CN105977421B - A kind of fixed mechanism of aircraft battery - Google Patents
A kind of fixed mechanism of aircraft battery Download PDFInfo
- Publication number
- CN105977421B CN105977421B CN201610451876.7A CN201610451876A CN105977421B CN 105977421 B CN105977421 B CN 105977421B CN 201610451876 A CN201610451876 A CN 201610451876A CN 105977421 B CN105977421 B CN 105977421B
- Authority
- CN
- China
- Prior art keywords
- lid
- locking member
- box body
- card slot
- sliding part
- 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.)
- Active
Links
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
-
- 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
Landscapes
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Electrochemistry (AREA)
- General Chemical & Material Sciences (AREA)
- Battery Mounting, Suspending (AREA)
Abstract
The invention discloses a kind of fixed mechanisms of aircraft battery, including box body, lid and retaining mechanism, the box body includes the cavity with opening, the lid is arranged in the opening of box body, lid includes the first lid and the second lid, first lid is fixedly installed on box body, first lid is equipped with card slot close to an end face of the second lid, the retaining mechanism includes sliding part and locking member, the locking member protrudes into the card slot, the sliding part is slidably disposed on the second lid, one end of sliding part passes through the second lid and connect with the locking member, the sliding of sliding part drives locking member to slide along the direction of the first lid to the second lid.A kind of fixed mechanism of aircraft battery provided by the invention, not only versatility is good, but also avoids using fixing pieces such as screws, so that it is convenient for disassembly and assembly, while also there is the simple technical effect of structure.
Description
Technical field
The present invention relates to aircraft field more particularly to a kind of fixed mechanisms of aircraft battery.
Background technique
Carry-on battery, as the important devices of aircraft, for providing the flying power of aircraft.Aircraft exists
Vibration is easy to produce in flight course, battery is because shaking or moving in order to prevent, and the connection between equipment to be powered generates
It loosens, causes aircraft to occur abnormal, it need to be fixed on board the aircraft by battery.
Application No. is 201510998771.9 Chinese invention patents to disclose a kind of battery and aircraft, the battery pack
Include battery core, battery case, at least one unblock button and at least one first power connector；The battery core is located at the battery
In shell, each unblock button at least one described unblock button is arranged on the battery case, the unblock button
Including button, resilient panel, button erecting bed and the first tight lock part, the button erecting bed is equipped with mounting hole, the button packet
Include press section and installation axle；The resilient panel is fixed on the battery case, and the button erecting bed is fixed on the electricity
On the shell of pond, and the resilient panel is between the battery case and the button erecting bed；One end of the installation axle
It is fixed on the press section, the other end passes through the mounting hole and contacts with the resilient panel, and first tight lock part is located at
Around the resilient panel；The aircraft is equipped with battery settling groove, is equipped with and the battery in the battery settling groove
In each unblock button corresponding second tight lock part of the first tight lock part, the first tight lock part and the second tight lock part cooperation, by institute
Battery lock is stated in battery settling groove.It need to be mounted on battery for fixing the unblock button of battery in above-mentioned patent, for one
As battery will be unable to be fixed in battery settling groove, the versatility of above-mentioned fixed form is poor, is unfavorable for using on a large scale；Together
When, the structure of the unblock button is more complex, will increase manufacturing cost.
In addition, in the prior art, being fixed also by the mode for being screwed battery cover on battery settling groove
Battery when fetching battery, needs to unscrew screw, again takes out battery after battery cover is removed, then reuse screw for battery
Lid is fixed on battery settling groove.The installation and removal process of such mode battery cover is cumbersome, and under screw dismounting after easily
It loses, if will be unable to fixed battery cover without spare screw, making troubles to using.
Summary of the invention
The technical problems to be solved by the present invention are: providing a kind of consolidating for the simple and convenient for disassembly and assembly aircraft battery of structure
Determine mechanism.
