CN204732455U - Aircraft battery case - Google Patents
Aircraft battery case Download PDFInfo
- Publication number
- CN204732455U CN204732455U CN201520457235.3U CN201520457235U CN204732455U CN 204732455 U CN204732455 U CN 204732455U CN 201520457235 U CN201520457235 U CN 201520457235U CN 204732455 U CN204732455 U CN 204732455U
- Authority
- CN
- China
- Prior art keywords
- box body
- opening
- battery case
- aircraft
- clamping block
- 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
Classifications
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
Abstract
The utility model discloses a kind of aircraft battery case.It comprises the box body be roughly rectangle, the lid bottom surface of box body being provided with the opening that can load rechargeable battery and can being arranged on opening, the form peripheral edge portions of opening is provided with can carry out spacing guide vane end stop by lid, the side of opening is provided with the mounting groove of connector, the sidewall of box body side end face has the charging inlet corresponding with connector and electric discharge interface, the end face of box body is provided with the locking device for being arranged on by box body on aircraft fuselage.After adopting above-mentioned structure, due to the rechargeable battery arranged in the box body of demountable structure that arranges and box body, modular mounting structure thus, not only can carry out disassembling, assembling and replacing fast to battery, also facilitate after dismounting and carry, and the rechargeable battery adopted can meet charging user demand repeatedly, and not need often to change battery, reduce replacement cost, improve service efficiency.
Description
Technical field
The utility model relates to a kind of decanning facility being applied to carry-on high polymer reason battery, specifically a kind of aircraft battery case.
Background technology
At present, domestic rotor craft supplying cell is mostly less, cruising time is short, large battery is adopted to solve the problem, but because the weight of large battery is larger, the loading capacity of aircraft can be increased, and it is very inconvenient directly large battery to be arranged on disassembling, assembling and replacing in aircraft body, therefore Large Copacity high polymer reason battery applications on board the aircraft few, even if there is a small amount of aircraft applications Large Copacity high polymer to manage battery, it uses renewal cost time-consuming, has also brought very large inconvenience.
Summary of the invention
The technical problems to be solved in the utility model be to provide one can fast insert-pull, disassembling operations convenient, the aircraft battery case of portable and module-integrated installation.
In order to solve the problems of the technologies described above, aircraft battery case of the present utility model, comprise the box body be roughly rectangle, the lid bottom surface of box body being provided with the opening that can load rechargeable battery and can being arranged on opening, the form peripheral edge portions of opening is provided with can carry out spacing guide vane end stop by lid, the side of opening is provided with the mounting groove of connector, the sidewall of box body side end face has the charging inlet corresponding with connector and electric discharge interface, the end face of box body is provided with the locking device for being arranged on by box body on aircraft fuselage.
Described locking device comprises the clamping block of the paired setting be connected on box body end face, every block clamping block all has lockpin hole, each lockpin hole all has one section of horizontally disposed draw-in groove, also comprise the lock pin that can intert in the lockpin hole of often pair of clamping block, the two ends of every root lock pin are provided with the bayonet lock adapted with draw-in groove, and described lock pin interts can make bayonet lock spacing at lockpin hole place after lockpin hole.
Described box body has some louvres.
It is two right that described clamping block is provided with, and is interspersed with lock pin respectively in often pair of clamping block.
Described electric discharge interface is provided with two.
After adopting above-mentioned structure, due to the rechargeable battery arranged in the box body of demountable structure that arranges and box body, modular mounting structure thus, not only can carry out disassembling, assembling and replacing fast to battery, also facilitate after dismounting and carry, and the rechargeable battery adopted can meet charging user demand repeatedly, and not need often to change battery, reduce replacement cost, improve service efficiency.
Accompanying drawing explanation
Fig. 1 is the main TV structure schematic diagram of the utility model aircraft battery case;
Fig. 2 is the side-looking structural representation of the utility model aircraft battery case;
Fig. 3 is locking device mounting structure schematic diagram in the utility model aircraft battery case.
Embodiment
Below in conjunction with the drawings and specific embodiments, aircraft battery case of the present utility model is described in further detail.
As shown in the figure, aircraft battery case of the present utility model, comprises the box body 1 be roughly rectangle, and box body 1 has some louvres 12; The lid 2 bottom surface of box body 1 being provided with the opening that can load rechargeable battery and can being arranged on opening, the form peripheral edge portions of opening is provided with can carry out spacing guide vane end stop 3 by lid 2, the side of opening is provided with the mounting groove of connector 4, the sidewall of box body 1 side end face has the charging inlet 5 corresponding with connector and electric discharge interface 6, the end face of box body 1 is provided with the locking device for being arranged on by box body on aircraft fuselage; Said locking device comprises the clamping block 7 that two couple be connected on box body 1 end face is arranged in pairs, every block clamping block 7 all has lockpin hole 8, each lockpin hole 8 all has one section of horizontally disposed draw-in groove 9, also comprise the lock pin 10 that can intert in the lockpin hole 8 of often pair of clamping block, the two ends of every root lock pin 10 are provided with the bayonet lock 11 adapted with draw-in groove 9, and lock pin 10 interts can make bayonet lock 11 spacing at lockpin hole 8 place after lockpin hole 8.
