CN205388979U - Battery structure for unmanned aerial vehicle - Google Patents

Battery structure for unmanned aerial vehicle Download PDF

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Publication number
CN205388979U
CN205388979U CN201620020129.3U CN201620020129U CN205388979U CN 205388979 U CN205388979 U CN 205388979U CN 201620020129 U CN201620020129 U CN 201620020129U CN 205388979 U CN205388979 U CN 205388979U
Authority
CN
China
Prior art keywords
battery
unmanned plane
cover plate
mounting groove
aerial vehicle
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
CN201620020129.3U
Other languages
Chinese (zh)
Inventor
范简华
赵永霞
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.)
Wuxi Miracle Science & Technology Co Ltd
Original Assignee
Wuxi Miracle Science & 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 Wuxi Miracle Science & Technology Co Ltd filed Critical Wuxi Miracle Science & Technology Co Ltd
Priority to CN201620020129.3U priority Critical patent/CN205388979U/en
Application granted granted Critical
Publication of CN205388979U publication Critical patent/CN205388979U/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

Abstract

The utility model discloses a battery structure for unmanned aerial vehicle, include: the unmanned aerial vehicle casing, be provided with the mounting groove in the unmanned aerial vehicle casing, the inside swing joint of mounting groove has battery case, be equipped with the battery in the battery case, the last swing joint of battery case has the apron, the apron rotates around battery case, and the pulling apron takes out battery case from the mounting groove. In this way, the utility model discloses battery structure for unmanned aerial vehicle can realize the dismouting of unmanned aerial vehicle battery fast, and the structure letter is answered, convenient to use, safe and reliable.

Description

Unmanned plane battery structure
Technical field
This utility model relates to unmanned plane field, particularly relates to a kind of unmanned plane battery structure.
Background technology
UAV is called for short " unmanned plane ", and english abbreviation is " UAV ", is the non-manned aircraft of the presetting apparatus manipulation utilizing radio robot with providing for oneself.In order to simplify the design structure of unmanned plane, sometimes by separately positioned to fuselage and power supply, when needs use unmanned plane, power supply and fuselage are connected, when unmanned plane need not be used, power supply dismounting are placed, is so also beneficial to the maintenance of fuselage and power supply.The present battery of unmanned plane is installed in body typically via polylith installing plate or separate space, extremely inconvenient during placing battery, and battery case weight is big, affects the flight efficiency of unmanned plane.
Summary of the invention
This utility model is mainly solving the technical problems that provide a kind of unmanned plane battery structure, it is possible to quickly realizing unmanned plane battery disassembly and assembly, structure letter is answered, easy to use, safe and reliable.
For solving above-mentioned technical problem, the technical scheme that this utility model adopts is: provide a kind of unmanned plane battery structure, including: unmanned plane casing, it is provided with mounting groove in described unmanned plane casing, described mounting groove internal activity is connected to battery container, is provided with battery, described battery container is connected with cover plate in described battery container, described cover plate rotates around battery container, pulls cover plate to be taken out from mounting groove by battery container.
In one preferred embodiment of this utility model, described battery container includes upper shell, lower house and end cap, and described upper cover body is connected with end cap respectively with lower cover.
In one preferred embodiment of this utility model, the middle part of described cover plate is hinged on end cap by rotating shaft.
In one preferred embodiment of this utility model, described cover plate is circular cover.
In one preferred embodiment of this utility model, described unmanned plane housing is provided with end cap and the installing port matched.
The beneficial effects of the utility model are: this utility model unmanned plane battery structure, it is possible to quickly realizing unmanned plane battery disassembly and assembly, structure letter is answered, easy to use, safe and reliable.
Accompanying drawing explanation
In order to be illustrated more clearly that the technical scheme in this utility model embodiment, below the accompanying drawing used required during embodiment is described is briefly described, apparently, accompanying drawing in the following describes is only embodiments more of the present utility model, for those of ordinary skill in the art, under the premise not paying creative work, it is also possible to obtain other accompanying drawing according to these accompanying drawings, wherein:
Fig. 1 is the structural representation of this utility model unmanned plane battery structure one preferred embodiment;
Fig. 2 is the battery case retracted arrangement schematic diagram of the unmanned plane battery structure shown in Fig. 1;
Fig. 3 is the partial structurtes schematic diagram of the unmanned plane battery structure shown in Fig. 2
In accompanying drawing, the labelling of each parts is as follows: 1, unmanned plane casing, and 2, mounting groove, 3, battery container, 4, battery, 5, cover plate, 6, upper shell, 7, lower house, 8, end cap, 9, installing port, 10, rotating shaft.
Detailed description of the invention
Technical scheme in this utility model embodiment will be clearly and completely described below, it is clear that described embodiment is only a part of embodiment of the present utility model, rather than whole embodiments.Based on the embodiment in this utility model, all other embodiments that those of ordinary skill in the art obtain under not making creative work premise, broadly fall into the scope of this utility model protection.
Refer to Fig. 1, a kind of unmanned plane battery structure, including: unmanned plane casing 1, it is provided with mounting groove 2 in described unmanned plane casing 1, described mounting groove 2 internal activity is connected to battery container 3, is provided with battery 4, described battery container 3 is connected with cover plate 5 in described battery container 3, described cover plate 5 rotates around battery container 3, pulls cover plate 5 to be taken out from mounting groove 2 by battery container 3.
It addition, described battery container 3 includes upper shell 6, lower house 7 and end cap 8, described upper cover body 6 is connected with end cap 8 respectively with lower cover 7.
It addition, the middle part of described cover plate 5 is hinged on end cap by rotating shaft 10.
It addition, described cover plate 5 is circular cover.
It addition, described unmanned plane housing 1 is provided with the installing port 9 matched with end cap 8.
This utility model unmanned plane battery structure specific works principle is as follows: by lower cover 5, cover plate 5 turns an angle around end cap 8, arrange with the inclined shape of end cap 8, then pull and battery container 3 can be pulled out from mounting groove 2 below cover plate 5, it is achieved battery container 3 pulls out.When needing to put back to battery container 3, cover plate 5 is promoted to make battery case 3 return in mounting groove 2, then rotating plate 5 to initial position.
It is different from prior art, this utility model unmanned plane battery structure, it is possible to quickly realizing unmanned plane battery disassembly and assembly, structure letter is answered, easy to use, safe and reliable.
The foregoing is only embodiment of the present utility model; not thereby the scope of the claims of the present utility model is limited; every equivalent structure utilizing this utility model description to make or equivalence flow process conversion; or directly or indirectly it is used in other relevant technical field, all in like manner include in scope of patent protection of the present utility model.