In order to solve the above-mentioned technical problem, the technical solution adopted by the present invention are as follows:
A kind of fixed mechanism of aircraft battery, including box body, lid and retaining mechanism, the box body include having opening
Cavity, the lid is arranged in the opening of box body, and lid includes the first lid and the second lid, and first lid is fixed
It is set on box body, the first lid is equipped with card slot close to an end face of the second lid, and the retaining mechanism includes sliding part and lock
Tight part, the locking member protrude into the card slot, and the sliding part is slidably disposed on the second lid, one end of sliding part
It is connect across the second lid and with the locking member, the sliding of sliding part drives locking member along the first lid to the side of the second lid
To sliding.
The beneficial effects of the present invention are: battery is mounted in the cavity on box body, and lid is set on box body, i.e.,
Battery can be stably placed in the enclosure space of box body and lid composition, no setting is required on battery unblock button, versatility
Good, the installation for being adaptable to multiple battery is fixed；First lid is equipped with card slot, and sliding part is slidably arranged, sliding part sliding
When drive locking member sliding, the sliding of locking member protrudes into locking member or far from card slot, thus realize the second lid locking or
It opens；It avoids being fixed using accessories such as screws, it is not only convenient for disassembly and assembly, and also structure is simple.
Detailed description of the invention
Fig. 1 is the decomposition diagram of the fixed mechanism of the aircraft battery of the embodiment of the present invention；
Fig. 2 is the combination diagram of the fixed mechanism of the aircraft battery of the embodiment of the present invention；
Fig. 3 is sectional view when the second lid is in locking state in Fig. 2 at A；
Fig. 4 is sectional view when the second lid is in the open state in Fig. 2 at A.
Label declaration:
1, box body；11, cavity；111, groove；2, lid；21, the first lid；211, card slot；22, the second lid；31, sliding
Moving part；32, locking member；321, positioning column；322, stage portion；323, locating slot；33, elastic component；4, limit film；5, elastic slice；6,
Shaft；7, battery.
Specific embodiment
In order to describe the technical content, the structural feature, the achieved object and the effect of this invention in detail, below in conjunction with embodiment
And attached drawing is cooperated to be explained in detail.
The most critical design of the present invention is: setting retaining mechanism, can avoid being fixed using fixing pieces such as screws, no
Only structure is simple, and convenient for disassembly and assembly.
A kind of fixed mechanism of aircraft battery referring to FIG. 1 to FIG. 4, including box body 1, lid 2 and retaining mechanism, institute
Stating box body 1 includes the cavity 11 with opening, and the lid 2 is arranged in the opening of box body 1, and lid 2 includes the first lid 21
With the second lid 22, first lid 21 is fixedly installed on box body 1, and the first lid 21 is close to an end face of the second lid 22
Equipped with card slot 211, the retaining mechanism includes sliding part 31 and locking member 32, and the locking member 32 protrudes into the card slot 211,
The sliding part 31 is slidably disposed on the second lid 22, one end of sliding part 31 pass through the second lid 22 and with the lock
Tight part 32 connects, and the sliding of sliding part 31 drives locking member 32 to slide along the direction of 21 to the second lid 22 of the first lid.
As can be seen from the above description, the beneficial effects of the present invention are: battery is mounted in the cavity on box body, and in box
Lid is set on body, battery can be stably placed in the enclosure space of box body and lid composition, no setting is required on battery
Unblock button, versatility is good, and the installation for being adaptable to multiple battery is fixed；First lid is equipped with card slot, and sliding part is slidably
Setting drives locking member sliding when sliding part slides, the sliding of locking member protrudes into locking member or far from card slot, to realize the
The locking or unlatching of two lids；It avoids being fixed using accessories such as screws, it is not only convenient for disassembly and assembly, and also structure is simple.
Further, the retaining mechanism further includes elastic component 33, and one end of the elastic component 33 is arranged described second
On lid 22, the other end of elastic component 33 is arranged on the locking member 32.
Seen from the above description, elastic component can be spring, and when the second lid is closed, locking member is stretched under the action of the elastic member
Enter in card slot, the connection of the first lid and the second lid is realized by locking member, when opening the second lid, elastic component is in compression
State, locking member stretch out card slot.
It further, further include limit film 4, the elastic component 33 is set between second lid 22 and limit film 4
And resist the limit film 4.
Seen from the above description, limit film is set, can prevent elastic component such as spring is when in a compressed state to arch upward, with limit
Piece, which pushes down elastic component, can play position-limiting action to elastic component, and can prevent from blocking when elastic component is flexible, keep elastic component flexible more
It is smooth.
Further, the material of the limit film 4 is stainless steel.
Seen from the above description, the material of limit film is stainless steel, and the surface of stainless steel is more smooth, can be to elastic component such as bullet
Spring it is long-term it is flexible play the role of one it is wear-resisting, keep telescopic spring more smooth, and the exception that will not block or generate " click click " is loud
Sound.
Further, the surface of the bottom of the card slot 211 is inclined surface, and the locking member 32 protrudes into the one of card slot 211
The surface of the end at end is inclined surface.
Seen from the above description, the bottom of card slot is inclined surface, and the end of locking member is to match with the bottom of card slot
Inclined surface is caught in when sliding locking piece, and has certain guiding role.
Further, the locking member 32 is equipped with stage portion 322, the stage portion 322 close to one end of the card slot 211
It protrudes into the card slot 211.
Seen from the above description, stage portion is set on locking member, the sliding stroke of locking member can be limited.
Further, the locking member 32 is equipped with locating slot 323, the sliding part 31 by the locating slot 323 with
Locking member 32 connects.
Seen from the above description, locating slot is set on locking member, sliding part can with the locating slot close-fitting on locking member or adopt
It is attached with mode for dispensing glue.
It further, further include elastic slice 5, the elastic slice 5 is arranged on the box body 1 and resists the lid 2.
Seen from the above description, when the second lid is opened, elastic slice is in and flicks state, and when battery cover closes, elastic slice is in
Compressive state, when pushing sliding part that locking member is made to stretch out card slot, the second lid is pushed open certain angle by elastic slice, and facilitating will with hand
Battery cover pulls open.
Further, second lid 22 is hinged on the box body 1 far from one end of first lid 21.
Seen from the above description, the second lid is hinged on box body, and when the second lid is opened, the second lid is without departing from box
Body itself, which prevent the possibility for falling off, losing when box body opening.
Further, the marginal position setting fluted 111 of the cavity 11.
Seen from the above description, the marginal position setting of cavity is fluted, can conveniently be put into the pick-and-place behaviour of the battery of cavity
Make, and the hand-held groove for facilitating battery taking and placing can be set on battery.
Please refer to Fig. 1 to Fig. 4, the embodiment of the present invention one are as follows:
A kind of fixed mechanism of aircraft battery, including box body 1, lid 2, retaining mechanism, limit film 4 and elastic slice 5, box body
1 includes the cavity 11 with opening, and cavity 11 is used for placing battery 7, the marginal position setting fluted 111 of cavity 11, lid 2
It is arranged in the opening of box body 1, lid 2 includes the first lid 21 and the second lid 22, and the first lid 21 is fixedly installed on box body 1
On, the second lid 22 can open and close to be arranged on box body 1, and the one end of the second lid 22 far from the first lid 21 is cut with scissors by shaft 6
It connects on box body 1.
First lid 21 is equipped with card slot 211 close to an end face of the second lid 22, and retaining mechanism includes sliding part 31, locking
The second side of the lid 22 far from box body 1 is arranged in part 32 and elastic component 33, sliding part 31, and locking member 32 is arranged in the second lid
22 other side, sliding part 31 are slidably disposed on the second lid 22, and one end of sliding part 31 passes through the second lid 22 simultaneously
It being connect with locking member 32, the sliding of sliding part 31 drives locking member 32 to slide along the direction of 21 to the second lid 22 of the first lid,
When locking member 32 slides, one end of locking member 32 is protruded into card slot 211 or far from card slot 211.It is set on the other end of locking member 32
There is positioning column 321, one end of elastic component 33 is arranged on the second lid 22, and the other end of elastic component 33 is set in positioning column 321
On.The second lid 22 is arranged in the one side of box body 1 in limit film 4, and elastic component 33 is set to the second lid 22 and limit film 4
Between and resist limit film 4.The material of limit film 4 is stainless steel.
The surface of the bottom of card slot 211 be inclined surface, locking member 32 protrude into the end of one end of card slot 211 surface be with
The inclined surface that the bottom of card slot 211 matches.Locking member 32 is additionally provided with stage portion 322 and locating slot 323, and stage portion 322 protrudes into
In card slot 211.One end that sliding part 31 is connect with locking member 32 is arranged in locating slot 323, and sliding part 31 and locking member 32 can
It is attached by close-fitting or mode for dispensing glue.Elastic slice 5 is arranged on box body 1 and resists lid 2.
In conclusion a kind of fixed mechanism of aircraft battery provided by the invention, not only versatility is good, but also avoids making
With fixing pieces such as screws, so that it is convenient for disassembly and assembly, while also there is the simple technical effect of structure.
The above description is only an embodiment of the present invention, is not intended to limit the scope of the invention, all to utilize this hair
Equivalents made by bright specification and accompanying drawing content are applied directly or indirectly in relevant technical field, similarly include
In scope of patent protection of the invention.
Claims (7)
1. a kind of fixed mechanism of aircraft battery, which is characterized in that including box body, lid and retaining mechanism, the box body packet
The cavity with opening is included, the lid is arranged in the opening of box body, and lid includes the first lid and the second lid, and described the
One lid is fixedly installed on box body, and the first lid is equipped with card slot close to an end face of the second lid, and the retaining mechanism includes
Sliding part and locking member, the locking member protrude into the card slot, and the sliding part is slidably disposed on the second lid, sliding
One end of moving part passes through and the second lid and connect with the locking member, and the sliding drive locking member of sliding part is along the first lid to the
The direction of two lids is slided, and the locking member is equipped with stage portion close to one end of the card slot, and the stage portion protrudes into the card
In slot, the stage portion limits the sliding stroke of locking member；
The surface of the bottom of the card slot is inclined surface, and the locking member protrudes into the surface of the end of one end of card slot as inclination
Face, the inclined surface on the card slot are mutually matched with the inclined surface on the locking member；
The locking member is equipped with locating slot, and the sliding part is connect by the locating slot with locking member.
2. the fixed mechanism of aircraft battery according to claim 1, which is characterized in that the retaining mechanism further includes bullet
Property part, one end of the elastic component is arranged on second lid, and the other end of elastic component is arranged on the locking member.
3. the fixed mechanism of aircraft battery according to claim 2, which is characterized in that it further include limit film, the bullet
Property part is set between the second lid and limit film and resists the limit film.
4. the fixed mechanism of aircraft battery according to claim 3, which is characterized in that the material of the limit film is not
Become rusty steel.
5. the fixed mechanism of aircraft battery according to claim 1, which is characterized in that it further include elastic slice, the elastic slice
It is arranged on the box body and resists the lid.
6. the fixed mechanism of aircraft battery according to claim 1, which is characterized in that second lid is far from described
One end of first lid is hinged on the box body.
