CN208939024U - A kind of buckle structure of battery and unmanned plane - Google Patents
A kind of buckle structure of battery and unmanned plane Download PDFInfo
- Publication number
- CN208939024U CN208939024U CN201821116642.8U CN201821116642U CN208939024U CN 208939024 U CN208939024 U CN 208939024U CN 201821116642 U CN201821116642 U CN 201821116642U CN 208939024 U CN208939024 U CN 208939024U
- Authority
- CN
- China
- Prior art keywords
- battery
- shell
- buckle structure
- key
- vehicle body
- 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
-
- 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
- Battery Mounting, Suspending (AREA)
Abstract
The utility model discloses a kind of buckle structure of battery, battery is mounted on unmanned aerial vehicle body by buckle structure, and buckle structure is provided on battery at least side, and buckle structure includes: key, battery includes the battery core of shell and setting inside the shell, is provided with the first via hole on side wall of outer shell；Key is installed inside the shell, and one end is put in the first via hole；Fastener is keyed with pressing, and the second via hole is provided on side wall of outer shell, and pressing keys drive fastener to stretch out shell or retraction shell via the second via hole；Block button hole is provided on unmanned aerial vehicle body with fastener corresponding position, fastener is stretched out after shell and sticked into block button hole, realizes the locking of battery and unmanned aerial vehicle body.The utility model additionally provides a kind of unmanned plane using above-mentioned buckle structure of battery.The advantages that buckle structure of battery provided by the utility model has structure simple, occupies little space, easy to operate.
Description
Technical field
The utility model relates to unmanned aerial vehicle design technical fields, and in particular to a kind of buckle structure of battery and use the battery
The unmanned plane of buckle structure.
Background technique
Unmanned plane is widely used because to have the advantages that maneuverability, rapid reaction, unmanned flight, operation require low for it
In fields such as agricultural, exploration, photography, border patrols.
Detachable battery, the locking solution between existing battery and unmanned aerial vehicle body are usually provided on unmanned aerial vehicle body
Structure is complicated for latch mechanism, and inconvenient for operation.
Utility model content
In order to solve the problems, such as that existing unmanned plane battery lock unlocking structure is complicated, the utility model provides a kind of battery
Buckle structure, battery are mounted on unmanned aerial vehicle body by buckle structure, and the battery is provided with buckle structure at least side,
The buckle structure includes:
Key, the battery include shell and the battery core that is arranged in the shell, and the is provided on the side wall of outer shell
One via hole；The key is mounted in the shell, and one end is put in first via hole；
Fastener is provided with the second via hole on the side wall of outer shell by being keyed with described, presses the key and drive institute
It states fastener and stretches out the shell or the retraction shell via second via hole；On the unmanned aerial vehicle body with the card
Fastener corresponding position is provided with block button hole, and the fastener is stretched out after the shell and sticked into the block button hole, realizes institute
State the locking of battery Yu the unmanned aerial vehicle body.
Preferably, being provided with buckle structure on two symmetrical side of described battery or so.
Preferably, be provided with bracket in the shell, the key is towards being vertically installed in the one side in the shell
One pillar；One end of the pillar is fixedly connected with the key, and the other end is placed on the bracket, and the key and the branch
Elastic component is provided between frame；
The key is pressed, the key compresses the elastic component and moves into the shell, while pillar is along the branch
Frame axial movement.
Preferably, the elastic component is a spring, the spring is set on the pillar, and both ends be against respectively it is described
On key side and the side of the bracket.
Preferably, the cradle top is provided with a recess, the other end of the pillar is placed in the recess.
Preferably, the key is towards being arranged textured portion in the one side of the outer side of shell.
Preferably, the shell includes upper cover and lower casing, the upper cover lid is located on the lower casing and connects formation one
Place the chamber resettling of battery core；First via hole, the second via hole are arranged on the upper cover side wall, and the bracket is arranged in institute
It states in lower casing inside bottom.
The utility model additionally provides a kind of unmanned plane, includes unmanned aerial vehicle body and setting on the unmanned aerial vehicle body
Battery, which is characterized in that the battery is realized and the lock of the unmanned aerial vehicle body using buckle structure of battery as described above
Fixed, unlock.
Preferably, battery installation position is provided with guide groove on the unmanned aerial vehicle body, it is provided on the battery side wall
Guide frame, the guide frame inject in the guide groove.
The utility model due to using the technology described above, is allowed to compared with prior art, have the following advantages that and accumulate
Pole effect:
Buckle structure of battery provided by the utility model drives fastener to stretch out directly by pressing keys to link
Or in retraction shell, fastener stretches out or retracts shell realization and locks or unlocks with the block button hole realization on unmanned aerial vehicle body；It should
The advantages that buckle structure of battery has structure simple, occupies little space, easy to operate.
Detailed description of the invention
In conjunction with attached drawing, by hereafter state detailed description, can be more clearly understood that the above-mentioned and other spy of the utility model
It seeks peace advantage, in which:
Fig. 1 is the overall structure diagram of battery in the utility model；
Fig. 2 is the fractionation schematic diagram of battery in the utility model；
Fig. 3 is the cross-sectional view in the utility model at buckle structure of battery.
Symbol description:
1- shell, 101- upper cover, the first via hole of 1011-, the second via hole of 1012-, 102- lower casing, 1021- bracket, 1022-
Recess, 2- battery, 3- buckle structure, 301- key, 302- fastener, 303- pillar, 304- elastic component, 4- guide frame.
Specific embodiment
Referring to the attached drawing for showing the utility model embodiment, the utility model is described in more detail.However, this reality
It can be realized in many different forms with novel, and should not be construed as being limited by the embodiment herein proposed.On the contrary, proposing
These embodiments be in order to reach sufficiently and complete disclosure, and make those skilled in the art understands completely this it is practical newly
The range of type.In these attached drawings, for clarity, the size and relative size in layer and region may be exaggerated.
Embodiment 1
Referring to Fig.1-2, the utility model provides a kind of buckle structure of battery, and battery is mounted on nobody by buckle structure
On machine fuselage；It is provided with buckle structure on battery at least side, battery includes shell 1 and the battery core 2 that is arranged in shell 1, card
Buckle structure 3 is arranged inside the shell；Specifically, being provided with the first via hole 1011 on 1 side wall of shell, key 301 is located in shell 1,
And one end is put in the first via hole 1011；The second via hole 1012 is additionally provided on 1 side wall of shell, fastener 302 is located at the second mistake
At 1012 position of hole；Pressing keys 301 drive fastener 302 mobile to which the second via hole 1012 stretches out shell 1 or retraction is outer
In shell 1.
Block button hole is provided on unmanned aerial vehicle body with 302 corresponding position of fastener, fastener 302 passes through the second via hole
It after 1012 stretching shells 1 and sticks into block button hole, realizes the locking of battery and unmanned aerial vehicle body.
Buckle structure of battery provided by the utility model drives fastener to stretch directly by pressing keys 301 to link
Out or in retraction shell 1, fastener 302 stretches out or retracts shell realization and realizes locking or solution with the block button hole on unmanned aerial vehicle body
Lock；The advantages that buckle structure of battery has structure simple, occupies little space, easy to operate.
In the present embodiment, it is provided with buckle structure 3 on two symmetrical side of battery or so, as Figure 2-3；The present embodiment
It is respectively arranged with buckle structure 3 on battery two sides, advantageously ensures that the stability that battery is connect with unmanned aerial vehicle body；Certainly,
In other embodiments, the setting number of buckle structure 3 and setting position can be adjusted as the case may be on battery,
Such as the buckle structure 3 for a buckle structure 3 or three being provided on battery case or more, herein it is uniformly distributed with no restrictions.
In the present embodiment, as shown in Figure 2, the lower end of key 301 is arranged in by connector for fastener 302, corresponding
The second via hole 1012 on shell 1 is also disposed at the lower section of the first via hole 1011；Wherein, 301 one of fastener 301 and key
It is made.
In the present embodiment, buckle structure 3 is mounted in shell 1 by bracket 1021.Specifically, being provided in shell 1
Bracket 1021, key 302 is towards being vertically installed with a pillar 303 in the one side in shell 1；One end of pillar 303 and key
301 are fixedly connected, and the other end is placed on bracket 303；Key 302 is located at the first via hole 1011, the first via hole 1011 and bracket
1021 support buckle structure jointly, and when pressing keys 302, key 302 is mobile relative to the first via hole 1011, pillar
303 is mobile relative to bracket.
Further, a recess 1022 is provided at the top of bracket 1022, the other end of pillar 303 is placed in recess 1022；
The present embodiment plays limit to pillar 303 radially by the setting of recess 1022, avoid the other end of pillar 303 with
Meaning movement；Wherein, the shape of recess 1022 is matched with the cross sectional shape of pillar 303, if such as pillar 303 section it is rounded,
The corresponding semicircular in shape of recess 1022, if corresponding recess 1022 is also in rectangle in another example the section of pillar 303 is in rectangle, this
Place is with no restrictions.
In the present embodiment, elastic component 304 is provided between key 301 and bracket 1022, under the action of elastic component 304
Case 301 drives fastener 302 to stretch out shell 1 always；In use process, pressing keys 301 are into shell 1 when the movement of side
It waits, 301 compression elastic piece 304 of key, key drives fastener 302 to be retracted in shell 1 at this time, realizes lock function；Work as release
After key 301, under the action of 304 elastic force of elastic component, push the side to outside shell of key 301 mobile, key 301 drives buckle
Part 302 is retracted in shell 1, realizes unlocking function.
Further, elastic component 304 is a spring, and spring is set on pillar 303, and both ends are against key 301 respectively
On the side of medial surface and bracket 1021.Certainly, the structure type and mounting means of elastic component in other embodiments
It is adjusted as the case may be, herein not with no restrictions.
In the present embodiment, key 301 is towards being arranged textured portion in the one side in the outside of shell 1, texture portion specifically by
Several tactic vertical lines are constituted.The present embodiment is by the setting in texture portion, to increase finger and when key 301 contacts
Frictional force, consequently facilitating operation, while increasing operating handle.
Fig. 2 is referred again to, shell 1 includes upper cover 101 and lower casing 102 in the present embodiment, and the lid of upper cover 101 is located on lower casing
102 and connect the chamber resettling to form a placement battery core 2.
Wherein, the modes such as viscose, buckle or ultrasonic bonding realize connection between upper cover 101 and lower casing 102, herein not
It is limited.
Wherein, the first via hole 1011, the second via hole 1012 are arranged on 101 side wall of upper cover, and bracket 1021 is arranged in lower casing
In 102 inside bottoms.
Certainly, in other embodiments the shape of battery case be not limited to it is illustrated above, can as the case may be into
Row adjustment, herein with no restrictions.
Embodiment 2
The present embodiment additionally provides a kind of unmanned plane, includes unmanned aerial vehicle body and the electricity that is arranged on unmanned aerial vehicle body
Pond；Wherein, battery realizes locking, unlock with unmanned aerial vehicle body using buckle structure of battery described in embodiment 1, herein not
It repeats again.
In the present embodiment, battery installation position is provided with guide groove on unmanned aerial vehicle body, on battery side wall along its length
Direction is provided with a guide frame, as shown in fig. 1；Battery injects guide groove by guide frame and slides along realization installation
Guiding role.
Those skilled in the art should be understood that the utility model can be realized with many other concrete forms without de-
Spirit or scope from itself.Although the case study on implementation of the utility model has been described, it should be understood that the utility model should not limit
Be made as these embodiments, those skilled in the art can as defined by the following claims the spirit of the utility model and
Within the scope of make change and modification.
Claims (9)
1. a kind of buckle structure of battery, battery are mounted on unmanned aerial vehicle body by buckle structure, which is characterized in that the battery
Buckle structure is at least provided on side, the buckle structure includes:
Key, the battery include shell and the battery core that is arranged in the shell, are provided with the first mistake on the side wall of outer shell
Hole；The key is mounted in the shell, and one end is put in first via hole；
Fastener is provided with the second via hole on the side wall of outer shell by being keyed with described, presses the key and drive the card
Fastener stretches out the shell or the retraction shell via second via hole；On the unmanned aerial vehicle body with the fastener
Corresponding position is provided with block button hole, and the fastener is stretched out after the shell and sticked into the block button hole, realizes the electricity
The locking in pond and the unmanned aerial vehicle body.
2. buckle structure of battery according to claim 1, which is characterized in that be respectively provided on two symmetrical side of described battery or so
There is buckle structure.