Claims (5)

1. a unmanned plane battery structure, it is characterized in that, including: unmanned plane casing, it is provided with mounting groove in described unmanned plane casing, described mounting groove internal activity is connected to battery container, is provided with battery, described battery container is connected with cover plate in described battery container, described cover plate rotates around battery container, pulls cover plate to be taken out from mounting groove by battery container.
2. unmanned plane battery structure according to claim 1, it is characterised in that described battery container includes upper shell, lower house and end cap, and described upper cover body is connected with end cap respectively with lower cover.
3. unmanned plane battery structure according to claim 2, it is characterised in that the middle part of described cover plate is hinged on end cap by rotating shaft.
4. unmanned plane battery structure according to claim 3, it is characterised in that described cover plate is circular cover.
5. unmanned plane battery structure according to claim 2, it is characterised in that described unmanned plane housing is provided with end cap and the installing port matched.
CN201620020129.3U 2016-01-11 2016-01-11 Battery structure for unmanned aerial vehicle Expired - Fee Related CN205388979U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620020129.3U CN205388979U (en) 2016-01-11 2016-01-11 Battery structure for unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620020129.3U CN205388979U (en) 2016-01-11 2016-01-11 Battery structure for unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
CN205388979U true CN205388979U (en) 2016-07-20

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620020129.3U Expired - Fee Related CN205388979U (en) 2016-01-11 2016-01-11 Battery structure for unmanned aerial vehicle

Country Status (1)

Country Link
CN (1) CN205388979U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105514315A (en) * 2016-01-11 2016-04-20 无锡觅睿恪科技有限公司 Cell structure for unmanned plane

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105514315A (en) * 2016-01-11 2016-04-20 无锡觅睿恪科技有限公司 Cell structure for unmanned plane

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Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
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: 20160720

Termination date: 20180111