CN211879420U - Battery fixing structure for unmanned aerial vehicle - Google Patents

Battery fixing structure for unmanned aerial vehicle Download PDF

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Publication number
CN211879420U
CN211879420U CN201922112755.1U CN201922112755U CN211879420U CN 211879420 U CN211879420 U CN 211879420U CN 201922112755 U CN201922112755 U CN 201922112755U CN 211879420 U CN211879420 U CN 211879420U
Authority
CN
China
Prior art keywords
battery
aerial vehicle
unmanned aerial
rotating seat
battery fixing
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.)
Expired - Fee Related
Application number
CN201922112755.1U
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Chinese (zh)
Inventor
张雷
程军
孙伟
崔磊
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.)
Henan Zhengda Aviation Industry Co ltd
Original Assignee
Henan Zhengda Aviation Industry 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 Henan Zhengda Aviation Industry Co ltd filed Critical Henan Zhengda Aviation Industry Co ltd
Priority to CN201922112755.1U priority Critical patent/CN211879420U/en
Application granted granted Critical
Publication of CN211879420U publication Critical patent/CN211879420U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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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 fixing structure for unmanned aerial vehicle, which comprises a battery fixing table, wherein one end of the battery fixing table is provided with a raised positioning block, the other end of the battery fixing table is symmetrically provided with a rotating seat, the rotating seat is provided with symmetrical blind holes, a rotating shaft is assembled between the two blind holes, two ends of the rotating shaft are assembled with torsional springs, the torsional springs are connected with the bottoms of the blind holes of the rotating seat, and one side of the rotating seat, which is close to a battery, is provided with a clamping groove; the middle part of the rotating shaft is provided with a pressing plate, and one side of the pressing plate, which is close to the battery, is provided with pressing teeth. The utility model discloses rational in infrastructure, can be comparatively convenient fasten fixedly to unmanned aerial vehicle battery box, if need take off the battery box when changing, it is also comparatively convenient to take off, has promoted unmanned aerial vehicle's availability factor greatly.