7. the fixed mechanism of aircraft battery according to claim 1, which is characterized in that the margin location of the cavity installs
It is equipped with groove.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610451876.7A CN105977421B (en) | 2016-06-21 | 2016-06-21 | A kind of fixed mechanism of aircraft battery |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610451876.7A CN105977421B (en) | 2016-06-21 | 2016-06-21 | A kind of fixed mechanism of aircraft battery |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105977421A CN105977421A (en) | 2016-09-28 |
| CN105977421B true CN105977421B (en) | 2019-03-12 |
Family
ID=57022312
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610451876.7A Active CN105977421B (en) | 2016-06-21 | 2016-06-21 | A kind of fixed mechanism of aircraft battery |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105977421B (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107278079B (en) * | 2017-08-09 | 2023-09-05 | 上海未来伙伴机器人有限公司 | Accommodating box flip structure and robot |
| CN112103442B (en) * | 2020-10-12 | 2024-05-28 | 广东好太太智能家居有限公司 | Lock battery box |
| WO2023077308A1 (en) * | 2021-11-03 | 2023-05-11 | 深圳市大疆创新科技有限公司 | Remote control |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203026568U (en) * | 2012-11-29 | 2013-06-26 | 深圳市新国都技术股份有限公司 | Switch structure |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2002025521A (en) * | 2000-07-05 | 2002-01-25 | Tookado:Kk | Battery pack in/out device |
| KR101168936B1 (en) * | 2006-05-16 | 2012-08-02 | 엘지전자 주식회사 | Battery cover locking apparatus and mobile terminal having the same |
| CN101635338B (en) * | 2008-07-23 | 2012-07-18 | 鸿富锦精密工业（深圳）有限公司 | Battery fixing device |
| CN204333055U (en) * | 2015-01-15 | 2015-05-13 | 上海小蚁科技有限公司 | A kind of easy-to-mount battery cover |
| CN205752324U (en) * | 2016-06-21 | 2016-11-30 | 深圳市高巨创新科技开发有限公司 | A kind of fixed mechanism of aircraft battery |
-
2016
- 2016-06-21 CN CN201610451876.7A patent/CN105977421B/en active Active
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203026568U (en) * | 2012-11-29 | 2013-06-26 | 深圳市新国都技术股份有限公司 | Switch structure |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105977421A (en) | 2016-09-28 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105977421B (en) | A kind of fixed mechanism of aircraft battery | |
| US10842037B2 (en) | Pull-out aiding device and chassis-wall module with pull-out aiding function | |
| US20130099640A1 (en) | Housing with rotation arm and panel for securing hard disk drive therein | |
| US4978949A (en) | Locking mechanism and support legs for removable display assembly | |
| US7596001B2 (en) | Expansion card retention assembly | |
| US8544967B2 (en) | Server rack | |
| US20120132661A1 (en) | Display device with detachable display module | |
| WO2019137256A1 (en) | Washing machine box and washing machine | |
| US8354182B2 (en) | Battery box and electronic device using the same | |
| TW201401975A (en) | Housing of electronic device | |
| CN110230625A (en) | Lock uint and dust preventing component and projection device | |
| CN205752324U (en) | A kind of fixed mechanism of aircraft battery | |
| CN209626276U (en) | Cell apparatus and electronic equipment | |
| CN105489234B (en) | A kind of airborne built-in plug-in and pull-off device of recording equipment storage dish | |
| TW201742527A (en) | Housing module and electronic device with circuit board quick-assembling function | |
| TWI517146B (en) | Fixing bracket | |
| WO2020052159A1 (en) | Water tank button device in tower fan and tower fan | |
| KR20010042779A (en) | Disc drive latch | |
| CN113677113B (en) | Handle mechanism and casing assembly comprising same | |
| US11039546B2 (en) | Pull-out aiding device and chassis-wall module with pull-out aiding function | |
| CN201159992Y (en) | Structure improvement of abstraction type winchester disk drive | |
| CN208833308U (en) | A kind of metering instrument controller and gas meter, flow meter of rotating folding cover board | |
| CN109725690B (en) | Case cover lock for tool-free server case disassembly and assembly | |
| KR20130087453A (en) | Locking device of glove box | |
| TW201619512A (en) | Latch device and server using the same |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |