CN205376594U - Unmanned aerial vehicle battery lock decides structure, unmanned aerial vehicle battery pack and unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle battery lock decides structure, unmanned aerial vehicle battery pack and unmanned aerial vehicle Download PDFInfo
- Publication number
- CN205376594U CN205376594U CN201521063533.0U CN201521063533U CN205376594U CN 205376594 U CN205376594 U CN 205376594U CN 201521063533 U CN201521063533 U CN 201521063533U CN 205376594 U CN205376594 U CN 205376594U
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- CN
- China
- Prior art keywords
- battery
- rear cover
- unmanned plane
- cell rear
- buckle
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- 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
The utility model is suitable for an unmanned air vehicle technique field provides an unmanned aerial vehicle battery lock decides structure, unmanned aerial vehicle battery pack and unmanned aerial vehicle, the locking structure is used for installing to be covered behind the battery, rotate including one end and connect covering just behind the battery, other end lock is in the locking handle covered behind the battery, install cover behind the battery and be used for and buckle, the setting of locking handle lock are in locking handle below and with the button of unblanking of going together down behind the buckle lock and moving to and both ends difference fixed connection is in the elastic component of covering behind buckle and the battery. Unmanned aerial vehicle battery pack includes foretell locking structure, unmanned aerial vehicle includes foretell unmanned aerial vehicle battery pack. The utility model discloses make the user can cover behind the battery locking the handle lock through the less application of force, during removable battery, upwards press button alright the drive buckle upward movement of unblanking to make buckle and the locking handle to throw off locking handle rotatable opening in order conveniently to take out the battery still.
Description
Technical field
This utility model belongs to unmanned air vehicle technique field, particularly relates to a kind of unmanned plane battery lock structure, unmanned plane battery component and unmanned plane.
Background technology
In prior art, unmanned plane has been applied in many industries.Its battery lock structure is generally adopted the buckle on the plastic shell of battery and fuselage locking, and intensity is relatively low, it is easy to fracture, and user needs firmly pressing plastic cement buckle when dismantling battery, is unfavorable for operation.
Utility model content
The purpose of this utility model is in that to overcome above-mentioned the deficiencies in the prior art, it is provided that a kind of unmanned plane battery lock structure, and it can pass through less force and easily with unmanned aerial vehicle body locking, battery be conciliate open locking.
This utility model is achieved in that and provides a kind of unmanned plane battery lock structure, for being arranged on cell rear cover, be rotatably connected on described cell rear cover including one end and the other end be fastened on the lock handle on described cell rear cover, be arranged on described cell rear cover and for the buckle fastened with described lock handle, be arranged on below described lock handle and fasten with described buckle after together with the button of unblanking that moves up and down, and two ends are respectively fixedly connected with the elastic component on described buckle and cell rear cover.
Further, described latch-up structure also includes the rotating shaft being arranged on described cell rear cover, and is set in the torsion spring in described rotating shaft, and one end of described torsion spring is connected on described cell rear cover, and the other end is connected on the inwall of described lock handle.
Further, described lock handle is provided with two projections near the side of described cell rear cover, each described projection offers the axis hole for described rotating shaft traverse, described cell rear cover offers the location hole corresponding with described axis hole.
Further, described latch-up structure also includes being arranged on described roller end and for limiting described rotating shaft rotating shaft fixed block axially movable.
Further, described lock handle has dead bolt near one end of described projection is extended.
Further, described lock handle is provided with through hole.
Further, described cell rear cover being provided with plastic cement post, described elastic component is set on described plastic cement post away from one end of described buckle；Described latch-up structure also includes the meson screw for being locked at by described elastic component on described plastic cement post.
Preferably, described lock handle is metallic article.
This utility model additionally provides a kind of unmanned plane battery component, including battery main body, the battery being housed in described battery main body, cover the cell rear cover being located at described battery main body one end, and be arranged on described cell rear cover and unmanned plane battery lock structure as described above.
This utility model additionally provides a kind of unmanned plane, including unmanned plane battery component described above.
Implement a kind of unmanned plane battery lock structure of the present utility model, have the advantages that by arranging the lock handle that one end is rotatably connected on cell rear cover and the other end is fastened on cell rear cover, and on cell rear cover, it is provided with buckle, unblank button and elastic component, this buckle fastens with lock handle and button of unblanking respectively, the two ends of elastic component are respectively fixedly connected with on buckle and cell rear cover, make to be fastened on cell rear cover by lock handle by less force, during dismounting battery, pressing up button of unblanking just can drive buckle to move upward, so that buckle disengages with lock handle, lock handle also rotatably opens to facilitate to take out battery.
Accompanying drawing explanation
In order to be illustrated more clearly that the technical scheme in this utility model embodiment, the accompanying drawing used required in embodiment will be briefly described below, 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.
Fig. 1 is the explosive view of the unmanned plane battery component that this utility model embodiment provides；
Fig. 2 is the perspective view of the unmanned plane battery component that this utility model embodiment provides；
Fig. 3 is the phantom of the unmanned plane battery component that this utility model embodiment provides；
Fig. 4 is the perspective view of the lock handle that this utility model embodiment provides；
Fig. 5 is the perspective view of the cell rear cover that this utility model embodiment provides.
Detailed description of the invention
In order to make the purpose of this utility model, technical scheme and advantage clearly understand, below in conjunction with drawings and Examples, this utility model is further elaborated.Should be appreciated that specific embodiment described herein is only in order to explain this utility model, be not used to limit this utility model.
It should be noted that be referred to as " being fixed on " or " being arranged at " another element when element, it can directly on another element or may be simultaneously present centering elements.When an element is known as " being connected to " another element, it can be directly to another element or may be simultaneously present centering elements.
Also, it should be noted the orientation term such as left and right, upper and lower in this utility model embodiment, be only relative concept or with the normal operating condition of product for reference each other, and should not be regarded as have restrictive.
As shown in Figure 1, Figure 2 and Figure 3, the unmanned plane battery lock structure that this utility model embodiment provides, it is used for being arranged on cell rear cover 2, unties this latch-up structure and replaceable battery.This latch-up structure specifically includes lock handle 3, buckle 4, unblank button 5 and elastic component 6.Wherein, one end of lock handle 3 is rotatably connected on cell rear cover 2, and the other end of lock handle 3 is fastened on cell rear cover 2.Buckle 4 is arranged on cell rear cover 2 and for fastening with lock handle 3, during dismounting battery, untie the fastening of lock handle 3 and buckle 4, the one end making lock handle 3 departs from cell rear cover 2, and be flipped up under being rotationally connected of the other end of lock handle 3, and then battery can be taken off from battery compartment.Unblank button 5 be arranged on the lower section of lock handle 3 and fasten with buckle 4 after can together with move up and down, after the button 5 of namely unblanking fastens with buckle 4, the button 5 moving up of unblanking, the fastening of handle 3 so that buckle 4 goes out of lock can be pressed, and then open lock handle 3.The two ends of elastic component 6 are respectively fixedly connected with on buckle 4 and cell rear cover 2, and elastic component 6 is in extended state.Preferably, elastic component 6 is extension spring.
This utility model embodiment is by arranging the lock handle 3 that one end is rotatably connected on cell rear cover 2 and the other end is fastened on cell rear cover 2, and on cell rear cover 2, it is provided with buckle 4, unblank button 5 and elastic component 6, this buckle 4 fastens with lock handle 3 and button 5 of unblanking respectively, the two ends of elastic component 6 are respectively fixedly connected with on buckle 4 and cell rear cover 2, make to be fastened on cell rear cover 2 by lock handle 3 by less force, during dismounting battery, pressing up button 5 of unblanking just can drive buckle 4 to move upward, so that buckle 4 and lock handle 3 disengage, lock handle 3 also rotatably opens to facilitate to take out battery.
Further, the latch-up structure of this utility model embodiment also includes rotating shaft 7 and torsion spring 8.Wherein, rotating shaft 7 is arranged on cell rear cover 2, and torsion spring 8 is set in rotating shaft 7, and one end of this torsion spring 8 is connected on cell rear cover 2, and the other end is connected on the inwall of lock handle 3.When lock handle 3 and buckle 4 depart from and fasten, lock handle 3 can upwards flick under the effect of torsion spring 8, to be convenient for changing battery.