In installation process, rechargeable battery is put into box body 1 by opening, then install lid 2, more each discharge and recharge interface line one_to_one corresponding is inserted in charging wire interface discharge line interface discharge lines interface, during charging, charger contacts is inserted in charging wire interface; During use, device power supply (DPS) interface is inserted discharge lines interface.
Claims (5)
1. an aircraft battery case, it is characterized in that: comprise the box body (1) be roughly rectangle, the lid (2) bottom surface of described box body (1) being provided with the opening that can load rechargeable battery and can being arranged on opening, the form peripheral edge portions of described opening is provided with can carry out spacing guide vane end stop (3) by lid (2), the side of described opening is provided with the mounting groove of connector (4), the sidewall of described box body (1) side end face has the charging inlet (5) corresponding with connector and electric discharge interface (6), the end face of described box body (1) is provided with the locking device for being arranged on by box body on aircraft fuselage.
2. according to aircraft battery case according to claim 1, it is characterized in that: described locking device comprises the clamping block (7) of the paired setting be connected on box body (1) end face, every block clamping block (7) all has lockpin hole (8), each described lockpin hole (8) all has one section of horizontally disposed draw-in groove (9), also comprise the lock pin (10) that can intert in the lockpin hole (8) of often pair of clamping block, the two ends of every root lock pin (10) are provided with the bayonet lock (11) adapted with draw-in groove (9), described lock pin (10) interts can make bayonet lock (11) spacing at lockpin hole (8) place after lockpin hole (8).
3. according to aircraft battery case according to claim 1, it is characterized in that: described box body (1) has some louvres (12).
4. according to aircraft battery case according to claim 2, it is characterized in that: it is two right that described clamping block (7) is provided with, and is interspersed with lock pin (10) respectively in often pair of clamping block (7).
5. according to aircraft battery case according to claim 2, it is characterized in that: described electric discharge interface (6) is provided with two.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520457235.3U CN204732455U (en) | 2015-06-30 | 2015-06-30 | Aircraft battery case |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520457235.3U CN204732455U (en) | 2015-06-30 | 2015-06-30 | Aircraft battery case |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204732455U true CN204732455U (en) | 2015-10-28 |
Family
ID=54390784
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520457235.3U Expired - Fee Related CN204732455U (en) | 2015-06-30 | 2015-06-30 | Aircraft battery case |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204732455U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11600880B2 (en) | 2020-09-01 | 2023-03-07 | Beta Air, Llc | System and method for securing battery in aircraft |
-
2015
- 2015-06-30 CN CN201520457235.3U patent/CN204732455U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11600880B2 (en) | 2020-09-01 | 2023-03-07 | Beta Air, Llc | System and method for securing battery in aircraft |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN201294399Y (en) | Parallel device of charging plant | |
| CN106450091B (en) | Power battery | |
| CN201409013Y (en) | Power supply adaptor | |
| CN207896675U (en) | The retired battery of electric vehicle matching energy storage inverter compatible with new battery | |
| US20130254568A1 (en) | Power supply device for server | |
| CN204732455U (en) | Aircraft battery case | |
| CN204857811U (en) | Assembled battery case | |
| CN204721017U (en) | A kind of portable type solar energy charger for mobile phone | |
| CN203800657U (en) | Mobile power supply with expansible cell grooves | |
| CN208955036U (en) | A kind of unmanned plane fast insert-pull cell apparatus | |
| CN102983372A (en) | Uninterruptible battery pack | |
| CN207303551U (en) | Connector | |
| CN209658279U (en) | A kind of power battery pack convenient for manually replacing | |
| CN208723584U (en) | A kind of vehicle electronic circuit converting system | |
| CN202160002U (en) | Multifunctional mobile phone charger | |
| CN111756105A (en) | Communication base station power supply system for gradient utilization of retired power battery | |
| CN202231449U (en) | Accumulator assembly in a UPS power supply | |
| CN205178570U (en) | Mobile power source | |
| CN204794173U (en) | Balanced charging device of battery | |
| CN208908421U (en) | A kind of power supply adaptor with mobile charging function | |
| CN212909105U (en) | UPS power supply of replaceable energy storage battery | |
| CN204287353U (en) | Charger performance parameter testing system and tool | |
| CN201887132U (en) | Rechargeable lithium cell device | |
| CN202145583U (en) | Battery charger of laptop | |
| CN212909009U (en) | Combined charger |
Legal Events
| 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 |
Granted publication date: 20151028 Termination date: 20210630 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |