CN201319384Y - Battery limiting structure - Google Patents
Battery limiting structure Download PDFInfo
- Publication number
- CN201319384Y CN201319384Y CNU2008201370881U CN200820137088U CN201319384Y CN 201319384 Y CN201319384 Y CN 201319384Y CN U2008201370881 U CNU2008201370881 U CN U2008201370881U CN 200820137088 U CN200820137088 U CN 200820137088U CN 201319384 Y CN201319384 Y CN 201319384Y
- Authority
- CN
- China
- Prior art keywords
- battery
- limiting structure
- elastic component
- position limiting
- locating 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.)
- Expired - Fee Related
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- 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
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- Battery Mounting, Suspending (AREA)
Abstract
A battery limiting structure is arranged in a battery accommodating chamber of an electronic device and used for fixing batteries. The battery limiting structure comprises an elastic element and a limit component, wherein one end of the elastic elements is connected with a machine body of the electronic device while the other end thereof adopts a free end, and the limit component is connected with the free end of the elastic element. When in use, the elastic elements can swing freely to enable the limit component to buckle the batteries selectively, so as to prevent the power supply from being affected by batteries separated from the battery accommodating chamber.
Description
Technical field
The utility model refers to a kind of battery position limiting structure that is applied to electronic installation especially relevant for a kind of battery fastening structure.
Background technology
The progress of science and technology brings human considerable convenient, and in this information fast in epoch of accumulation, and many electronic installations are in the one-tenth work or indispensable product in life.Desiring to make this electronic installation to obtain mobility and handled easily, is to be unified design in the inside of electronic installation equipped with battery, also is about to the battery accommodation chamber that battery is placed in electronic installation inside, in order to required electric power to be provided.
With the camera is example, in order to make things convenient for the user to use out of doors, be to provide camera required electric power by battery, so can be provided with a battery chamber in camera inside, this battery chamber is used for set battery, see also Figure 1A, shown in Figure 1B and Fig. 1 C, among the figure, camera is provided with a 1a of battery chamber, one fastener 2a, an one spring 3a and a cover plate 4a, the 1a of this battery chamber is in order to hold a battery 5a, just make this battery 5a, among negative pole and the 1a of battery chamber just, negative terminal connects, reach the purpose that power supply is provided by this battery 5a, wherein this spring 3a is connected between this fastener 2a and the 1a of this battery chamber, and this fastener 2a is subjected to the effect of this spring 3a and push against and fix this battery 5a (shown in Fig. 1 C) in the 1a of this battery chamber.
So, battery chamber's structure of above-mentioned electronic installation still exists and can improve part:
1, its effect of spring 3a competence exertion because fastener 2a must arrange in pairs or groups therefore when spring 3a damage, is promptly represented the fixing function of fastener 2a forfeiture.
2, cost of parts is higher, because use a part (spring 3a) more.
3, owing to must assemble this fastener 2a and this spring 3a, therefore increase the time of assembling, and then reduce output.
In view of this, the improving of the above-mentioned disappearance of this creator thoughts, and according to the correlation experience of being engaged in for many years in this respect, the concentrated observation and research, and cooperate the utilization of scientific principle, and propose a kind of reasonable in design and effectively improve the utility model of above-mentioned disappearance.
The utility model content
A purpose of the present utility model is to provide a kind of battery position limiting structure, and it can replace present employed spring, makes this battery position limiting structure have the function that can automatically return to initial position.
Another purpose of the present utility model is to provide a kind of battery position limiting structure, and it is simple in structure, and the number of parts of using is few, can reduce cost of parts and reduce assembling man-hour.
In order to reach above-mentioned purpose, the utility model provides a kind of battery position limiting structure, it is arranged at the fuselage body of electronic installation, and the fuselage body of this electronic installation is provided with an ostiolate battery room, see through this opening and can install a battery in this battery room, this battery position limiting structure includes: an elastic component, integrated this fuselage body that is connected in of an end be near this battery room place, and the other end of this elastic component then is one to extend and can swing freely free end toward this opening direction; An and locating part, it is incorporated into the free end of this elastic component and exposes to this opening, when being equiped with this battery in this battery room, but the elastic force of this this elastic component of locating part mat remains on the position that can be connected to this battery one side, so that this battery is limited in this battery room.
Preferably, this elastic component and this fuselage body are formed in one.
Preferably, this elastic component is an elastic arm, and this elastic arm is integrated is extended by this fuselage body.
Preferably, have one between this elastic component and this battery at interval.
Preferably, this locating part has one and is sphenoid and is positioned at the outer clamping part of this opening, and the flattened side backstop of this sphenoid of mat is lived this battery.
Preferably, this elastic component is in being equipped with a combined hole near free end, and this locating part has a fixed leg, and this fixed leg embeds and is fixed in this combined hole.
Preferably, this elastic component is in convexing with a fixed leg near free end, and this locating part is equipped with a combined hole, and this fixed leg embeds and is fixed in this combined hole.
Preferably, this fuselage body further is provided with one in order to replace the yoke frame of this battery in this battery room bottom.
Preferably, this yoke frame is a spring or a shell fragment.
Preferably, this elastic component is a working of plastics.
Preferably, the material of the fuselage body of this electronic installation is a plastic material.
Be with, see through battery position limiting structure of the present utility model beneficial effect described as follows be provided:
The structural design of not having any complexity, just can replace spring provides buckle elastic force, allows this locating part can automatically return to the home position with the snap fit battery; Moreover the utility model is operated easily, and is smoothly very convenient in the use.
In addition, of the present utility modelly simple in structurely can effectively save cost of manufacture, and because part is few, make assembling can further reduce man-hour, improve output.
In order further to understand the utility model is to reach technology, method and the effect that set purpose is taked, see also following about detailed description of the present utility model and accompanying drawing, believe the purpose of this utility model, feature and characteristics, go deep into and concrete understanding when getting one thus, yet appended graphic reference and the explanation usefulness of only providing not is to be used for the utility model is limited.
Description of drawings
Figure 1A is the battery buckle structural representation of known electronic installation.
Figure 1B is the user mode figure of the battery buckle of known electronic installation.
Fig. 1 C is another user mode figure of the battery buckle of known electronic installation.
Fig. 2 is the schematic perspective view of battery position limiting structure of the present utility model.
Fig. 3 is another schematic perspective view of battery position limiting structure of the present utility model.
Fig. 4 is the partial enlarged drawing of battery position limiting structure of the present utility model.
Fig. 5 is the user mode schematic diagram of battery position limiting structure of the present utility model.
Fig. 6 is another user mode schematic diagram of battery position limiting structure of the present utility model.
Fig. 7 is the cross-sectional schematic of battery position limiting structure of the present utility model.
The primary clustering symbol description
One, known
The 1a battery chamber
The 2a fastener
The 3a spring
The 4a cover plate
The 5a battery
Two, the utility model
1 fuselage body
11 battery rooms
12 openings
2 batteries
3 elastic components
31 combined holes
4 locating parts
41 clamping parts
42 fixed legs
5 yoke frames
6 electroconductive elastic sheets
Embodiment
Please cooperate consult shown in Figure 2, the utility model provides a kind of battery position limiting structure, it is applied to (is example with the camera) on the electronic installation, wherein the fuselage body 1 of this electronic installation is provided with a battery room 11, this battery room 11 is in order to install a ccontaining battery 2, this battery 2 can be a lithium battery, and this battery 2 of mat provides the electronic installation running required electric power; In addition, fuselage body 1 contiguous these battery room 11 parts of this electronic installation offer an opening 12, and this opening 12 communicates with this battery room 11, and the user can see through this opening 12 and battery 2 is placed into this battery room 11 by this.
Please refer to shown in Figure 3, battery position limiting structure of the present utility model is positioned at the battery room 11 of electronic installation, this battery position limiting structure includes: an elastic component 3 and a locating part 4 that is connected with this elastic component 3, this elastic component 3 of mat is worked in coordination with this locating part 4, fix this battery 2 in this battery room 11 with this locating part 4, avoid this battery 2 to deviate from this battery room 11, and cause electronic installation to decommission.
This elastic component 3 is arranged in this battery room 11 and contiguous this opening 12, and this elastic component 3 is this fuselage body 1 one-body molded arm body that extends, wherein an end of this elastic component 3 is connected and fixed on this fuselage body 1 near these battery room 11 places, the other end of this elastic component 3 then is one to extend and can swing freely free end (as shown in Figure 4) toward this opening 12 directions, the design that mat is above-mentioned, this elastic component 3 is the action that fulcrum is swung with a fixing end; In addition, this elastic component 3 is all plastic material with the material of this fuselage body 1, and so when producing, this elastic component 3 can integratedly produce each other with this fuselage body 1, except that saving production cost, also can save the time of assembling.
This locating part 4 is connected in the free end of this elastic component 3 and exposes to this opening 12, therefore this locating part 4 can be with these elastic component 3 swings, wherein this locating part 4 has one and is sphenoid and is positioned at the outer clamping part 41 of this opening 12, and the operation plate body of a suitable length is extended on these clamping part 41 tops, the flattened side of this sphenoid of mat is come backstop to live this battery 2 and is stopped this battery 2 with this operation plate body, be with, when being equiped with this battery 2 in this battery room 11, but the elastic force of this this elastic component 3 of locating part 4 mats remains on the position that can be connected to these battery 2 one sides, so that this battery 2 is limited in this battery room 11, avoid this battery 2 to deviate from from this battery room 11.
See also shown in Figure 4, in present embodiment, this elastic component 3 further is equipped with a combined hole 31 in contiguous free end, and this locating part 4 is except that having this clamping part 41, further protrude out a fixed leg 42, the fixed leg 42 of this locating part 4 is embedded in the combined hole 31 of this elastic component 3, and this elastic component 3 can closely be connected each other with this locating part 4 by this; Comprehensive the above, can think and be, this combined hole 31 also can be exchanged mutually with this fixed leg 42, promptly this elastic component 3 protrudes out this fixed leg 42, and this locating part 4 wears this combined hole 31, the fixed leg 42 of this elastic component 3 is embedded in the combined hole 31 of this locating part 4.
In addition, for the battery room 11 of this battery 2 from electronic installation withdrawed from, can one yoke frame 5 further be set in these battery room 11 bottoms, this yoke frame 5 can be form of springs or shell fragment form, in the present embodiment, this yoke frame 5 is a spring, by this when this battery 2 is placed in this battery room 11, this battery 2 is resisted against this yoke frame 5, make this yoke frame 5 by compression, in case this battery 2 breaks away from stopping of these clamping parts 41, this yoke frame 5 is elastic recovery and promote this battery 2 immediately, and this battery 2 is withdrawed from from the battery room 11 of this electronic installation; By the above, can think and be, this yoke frame 5 also can replace by plural conductive shell fragment 6, this plural conductive shell fragment 6 provides the electric connection between the assembly (figure does not show) in this battery 2 and this electronic installation, electric power with this battery 2 can be used by this, this plural conductive shell fragment 6 is except the media of being used as conduct power, also because the design of bending like this and the collocation of metal material, make this plural conductive shell fragment 6 have certain elastic force, therefore this plural conductive shell fragment 6 can be used as the assembly that withdraws from this battery 2, so when making, can not need make the battery room 11 of this yoke frame 5 in this electronic installation, but directly replace with this plural conductive shell fragment 6, in the present embodiment, this yoke frame 5 is together to be made in the battery room 11 of this electronic installation with this plural conductive shell fragment 6.
See also shown in Figure 5, Fig. 5 is user mode figure of the present utility model, when this battery 2 is installed, this this locating part 4 of battery 2 pushing tows, because this locating part 4 is connected in the free end of this elastic component 3, and an end of this elastic component 3 is connected and fixed on this fuselage body 1, so the free end of this elastic component 3 begins swing, this locating part 4 is removed from this opening 12, and then exposed complete opening 12 so that allow this battery 2 be placed in this battery room 11 by this opening 12 smoothly.
See also shown in Figure 6, owing to loading this battery 2 in the way of this battery room 11, this elastic component 3 is subjected to the influence thereby the stress deformation of this locating part 4, but when this battery 2 is placed in this battery room 11 and this battery 2 when no longer pushing against this locating part 4 fully, 3 of this elastic components are as the spring-like home position that automatically returns to, and then allow this battery 2 of clamping part 41 snap fit of this locating part 4, avoid this battery 2 to deviate from and cause electronic installation to decommission from this battery room 11.In addition, see also (Fig. 7 is the cross-sectional schematic of symbol 7-7 among Fig. 4) shown in Figure 7, has an interval D between this elastic component 3 and this battery 2, this interval D prevents to be placed in battery 2 these elastic components 3 of pushing and pressing of this battery room 11 by this and then the locating part 4 of this battery 2 of snap fit is broken away from order to isolate this battery 2 and this elastic component 3.
Comprehensive the above, battery position limiting structure of the present utility model has following characteristics:
1, the utility model utilizes serial verb construction design cleverly, does not have the mechanism of any complexity fully, can provide as spring-like elastic recovery function.
2, of the present utility modelly simple in structurely can save cost of manufacture, and effectively reduce built-up time.
3, the utility model utilizes fuselage body to grow the elasticity of plastics arm, in order to provide buckle elastic force to automatically return to the home position.
4, the utility model need not to use spring, just can provide elastic force, allows locating part return back to home position and then this battery of snap fit.
5, the utility model processing ease is smoothly very convenient, has practicality.
But the above only is preferred embodiment of the present utility model; non-ly be intended to limit to scope of patent protection of the present utility model; so the equivalence of using the utility model specification and graphic content to do such as changes, and all in like manner all is contained in the rights protection scope of the present utility model, closes and gives Chen Ming.
Claims (10)
1, a kind of battery position limiting structure, it is arranged at the fuselage body of electronic installation, and the fuselage body of this electronic installation is provided with an ostiolate battery room, sees through this opening and can install a battery in this battery room, it is characterized in that this battery position limiting structure includes:
One elastic component, integrated this fuselage body that is connected in of an end be near this battery room place, and the other end of this elastic component then is one to extend and can swing freely free end toward this opening direction; And
One locating part, it is incorporated into the free end of this elastic component and exposes to this opening, when being equiped with this battery in this battery room, but the elastic force of this this elastic component of locating part mat remains on the position that can be connected to this battery one side, so that this battery is limited in this battery room.
2, battery position limiting structure as claimed in claim 1 is characterized in that: this elastic component is an elastic arm.
3, battery position limiting structure as claimed in claim 1 is characterized in that: have one between this elastic component and this battery at interval.
4, battery position limiting structure as claimed in claim 1 is characterized in that: this locating part has one and is sphenoid and is positioned at the outer clamping part of this opening, and the flattened side backstop of this sphenoid of mat is lived this battery.
5, battery position limiting structure as claimed in claim 1 is characterized in that: this elastic component is in being equipped with a combined hole near free end, this locating part has a fixed leg, and this fixed leg embeds and is fixed in this combined hole.
6, battery position limiting structure as claimed in claim 1 is characterized in that: this elastic component is in convexing with a fixed leg near free end, this locating part is equipped with a combined hole, and this fixed leg embeds and is fixed in this combined hole.
7, battery position limiting structure as claimed in claim 1 is characterized in that: this fuselage body further is provided with one in order to replace the yoke frame of this battery in this battery room bottom.
8, battery position limiting structure as claimed in claim 7 is characterized in that: this yoke frame is a spring or a shell fragment.
9, battery position limiting structure as claimed in claim 1 is characterized in that: this elastic component is a working of plastics.
10, battery position limiting structure as claimed in claim 1 is characterized in that: the material of the fuselage body of this electronic installation is a plastic material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008201370881U CN201319384Y (en) | 2008-10-24 | 2008-10-24 | Battery limiting structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008201370881U CN201319384Y (en) | 2008-10-24 | 2008-10-24 | Battery limiting structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201319384Y true CN201319384Y (en) | 2009-09-30 |
Family
ID=41198146
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2008201370881U Expired - Fee Related CN201319384Y (en) | 2008-10-24 | 2008-10-24 | Battery limiting structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201319384Y (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105789677A (en) * | 2016-03-29 | 2016-07-20 | 惠州金源精密自动化设备有限公司 | Limiting battery layer assembly fixture and assembly equipment thereof |
| CN108336269A (en) * | 2018-01-31 | 2018-07-27 | 苏州科瓴精密机械科技有限公司 | A kind of battery cabin door structure and toolroom machine |
-
2008
- 2008-10-24 CN CNU2008201370881U patent/CN201319384Y/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105789677A (en) * | 2016-03-29 | 2016-07-20 | 惠州金源精密自动化设备有限公司 | Limiting battery layer assembly fixture and assembly equipment thereof |
| CN105789677B (en) * | 2016-03-29 | 2019-01-04 | 惠州金源精密自动化设备有限公司 | A kind of battery limiting group layer fixture and its assembling equipment |
| CN108336269A (en) * | 2018-01-31 | 2018-07-27 | 苏州科瓴精密机械科技有限公司 | A kind of battery cabin door structure and toolroom machine |
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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: 20090930 Termination date: 20151024 |
|
| EXPY | Termination of patent right or utility model |