Specifically, as shown in Figure 4, two projections 31 it are provided with near the side of cell rear cover 2 at lock handle 3, two projections 31 set up separately in the both sides of lock handle 3, and on each protruding 31, offer the axis hole 311 extending transversely through this projection 31, this axis hole 311 is for for rotating shaft 7 traverse, and the two ends of rotating shaft 7 correspondence respectively is through the axis hole 311 of two projections 31, and torsion spring 8 is set on the rotating shaft 7 position between two axis holes 311.Accordingly, as it is shown in figure 5, offer the location hole 21 corresponding with above-mentioned axis hole 311 on cell rear cover 2.Specifically, cell rear cover 2 offers hole 21, two location.
Further, the latch-up structure of this utility model embodiment also includes being arranged on rotating shaft 7 end and for limiting rotating shaft 7 rotating shaft fixed block 9 axially movable.It is understood that rotating shaft fixed block 9 can be respectively provided with in the end, two ends of rotating shaft 7, it is also possible to by one end end abutment of rotating shaft 7 on cell rear cover 2, and arrange rotating shaft fixed block 9 on the other end end of rotating shaft 7.
Further, extended there is dead bolt 32 at lock handle 3 near one end of protruding 31.This dead bolt 32 can tilt when installing battery, locks with unmanned aerial vehicle body, and this dead bolt 32 can decline when dismantling battery and disengage and the locking of fuselage.
Further, lock handle 3 is additionally provided with through hole 33.By this through hole 33 namely it can be seen that the power supply indicator being positioned on cell rear cover 2.
Further, being provided with plastic cement post on cell rear cover 2, elastic component 6 is set on plastic cement post away from one end of buckle 4.The latch-up structure of this utility model embodiment also includes the meson screw 10 for being locked at by elastic component 6 on plastic cement post.It is understood that elastic component 6 can also be otherwise fixed on cell rear cover 2.
Further, lock handle 3 is made up of metal material, it is possible to ensureing integrally-built intensity, reliability is higher.Preferably, lock handle 3 is made up of aluminum alloy materials.
Battery, when installing battery, is pushed unmanned plane battery compartment, is pressed down on by lock handle 3 by this utility model embodiment, until blocking with buckle 4, in pressing process, the dead bolt 32 above lock handle 3 can tilt, and locks with unmanned aerial vehicle body；During dismounting battery, button 5 of unblanking presses up, button 5 of unblanking can drive buckle 4 upward sliding together, and disengage with lock handle 3, elastic force effect due to torsion spring 8, lock handle 3 can be upspring automatically, and dead bolt 32 decline disengages the locking with fuselage, and user holds lock handle 3 and battery pulls out unmanned plane battery compartment.
This utility model additionally provides a kind of unmanned plane battery component, it includes battery main body 1, be housed in battery main body 1 battery, lid are located at the cell rear cover 2 of one end of battery main body 1, and are arranged on cell rear cover 2 and unmanned plane battery lock structure as described above.
This utility model additionally provides a kind of unmanned plane, and it includes unmanned plane battery component described above.
In sum, implement a kind of unmanned plane battery lock structure of the present utility model, unmanned plane battery component and unmanned plane, it is by arranging the lock handle 3 that one end is rotatably connected on cell rear cover 2 and the other end is fastened on cell rear cover 2, and on cell rear cover 2, it is provided with buckle 4, unblank button 5 and elastic component 6, this buckle 4 fastens with lock handle 3 and button 5 of unblanking respectively, the two ends of elastic component 6 are respectively fixedly connected with on buckle 4 and cell rear cover 2, make to be fastened on cell rear cover 2 by lock handle 3 by less force, during dismounting battery, pressing up button 5 of unblanking just can drive buckle 4 to move upward, so that buckle 4 and lock handle 3 disengage, lock handle 3 also rotatably opens to facilitate to take out battery.Meanwhile, during dismounting battery, user can be gripped easily and pull out battery for the lock handle 3 automatically upspring, and can promote Consumer's Experience.
The foregoing is only preferred embodiment of the present utility model, not in order to limit this utility model, all any amendment, equivalent replacement or improvement etc. made within spirit of the present utility model and principle, should be included within protection domain of the present utility model.
Claims (10)
1. a unmanned plane battery lock structure, it is characterized in that, for being arranged on cell rear cover (2), it is rotatably connected on the lock handle (3) that described cell rear cover (2) is gone up and the other end is fastened on described cell rear cover (2) including one end, it is arranged on described cell rear cover (2) and above and is used for the buckle (4) fastened with described lock handle (3), the button of unblanking (5) moved up and down together with after being arranged on described lock handle (3) lower section and fastening with described buckle (4), and two ends are respectively fixedly connected with the elastic component (6) on described buckle (4) and cell rear cover (2).
2. unmanned plane battery lock structure as claimed in claim 1, it is characterized in that, described latch-up structure also includes the rotating shaft (7) being arranged on described cell rear cover (2), and it is set in the torsion spring (8) in described rotating shaft (7), one end of described torsion spring (8) is connected on described cell rear cover (2), and the other end is connected on the inwall of described lock handle (3).
3. unmanned plane battery lock structure as claimed in claim 2, it is characterized in that, described lock handle (3) is provided with two projections (31) near the side of described cell rear cover (2), each described projection (31) offers the axis hole (311) for described rotating shaft (7) traverse, described cell rear cover (2) offers the location hole (21) corresponding with described axis hole (311).
4. unmanned plane battery lock structure as claimed in claim 3, it is characterised in that described latch-up structure also includes being arranged on described rotating shaft (7) end and being used for limiting described rotating shaft (7) rotating shaft fixed block (9) axially movable.
5. unmanned plane battery lock structure as claimed in claim 3, it is characterised in that one end of the close described projection (31) of described lock handle (3) is extended dead bolt (32).
6. unmanned plane battery lock structure as claimed in claim 1, it is characterised in that be provided with through hole (33) on described lock handle (3).
7. unmanned plane battery lock structure as claimed in claim 1, it is characterised in that being provided with plastic cement post on described cell rear cover (2), described elastic component (6) is set on described plastic cement post away from one end of described buckle (4)；Described latch-up structure also includes the meson screw (10) for being locked at by described elastic component (6) on described plastic cement post.
8. unmanned plane battery lock structure as claimed in claim 1, it is characterised in that described lock handle (3) is metallic article.
9. a unmanned plane battery component, it is characterized in that, including battery main body (1), the battery being housed in described battery main body (1), cover the cell rear cover (2) being located at described battery main body (1) one end, and be arranged on the described cell rear cover (2) unmanned plane battery lock structure above and as described in any one of claim 1-8.
10. a unmanned plane, it is characterised in that include unmanned plane battery component as claimed in claim 9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521063533.0U CN205376594U (en) | 2015-12-17 | 2015-12-17 | Unmanned aerial vehicle battery lock decides structure, unmanned aerial vehicle battery pack and unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521063533.0U CN205376594U (en) | 2015-12-17 | 2015-12-17 | Unmanned aerial vehicle battery lock decides structure, unmanned aerial vehicle battery pack and unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205376594U true CN205376594U (en) | 2016-07-06 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201521063533.0U Expired - Fee Related CN205376594U (en) | 2015-12-17 | 2015-12-17 | Unmanned aerial vehicle battery lock decides structure, unmanned aerial vehicle battery pack and unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205376594U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018024086A1 (en) * | 2016-08-01 | 2018-02-08 | 亿航智能设备（广州）有限公司 | Battery and aircraft |
| WO2018119739A1 (en) * | 2016-12-28 | 2018-07-05 | 深圳市大疆创新科技有限公司 | Battery fixing mechanism, frame of unmanned aerial vehicle, and battery management device |
| CN108513564A (en) * | 2017-04-26 | 2018-09-07 | 深圳市大疆创新科技有限公司 | Electronic equipment |
| WO2023066301A1 (en) * | 2021-10-22 | 2023-04-27 | 深圳市道通智能航空技术股份有限公司 | Battery compartment assembly and unmanned aerial vehicle |
-
2015
- 2015-12-17 CN CN201521063533.0U patent/CN205376594U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018024086A1 (en) * | 2016-08-01 | 2018-02-08 | 亿航智能设备（广州）有限公司 | Battery and aircraft |
| WO2018119739A1 (en) * | 2016-12-28 | 2018-07-05 | 深圳市大疆创新科技有限公司 | Battery fixing mechanism, frame of unmanned aerial vehicle, and battery management device |
| CN108513564A (en) * | 2017-04-26 | 2018-09-07 | 深圳市大疆创新科技有限公司 | Electronic equipment |
| WO2023066301A1 (en) * | 2021-10-22 | 2023-04-27 | 深圳市道通智能航空技术股份有限公司 | Battery compartment assembly and unmanned aerial vehicle |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160706 Termination date: 20191217 |