Description

Battery fixing structure for unmanned aerial vehicle
Technical Field
The utility model relates to an unmanned aerial vehicle, especially a battery fixed knot constructs for unmanned aerial vehicle suitable for large-scale unmanned aerial vehicle.
Background
Present unmanned aerial vehicle's use is comparatively general, but along with some large-scale unmanned aerial vehicle's popularization, the volume of its battery is also bigger, and current battery fixed knot constructs can not satisfy the operation needs completely, and it is comparatively inconvenient to lead to unmanned aerial vehicle's battery to change the operation, and the process can be more complicated, just so need design one kind can satisfy the battery fixed knot structure of unmanned aerial vehicle operation needs.
Disclosure of Invention
The utility model aims at designing a battery fixed knot constructs for unmanned aerial vehicle rational in infrastructure, use convenient.
The technical scheme of the utility model, a battery fixed knot constructs for unmanned aerial vehicle, it includes the battery fixed station, its characterized in that: a protruding positioning block is arranged at one end of the battery fixing table, a rotating seat is symmetrically arranged at the other end of the battery fixing table, symmetrical blind holes are formed in the rotating seat, a rotating shaft is assembled between the two blind holes, torsion springs are assembled at two ends of the rotating shaft, the torsion springs are connected with the bottoms of the blind holes of the rotating seat, and a clamping groove is formed in one side, close to the battery, of the rotating seat; the middle part of the rotating shaft is provided with a pressing plate, and one side of the pressing plate, which is close to the battery, is provided with pressing teeth.
The shape of the protruding positioning block is matched with a positioning hole reserved at the bottom of the battery box body.
The size of the clamping groove is matched with the size of a clamping column reserved at the bottom of the battery box body.
The utility model has the advantages that: its is rational in infrastructure, can be comparatively convenient fasten fixedly to unmanned aerial vehicle battery box, if need take off the battery box when changing, it is also comparatively convenient to take off, has promoted unmanned aerial vehicle's availability factor greatly.
Drawings
Fig. 1 is a schematic view of the overall structure of the present invention.
Fig. 2 is a schematic structural diagram of the battery box of the present invention after being installed.
Fig. 3 is a schematic structural view of the battery box of the present invention after being taken down.
Detailed Description
In order to make the objects and technical solutions of the present invention more clearly understood, the present invention will be described in detail with reference to the accompanying drawings and the following detailed description. It should be understood that the detailed description and specific examples, while indicating the invention, are given by way of illustration only.
A battery fixing structure for an unmanned aerial vehicle comprises a battery fixing table 1, wherein a protrusion positioning block 3 is arranged at one end of the battery fixing table, a rotating seat 4 is symmetrically arranged at the other end of the battery fixing table, symmetrical blind holes are formed in the rotating seat, a rotating shaft 5 is assembled between the two blind holes, torsion springs are assembled at two ends of the rotating shaft, the torsion springs are connected with the bottoms of the blind holes of the rotating seat, and a clamping groove 9 is formed in one side, close to a battery, of the rotating seat; the middle part of the rotating shaft is provided with a pressing plate 7, and one side of the pressing plate close to the battery is provided with pressing teeth 6.
The shape of the raised positioning block is matched with a positioning hole reserved at the bottom of the battery box body 2.
The size of the clamping groove is matched with the size of a clamping column 10 reserved at the bottom of the battery box body 2.
When the utility model is used, the battery box body is positioned by utilizing the raised positioning block, and the end part of the positioning block is clamped into the positioning hole reserved at the bottom of the battery box body; the pressing plate is pressed afterwards, then the clamping columns reserved at the bottom of the battery box body are clamped into the clamping grooves, then the pressing plate is put down, the pressing teeth can press the clamping columns, and therefore the battery box body is fixed.
The above examples are merely illustrative for clarity and are not intended to limit the embodiments. Other variations and modifications will be apparent to persons skilled in the art in light of the above description. It is not necessary or necessary to exhaustively enumerate all embodiments herein, and obvious variations or modifications can be made without departing from the scope of the invention.

Claims (3)

1. The utility model provides a battery fixed knot constructs for unmanned aerial vehicle, it includes the battery fixed station, its characterized in that: a protruding positioning block is arranged at one end of the battery fixing table, a rotating seat is symmetrically arranged at the other end of the battery fixing table, symmetrical blind holes are formed in the rotating seat, a rotating shaft is assembled between the two blind holes, torsion springs are assembled at two ends of the rotating shaft, the torsion springs are connected with the bottoms of the blind holes of the rotating seat, and a clamping groove is formed in one side, close to the battery, of the rotating seat; the middle part of the rotating shaft is provided with a pressing plate, and one side of the pressing plate, which is close to the battery, is provided with pressing teeth.
2. The battery fixing structure for the unmanned aerial vehicle as claimed in claim 1, wherein: the shape of the protruding positioning block is matched with a positioning hole reserved at the bottom of the battery box body.
3. The battery fixing structure for the unmanned aerial vehicle as claimed in claim 1, wherein: the size of the clamping groove is matched with the size of a clamping column reserved at the bottom of the battery box body.
CN201922112755.1U 2019-12-01 2019-12-01 Battery fixing structure for unmanned aerial vehicle Expired - Fee Related CN211879420U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201922112755.1U CN211879420U (en) 2019-12-01 2019-12-01 Battery fixing structure for unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201922112755.1U CN211879420U (en) 2019-12-01 2019-12-01 Battery fixing structure for unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
CN211879420U true CN211879420U (en) 2020-11-06

Family

ID=73244010

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201922112755.1U Expired - Fee Related CN211879420U (en) 2019-12-01 2019-12-01 Battery fixing structure for unmanned aerial vehicle

Country Status (1)

Country Link
CN (1) CN211879420U (en)

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CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20201106