volume, lightweight, capacity be big, voltage to have battery 7 Stable the advantages of.In fact, the species of battery 7 can also specifically be considered as the case may be.
A kind of battery fast assembling-disassembling positioning and locking device that this utility model is provided is described in detail above.Specifically The explanation of embodiment is only intended to help and understands method of the present utility model and its core concept.It should be pointed out that for this technology For the those of ordinary skill in field, on the premise of without departing from this utility model principle, this utility model can also be carried out Some improvement and modification, these are improved and modification is also fallen in this utility model scope of the claims.

Claims (5)

1. a kind of battery fast assembling-disassembling positioning and locking device, it is characterised in that:Including fixing and locking mechanism and battery holding mechanism, The fixing and locking mechanism includes base plate (4), and the base plate (4) is cuboid platy structure, base plate (4) upper surface middle part Open up fluted, firm banking (1) is separately installed with described four angles of base plate (4) upper surface, it is solid on the firm banking (1) Dingan County is equipped with shell fragment (5), and shell fragment (5) upper end is connected with briquetting (2), on the briquetting (2) lock-screw (3) is provided with, The briquetting (2) is connected by lock-screw (3) with shell fragment (5);The battery holding mechanism includes screw (9), upper deckle board (8) With lower frame plate (10), the upper deckle board (8) and lower frame plate (10) are provided with guide block (6), the guide block between four relative angles (6) it is connected with upper deckle board (8), lower frame plate (10) by screw (9), is provided between the upper deckle board (8) and lower frame plate (10) Battery (7), the battery holding mechanism is arranged in groove and is fixed by fixing and locking mechanism locking.
2. a kind of battery fast assembling-disassembling positioning and locking device according to claim 1, it is characterised in that:The briquetting (2) Edge rounding.
3. a kind of battery fast assembling-disassembling positioning and locking device according to claim 2, it is characterised in that:The groove is square Shape.
4. a kind of battery fast assembling-disassembling positioning and locking device according to claim 3, it is characterised in that:The screw (9) For interior hexagonal round head screw.
5. a kind of battery fast assembling-disassembling positioning and locking device according to claim 4, it is characterised in that:The battery (7) For lithium battery.
CN201621121453.0U 2016-10-13 2016-10-13 Battery quick assembly disassembly positioning locking device Active CN206163564U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201621121453.0U CN206163564U (en) 2016-10-13 2016-10-13 Battery quick assembly disassembly positioning locking device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201621121453.0U CN206163564U (en) 2016-10-13 2016-10-13 Battery quick assembly disassembly positioning locking device

Publications (1)

Publication Number Publication Date
CN206163564U true CN206163564U (en) 2017-05-10

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112224399A (en) * 2020-09-30 2021-01-15 北京卫通新科测控技术有限公司 Tilting composite wing unmanned aerial vehicle convenient for battery replacement

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112224399A (en) * 2020-09-30 2021-01-15 北京卫通新科测控技术有限公司 Tilting composite wing unmanned aerial vehicle convenient for battery replacement
CN112224399B (en) * 2020-09-30 2022-04-05 北京卫通新科测控技术有限公司 Tilting composite wing unmanned aerial vehicle convenient for battery replacement

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GR01 Patent grant
GR01 Patent grant
PE01 Entry into force of the registration of the contract for pledge of patent right
PE01 Entry into force of the registration of the contract for pledge of patent right

Denomination of utility model: A locking device for quick disassembly and assembly of battery

Effective date of registration: 20200820

Granted publication date: 20170510

Pledgee: Beijing Yanhong Financing Guarantee Co.,Ltd.

Pledgor: BEIJING HANGJING INNOVATION SCIENCE & TECHNOLOGY Co.,Ltd.

Registration number: Y2020990001003

PC01 Cancellation of the registration of the contract for pledge of patent right
PC01 Cancellation of the registration of the contract for pledge of patent right

Date of cancellation: 20210824

Granted publication date: 20170510

Pledgee: Beijing Yanhong Financing Guarantee Co.,Ltd.

Pledgor: BEIJING HANGJING INNOVATION SCIENCE & TECHNOLOGY Co.,Ltd.

Registration number: Y2020990001003

PE01 Entry into force of the registration of the contract for pledge of patent right

Denomination of utility model: A fast disassembly, positioning and locking device for battery

Effective date of registration: 20210924

Granted publication date: 20170510

Pledgee: Beijing Yanhong Financing Guarantee Co.,Ltd.

Pledgor: BEIJING HANGJING INNOVATION SCIENCE & TECHNOLOGY Co.,Ltd.

Registration number: Y2021990000876

PE01 Entry into force of the registration of the contract for pledge of patent right
PC01 Cancellation of the registration of the contract for pledge of patent right
PC01 Cancellation of the registration of the contract for pledge of patent right

Date of cancellation: 20230105

Granted publication date: 20170510

Pledgee: Beijing Yanhong Financing Guarantee Co.,Ltd.

Pledgor: BEIJING HANGJING INNOVATION SCIENCE & TECHNOLOGY CO.,LTD.

Registration number: Y2021990000876

PE01 Entry into force of the registration of the contract for pledge of patent right
PE01 Entry into force of the registration of the contract for pledge of patent right

Denomination of utility model: A quick disassembly, positioning and locking device for battery

Effective date of registration: 20230214

Granted publication date: 20170510

Pledgee: Beijing Yanhong Financing Guarantee Co.,Ltd.

Pledgor: BEIJING HANGJING INNOVATION SCIENCE & TECHNOLOGY CO.,LTD.

Registration number: Y2023110000065

PC01 Cancellation of the registration of the contract for pledge of patent right
PC01 Cancellation of the registration of the contract for pledge of patent right

Granted publication date: 20170510

Pledgee: Beijing Yanhong Financing Guarantee Co.,Ltd.

Pledgor: BEIJING HANGJING INNOVATION SCIENCE & TECHNOLOGY CO.,LTD.

Registration number: Y2023110000065