3. buckle structure of battery according to claim 1, which is characterized in that bracket is provided in the shell, it is described to press
Key is towards being vertically installed with a pillar in the one side in the shell；One end of the pillar is fixedly connected with the key, another
End is placed on the bracket, and is provided with elastic component between the key and the bracket；
The key is pressed, the key compresses the elastic component and moves into the shell, while pillar is along the support shaft
To movement.
4. buckle structure of battery according to claim 3, which is characterized in that the elastic component is a spring, the spring
It is set on the pillar, and both ends are against respectively on the key side and the side of the bracket.
5. buckle structure of battery according to claim 3, which is characterized in that the cradle top is provided with a recess, institute
The other end for stating pillar is placed in the recess.
6. buckle structure of battery according to claim 1, which is characterized in that the key towards the outer side of shell one
Textured portion is set on face.
7. buckle structure of battery according to claim 3, which is characterized in that the shell includes upper cover and lower casing, institute
Upper cover lid is stated to be located on the lower casing and connect the chamber resettling to form a placement battery core；First via hole, the second via hole are set
It sets on the upper cover side wall, the bracket is arranged in the lower casing inside bottom.
The battery that 8. a kind of unmanned plane includes unmanned aerial vehicle body and is arranged on the unmanned aerial vehicle body, which is characterized in that institute
State battery using the buckle structure of battery described in any one of claim 1-7 realize locking with the unmanned aerial vehicle body,
Unlock.
9. unmanned plane according to claim 8, which is characterized in that battery installation position is provided on the unmanned aerial vehicle body
Guide groove, guide frame is provided on the battery side wall, and the guide frame injects in the guide groove.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821116642.8U CN208939024U (en) | 2018-07-13 | 2018-07-13 | A kind of buckle structure of battery and unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821116642.8U CN208939024U (en) | 2018-07-13 | 2018-07-13 | A kind of buckle structure of battery and unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208939024U true CN208939024U (en) | 2019-06-04 |
Family
ID=66716135
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821116642.8U Active CN208939024U (en) | 2018-07-13 | 2018-07-13 | A kind of buckle structure of battery and unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208939024U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112350020A (en) * | 2020-10-30 | 2021-02-09 | 浙江大华技术股份有限公司 | Battery pack fixing structure, battery pack and shooting equipment |
-
2018
- 2018-07-13 CN CN201821116642.8U patent/CN208939024U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112350020A (en) * | 2020-10-30 | 2021-02-09 | 浙江大华技术股份有限公司 | Battery pack fixing structure, battery pack and shooting equipment |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106760988B (en) | A kind of slim padlock easily to operate | |
| CN208939024U (en) | A kind of buckle structure of battery and unmanned plane | |
| CN205273582U (en) | Seat pocket and children's shallow of hasp, children's shallow | |
| CN207264115U (en) | The connection structure and wrist-watch of a kind of wrist-watch | |
| CN103151646A (en) | Quick unlocking structure of electric connector | |
| CN109209069A (en) | Unblock button mechanism | |
| CN205935941U (en) | Two manual -automatic locks of holding up | |
| CN209023140U (en) | A kind of battery lock unlocking mechanism and unmanned plane | |
| CN209891889U (en) | U-shaped intelligent mortise lock | |
| CN110512959A (en) | A kind of electronic lock body | |
| CN207044612U (en) | Secondary demolding mechanism | |
| CN103850538A (en) | Coded lock | |
| CN108939271A (en) | A kind of novel more kinetic energy gynecological administration devices | |
| CN205743371U (en) | Mortise bolt | |
| CN211776604U (en) | A electron intelligence lock structure for case and bag | |
| CN209799634U (en) | Lock catch for safety lock | |
| CN208996583U (en) | Lock and vehicle for vehicle | |
| CN206928785U (en) | One kind has a spoon digital intelligent-controlled lock core | |
| CN208993375U (en) | A kind of push button drawing pin | |
| CN208211622U (en) | A kind of tamper chest card | |
| CN209799629U (en) | Door lock device | |
| CN207486032U (en) | Lockup switch and with its vehicle | |
| CN214659433U (en) | Intelligent electronic lock | |
| CN215056221U (en) | Rack slider type intelligent lock with multiple stations | |
| CN210978079U (en) | Lock catch mechanism |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |