CN205494970U - Multiaxis aircraft battery compartment structure - Google Patents
Multiaxis aircraft battery compartment structure Download PDFInfo
- Publication number
- CN205494970U CN205494970U CN201620159090.3U CN201620159090U CN205494970U CN 205494970 U CN205494970 U CN 205494970U CN 201620159090 U CN201620159090 U CN 201620159090U CN 205494970 U CN205494970 U CN 205494970U
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- CN
- China
- Prior art keywords
- battery
- encapsulation
- aircraft
- fixed
- cap
- 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
Links
- 238000005538 encapsulation Methods 0.000 claims abstract description 38
- 230000007812 deficiency Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 238000004806 packaging method and process Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
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- Battery Mounting, Suspending (AREA)
Abstract
The utility model relates to a multiaxis aircraft battery compartment structure, include the aircraft body and set up the flight unit on the aircraft body, be provided with the fixed storehouse of battery on the aircraft body, fixedly connected with encapsulation battery in the fixed storehouse of battery, the encapsulation battery includes encapsulation lid, lower encapsulation lid and group battery, go up the encapsulation lid, down the encapsulation cover down fixed connection, the group battery fix last encapsulation lid encapsulate under and cover in, be provided with power plug on the group battery, the encapsulation battery is located the fixed storehouse back of battery, and power plug is fixed with the connector that the battery was fixed in the storehouse, and the two constitutes the electric connection. This structure is through with group battery encapsulation, can the very easy group battery that will encapsulate fix in the battery of aircraft fixed storehouse, with the aircraft can be simply swift the completion electric connection.
Description
Technical field
This utility model relates to Multi-axis aircraft field, particularly a kind of Multi-axis aircraft battery compartment
Structure.
Background technology
Multi-axis aircraft is provided with multiple flying unit, and the rotary shaft of each flying unit is all in perpendicular
Straight position, each flying unit can individually control, by controlling the state of flight of each flying unit,
Realize different offline mode so that state of flight is rich and varied；But the most on the market
The electric supply installation of aircraft is all that set of cells is passed through power line and is arranged on inserting of power cord ends
After the circuit board composition of joint and aircraft electrically connects, powering aircraft, this structure is often
Power line is exposed, there is certain potential faults, and affect attractive in appearance；In the process of use
In especially by aircraft shooting video during, run into the situation that electricity is not enough, change
Battery is very inconvenient due to the existence of power line, wastes the time, has missed fine piece of video
Section.
Utility model content
Technical problem to be solved in the utility model is to provide a kind of Multi-axis aircraft battery compartment
Structure, its starting point is battery unit package, it is possible to easily by packaged battery
Group is fixing on board the aircraft, with aircraft can with simple and fast complete electrically connect.
For solving above-mentioned technical problem, this utility model realizes as follows: this practicality
Novel described a kind of Multi-axis aircraft battery box structure includes aircraft body and is arranged at flight
Flying unit on device body, it is characterised in that: it is provided with battery on described aircraft body solid
Determine storehouse, in described battery fixed bin, to be fixedly connected with encapsulation battery；Described encapsulation battery includes
Cap, lower cap and set of cells；Described upper cap, lower cap are fixing up and down to be connected,
Set of cells is fixed in cap and lower cap；It is provided with power supply in described set of cells to insert
Head, after encapsulation battery is positioned at battery fixed bin, attaching plug and the connection in battery fixed bin
Head is fixing, and the two composition electrically connects.
It is provided with draw-in groove on described upper cap, lower cap is provided with encapsulation clamping boss,
Draw-in groove and encapsulation clamping boss is relied on to fix between upper cap and lower cap.
Battery clamping boss, the battery clamping boss of encapsulation battery it is provided with on described encapsulation battery
With the breach clamping in battery fixed bin on aircraft body.
Good effect of the present utility model: a kind of Multi-axis aircraft battery compartment described in the utility model
Structure its by by set of cells integration packaging, and battery fixed bin is set on aircraft body,
So efficiently encapsulation battery can be inserted in battery fixed bin, and complete to encapsulate battery and fly
The electrically connecting of row device, it is to avoid power line such as leaks outside at the design deficiency, improves whole aircraft
Outward appearance, and less fault rate；When running into electricity deficiency and needing the situation changing battery, only
Need the afterbody of flicking encapsulation battery so that battery clamping boss divides with the breach in battery fixed bin
Opening and can be taken out by battery, new encapsulation battery only needs directly to push in battery fixed bin, clamping
Fixing, whole process exceeds much than conventional battery connecting construction efficiency.
Accompanying drawing explanation
With detailed description of the invention this utility model made further details of theory below in conjunction with the accompanying drawings
Bright.
Fig. 1 is the structural representation that aircraft is overall
Fig. 2 is the structural representation that encapsulation battery decomposes with aircraft
Fig. 3 is the structural representation of encapsulation battery
Fig. 4 is the decomposition texture schematic diagram of encapsulation battery
Fig. 5 is the structural representation of encapsulation battery
In figure, 1 aircraft body 2 flying unit 3 encapsulates battery 4 battery fixed bin
7 times cap 8 set of cells 9 draw-in grooves of cap 6 attaching plug on 5
10 encapsulation clamping boss 11 battery clamping boss
Detailed description of the invention
As shown in Figures 1 to 5, a kind of Multi-axis aircraft battery box structure described in the utility model
Including aircraft body (1) and the flying unit (2) that is arranged on aircraft body (1),
Battery fixed bin (4), described battery fixed bin (4) it is provided with on described aircraft body (1)
Inside it is fixedly connected with encapsulation battery (3)；Described encapsulation battery (3) include cap (5),
Lower cap (7) and set of cells (8)；Described upper cap (5), lower cap (7)
Fixing connection up and down, set of cells (8) is fixed on cap (5) and lower cap (7)
In；Being provided with attaching plug (6) in described set of cells (8), encapsulation battery (3) is positioned at
After in battery fixed bin (4), attaching plug (6) and the connection in battery fixed bin (4)
Head is fixing, and the two composition electrically connects.
Being provided with draw-in groove (9) on described upper cap (5), lower cap (7) is upper to be arranged
There is encapsulation clamping boss (10), between upper cap (5) and lower cap (7), rely on card
Groove (9) and encapsulation clamping boss (10) are fixed.
Battery clamping boss (11), encapsulation battery (3) it is provided with on described encapsulation battery (3)
The upper battery fixed bin (4) of battery clamping boss (11) and aircraft body (1) in lack
Mouth clamping.
A kind of Multi-axis aircraft that this utility model that simply explains through diagrams recited above is relevant
Some functional structure principles of battery box structure, owing to coming the technical staff in constructed field
Saying and be easy to carry out on this basis some amendments, therefore this specification is not really wanted this practicality
Novel described a kind of Multi-axis aircraft battery box structure is confined to shown or described concrete
In mechanism and the scope of application, therefore every corresponding amendment that may be utilized and equivalent, all belong to
Protection domain in this utility model patent.
Claims (3)
1. a Multi-axis aircraft battery box structure, flies including aircraft body and being arranged at
Flying unit on row device body, it is characterised in that: it is provided with battery on described aircraft body
Fixed bin, is fixedly connected with encapsulation battery in described battery fixed bin；Described encapsulation battery includes
Upper cap, lower cap and set of cells；Described upper cap, lower cap are fixing up and down to be connected
Connecing, set of cells is fixed in cap and lower cap；It is provided with power supply in described set of cells
Plug, after encapsulation battery is positioned at battery fixed bin, attaching plug and the company in battery fixed bin
Joint is fixed, and the two composition electrically connects.
A kind of Multi-axis aircraft battery box structure the most according to claim 1, it is special
Levy and be: on described upper cap, be provided with draw-in groove, lower cap is provided with encapsulation clamping convex
Platform, relies on draw-in groove and encapsulation clamping boss to fix between upper cap and lower cap.
A kind of Multi-axis aircraft battery box structure the most according to claim 1, it is special
Levy and be: on described encapsulation battery, be provided with battery clamping boss, the battery clamping of encapsulation battery
Boss and the breach clamping in battery fixed bin on aircraft body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620159090.3U CN205494970U (en) | 2016-03-03 | 2016-03-03 | Multiaxis aircraft battery compartment structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620159090.3U CN205494970U (en) | 2016-03-03 | 2016-03-03 | Multiaxis aircraft battery compartment structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205494970U true CN205494970U (en) | 2016-08-24 |
Family
ID=56727218
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620159090.3U Expired - Fee Related CN205494970U (en) | 2016-03-03 | 2016-03-03 | Multiaxis aircraft battery compartment structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205494970U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109562837A (en) * | 2016-10-25 | 2019-04-02 | 深圳市大疆创新科技有限公司 | Unmanned vehicle and battery warehouse component and battery compartment |
-
2016
- 2016-03-03 CN CN201620159090.3U patent/CN205494970U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109562837A (en) * | 2016-10-25 | 2019-04-02 | 深圳市大疆创新科技有限公司 | Unmanned vehicle and battery warehouse component and battery compartment |
| CN109562837B (en) * | 2016-10-25 | 2022-03-22 | 深圳市大疆创新科技有限公司 | Unmanned vehicles and battery compartment subassembly and battery compartment |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20190409 Address after: 515800 D area, Concord Industrial Zone, south of Lai Mei Road, Chenghai District, Shantou, Guangdong. Patentee after: Guangdong Weili Intelligent Technology Co., Ltd. Address before: 515000 Block 1102, Block B8, Pumeihui Jingyuan, Guangyi Street, Chenghai District, Shantou City, Guangdong Province Patentee before: Chen Lian |
|
| 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: 20160824 Termination date: 20200303 |