CN213936418U - Battery compartment structure and unmanned aerial vehicle - Google Patents
Battery compartment structure and unmanned aerial vehicle Download PDFInfo
- Publication number
- CN213936418U CN213936418U CN202022738529.7U CN202022738529U CN213936418U CN 213936418 U CN213936418 U CN 213936418U CN 202022738529 U CN202022738529 U CN 202022738529U CN 213936418 U CN213936418 U CN 213936418U
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- shell
- housing
- cover
- locking
- battery compartment
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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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Abstract
The utility model provides a battery compartment structure and unmanned aerial vehicle, the battery compartment structure includes: a housing for housing a battery; a case cover for sealing the case; the shell cover is mounted on the shell in a matching manner; the locking piece is used for being matched with the locking seat so as to lock the shell and the shell cover; the locking piece is arranged at the first end of the shell cover; the locking seat is used for locking the locking piece; the locking seat is arranged at the first end of the shell and is opposite to the locking piece; the elastic connecting mechanism is used for connecting the shell and the shell cover; the first end of the elastic connecting mechanism is connected with the second end of the shell, and the second end of the elastic connecting mechanism is connected with the second end of the shell cover; when the locking piece is separated from the locking seat, the shell cover and the shell are driven to be separated by the elastic connecting mechanism. The utility model provides a pair of battery compartment structure and unmanned aerial vehicle adopt the torsional spring to install on the erection column of elastic connection mechanism, but torsional spring drive rotation end makes the cap bounce automatically when opening.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle, concretely relates to battery compartment structure and unmanned aerial vehicle.
Background
At present, the application range of multi-rotor unmanned aerial vehicles is wider and wider, and the unmanned aerial vehicles are required to have all-weather working capacity in certain scenes. Therefore, the aspect of the unmanned aerial vehicle organism needs to have certain rain-proof ability. The battery compartment is used as an important waterproof position, and needs to be sealed and convenient for battery replacement. The common hinge structure can open and close the battery compartment cover, but the hinge is provided with an outer leakage part and a gap, and rainwater easily permeates into the battery compartment.
Many composite fuselage multi-rotor and fixed wing drones have adopted the form of ready-made hinges in the design of the battery compartment housing. One end of the hinge is fixed on the machine body, and the other end of the hinge is fixed on the battery compartment shell. When the battery is replaced, the pressing type door lock switch of the battery compartment shell is opened, and then the battery compartment shell is lifted up to replace the battery.
The hinge commonly used in the market has a simple structure, the hinge rotating shaft is positioned at the position of a boundary between the movable end and the fixed end, and a gap is left at the position. The hinge is used for the upper cover of the battery bin of the unmanned aerial vehicle, rainwater easily permeates into the interior of the battery bin from the position, and the hinge is easy to rust and corrode. The locking of the upper cover of the battery compartment usually adopts a slide fastener form, an easily-shifted slide fastener is designed outside the machine body, and after shifting, the upper cover is lifted upwards. This locking, although practical in form, is not aesthetically pleasing and is relatively complex in construction.
SUMMERY OF THE UTILITY MODEL
In view of the above, the present invention provides a battery compartment structure and an unmanned aerial vehicle that overcome the above problems or at least partially solve the above problems.
In order to solve the technical problem, the utility model provides a battery compartment structure, include:
a housing for housing a battery;
a case cover for sealing the case; the shell cover is mounted on the shell in a matching manner;
the locking piece is used for being matched with the locking seat so as to lock the shell and the shell cover; the locking piece is arranged at the first end of the shell cover;
the locking seat is used for locking the locking piece; the locking seat is arranged at the first end of the shell and is opposite to the locking piece;
the elastic connecting mechanism is used for connecting the shell and the shell cover; the first end of the elastic connecting mechanism is connected with the second end of the shell, and the second end of the elastic connecting mechanism is connected with the second end of the shell cover;
when the locking piece is separated from the locking seat, the shell cover and the shell are driven to be separated by the elastic connecting mechanism.
Preferably, the housing includes a receiving cavity in which the battery is placed, and the housing cover completely covers the receiving cavity when the housing cover is fittingly mounted to the housing.
Preferably, the edge of the opening of the housing is protruded outwards to form a flange, and when the housing cover is fittingly mounted on the housing, the flange is tightly attached to the bottom wall of the housing cover.
Preferably, the locking member comprises a locking hook disposed on the bottom wall in the first end of the housing cover.
Preferably, the locking seat comprises a pressing type door lock switch, the outer surface of the first end of the shell is inwards recessed to form an installation groove, the pressing type door lock switch is arranged in the installation groove, and when the shell cover is installed on the shell in an adaptive mode, the lock hook in the locking piece is inserted into the installation groove and fastened with the pressing type door lock switch.
Preferably, the number of the locking member and the locking seat is 2.
Preferably, the elastic connection mechanism includes: stiff end, torsional spring and rotation end, wherein, the stiff end set up in on the first end lateral wall of casing, and outside extension forms the erection column, correspond on the first end lateral wall of casing rotation end department is formed with the dead slot, the first end of rotation end is formed with the lantern ring, lantern ring cover is located on the erection column, the second end of rotation end passes the dead slot and with the interior diapire of cap is connected, the torsional spring cover is located on the erection column, and first end with the stiff end is connected and the second end with the rotation end is connected, the rotation end is in move and realize in the dead slot the casing with opening and shutting of cap.
Preferably, a first fixing hole is formed in the fixing end, and the first end of the torsion spring is inserted into the first fixing hole.
Preferably, a second fixing hole is formed in the rotating end, and the second end of the torsion spring is inserted into the second fixing hole.
The utility model also provides an unmanned aerial vehicle, include as in any one of the above-mentioned battery compartment structure.
The embodiment of the utility model provides an in one or more technical scheme, following technological effect or advantage have at least: the application provides a pair of battery compartment structure and unmanned aerial vehicle have following advantage:
(1) the front end of the battery compartment adopts an elastic connecting mechanism, the elastic connecting mechanism is hidden in the battery compartment, a torsion spring is arranged on an installation column of the elastic connecting mechanism, and the torsion spring drives a rotating end to enable the shell cover to automatically bounce when the shell cover is opened;
(2) two push type door lock switches are adopted at the rear end of the battery bin, so that a user can open and close the shell cover and the shell body in a mode of pressing the designated positions of the battery bin, and double redundancy of the switches is realized;
(3) the shell cover is arranged on the shell body in a full wrapping mode, and can cover the window of the shell body in a whole mode, so that the rainproof effect is achieved.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings required to be used in the description of the embodiments are briefly introduced below, and it is obvious that the drawings in the following description are some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.
Fig. 1 is a schematic view illustrating an opened state of a battery compartment structure according to an embodiment of the present invention;
fig. 2 is a schematic diagram of a closed state of a battery compartment structure provided in an embodiment of the present invention;
fig. 3 is a schematic structural diagram of an open state of a battery compartment structure according to an embodiment of the present invention;
fig. 4 is a schematic structural diagram of an elastic connection mechanism in a battery compartment structure according to an embodiment of the present invention;
FIG. 5 is an enlarged schematic view of the structure at A in FIG. 4;
fig. 6 is a schematic structural diagram of a locking seat in a battery compartment structure according to an embodiment of the present invention.
Detailed Description
The present invention will be described in detail below with reference to specific embodiments and examples, and the advantages and various effects of the present invention will be more clearly apparent from the description. It will be understood by those skilled in the art that the present embodiments and examples are illustrative of the present invention, and are not to be construed as limiting the invention.
Throughout the specification, unless otherwise specifically noted, terms used herein should be understood as having meanings as commonly used in the art. Accordingly, unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. If there is a conflict, the present specification will control.
Unless otherwise specifically stated, various raw materials, reagents, instruments, equipment and the like used in the present invention are commercially available or can be prepared by an existing method.
As shown in fig. 1-6, in the embodiment of the present application, the utility model provides a battery compartment structure, include:
a case 10 for placing a battery;
a case cover 20 for sealing the case 10; the shell cover 20 is fittingly mounted on the shell 10;
a locking member 30 for cooperating with the locking seat 40 to lock the housing 10 with the housing cover 20; the locking piece 30 is arranged at the first end of the shell cover 20;
a locking seat 40 for locking the locker 30; the locking seat 40 is disposed at a first end of the housing 10 and opposite to the locking member 30;
an elastic coupling mechanism 50 for coupling the housing 10 and the housing cover 20; a first end of the elastic connection mechanism 50 is connected with a second end of the housing 10, and a second end is connected with a second end of the housing cover 20;
wherein, when the locking member 30 is disengaged from the locking seat 40, the elastic connection mechanism 50 drives the housing cover 20 to be separated from the housing 10.
In the embodiment of the present application, when the battery compartment structure is closed, the housing cover 20 is pressed to move toward the housing 10, and the locking member 30 is locked in the locking seat 40, and the housing cover 20 and the housing 10 are completely and hermetically mounted; when the battery compartment structure is opened, the housing cover 20 is pushed away from the housing 10 and the locking member 30 in the locking seat 40 is released, and the elastic connection mechanism 50 automatically springs the housing cover 20 away from the housing 10.
As shown in fig. 1 to 6, in the embodiment of the present application, the housing 10 includes a receiving cavity 11, the battery is placed in the receiving cavity 11, and when the housing cover 20 is fittingly mounted on the housing 10, the housing cover 20 completely covers the receiving cavity 11. The receiving cavity 11 is formed in the housing 10 and is recessed inward, and when the housing cover 20 is placed on the housing 10, the housing cover 20 completely covers the receiving cavity 11.
Referring to fig. 1-6, in the embodiment of the present application, the opening edge of the housing 10 is extended to protrude outward to form a flange 12, and when the housing cover 20 is fittingly mounted on the housing 10, the flange 12 abuts against the inner bottom wall of the housing cover 20. The flange 12 is disposed along the periphery of the opening of the housing 10 and is formed to protrude outward toward the housing cover 20, and when the housing cover 20 is covered on the housing 10, the flange 12 is closely attached to the inner bottom wall of the housing cover 20 without a gap, thereby enhancing the sealing performance between the housing 10 and the housing cover 20.
Referring to fig. 1 to 6, in the embodiment of the present application, the locking member 30 includes a locking hook 31, and the locking hook 31 is disposed on the inner bottom wall of the first end of the housing cover 20.
Referring to fig. 1 to 6, in the embodiment of the present application, the locking seat 40 includes a push type door lock switch 41, the outer surface of the first end of the housing 10 is recessed inward to form a mounting groove 13, the push type door lock switch 41 is disposed in the mounting groove 13, and when the housing cover 20 is fittingly mounted on the housing 10, the locking hook 31 of the locking member 30 is inserted into the mounting groove 13 and fastened to the push type door lock switch 41.
In the embodiment of the present application, when the housing cover 20 is covered on the housing 10, the latch hook 31 is correspondingly inserted into the pressing type door lock switch 41 and locked by the pressing type door lock switch; when it is necessary to open the case cover 20, the push type door lock switch 41 is pressed, and the push type door lock switch 41 releases the latch hook 31.
In the embodiment of the present application, the number of the locker 30 and the locking socket 40 is 2, as shown in fig. 1 to 6. Specifically, the number of the latch hooks 31 and the number of the push type door lock switches 41 are 2, and 2 corresponding locking structures are formed, and the 2 locking structures can form redundancy to ensure the locking between the case cover 20 and the case 10.
As shown in fig. 1 to 6, in the present embodiment, the elastic connection mechanism 50 includes: stiff end 51, torsional spring 52 and rotation end 53, wherein, stiff end 51 set up in on the first end lateral wall of casing 10, and outside extension forms erection column 54, correspond on the first end lateral wall of casing 10 rotation end 53 department is formed with dead slot 55, the first end of rotation end 53 is formed with lantern ring 56, lantern ring 56 cover is located on the erection column 54, the second end of rotation end 53 passes dead slot 55 and with the interior diapire of cap 20 is connected, torsional spring 52 cover is located on the erection column 54, and first end with stiff end 51 is connected and the second end with rotation end 53 is connected, rotation end 53 is in move in the dead slot 55 and realize casing 10 with opening and shutting of cap 20.
In the embodiment of the present application, when the housing 10 and the housing cover 20 are closed, the housing 10 is forced by an external force to move toward the housing cover 20, the rotating end 53 drives the torsion spring 52 to rotate around the mounting post 54, and the rotating end 53 rotates around the mounting post 54 in the empty slot 55 until the housing cover 20 is covered on the housing 10; when the housing 10 is opened, the pressing type door lock switch 41 is pressed, the pressing type door lock switch 41 releases the latch hook 31, the torsion spring 52 releases the elastic potential energy of the torsion spring to drive the rotating end 53 to rotate around the mounting column 54 in the hollow groove 55, and the rotating end 53 drives the housing cover 20 to bounce away from the housing 10.
As shown in fig. 1 to 6, in the embodiment of the present application, the fixing end 51 is provided with a first fixing hole 57, and the first end of the torsion spring 52 is inserted into the first fixing hole 57. The first end of the torsion spring 52 is fastened in the first fixing hole 57 so that the fixed end 51 is coupled with the torsion spring 52.
In the embodiment of the present application, as shown in fig. 1 to 6, a second fixing hole 58 is formed on the rotating end 53, and the second end of the torsion spring 52 is inserted into the second fixing hole 58. The second end of the torsion spring 52 is fastened in the second fixing hole 58 so that the connection between the rotating end 53 and the torsion spring 52 is accomplished.
The application provides a pair of battery compartment structure and unmanned aerial vehicle have following advantage:
(1) the front end of the battery compartment adopts an elastic connecting mechanism, the elastic connecting mechanism is hidden in the battery compartment, a torsion spring is arranged on an installation column of the elastic connecting mechanism, and the torsion spring drives a rotating end to enable the shell cover to automatically bounce when the shell cover is opened;
(2) two push type door lock switches are adopted at the rear end of the battery bin, so that a user can open and close the shell cover and the shell body in a mode of pressing the designated positions of the battery bin, and double redundancy of the switches is realized;
(3) the shell cover is arranged on the shell body in a full wrapping mode, and can cover the window of the shell body in a whole mode, so that the rainproof effect is achieved.
Finally, it should also be noted that the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. The terms "first" and "second" in this application are to be understood as terms.
While the preferred embodiments of the present invention have been described, additional variations and modifications in those embodiments may occur to those skilled in the art once they learn of the basic inventive concepts. It is therefore intended that the appended claims be interpreted as including the preferred embodiment and all such alterations and modifications as fall within the scope of the invention.
It will be apparent to those skilled in the art that various changes and modifications may be made without departing from the spirit and scope of the invention. Thus, if such modifications and variations of the present invention fall within the scope of the claims and their equivalents, the present invention is also intended to include such modifications and variations.
Claims (10)
1. A battery compartment structure, comprising:
a housing for housing a battery;
a case cover for sealing the case; the shell cover is mounted on the shell in a matching manner;
the locking piece is used for being matched with the locking seat so as to lock the shell and the shell cover; the locking piece is arranged at the first end of the shell cover;
the locking seat is used for locking the locking piece; the locking seat is arranged at the first end of the shell and is opposite to the locking piece;
the elastic connecting mechanism is used for connecting the shell and the shell cover; the first end of the elastic connecting mechanism is connected with the second end of the shell, and the second end of the elastic connecting mechanism is connected with the second end of the shell cover;
when the locking piece is separated from the locking seat, the shell cover and the shell are driven to be separated by the elastic connecting mechanism.
2. The battery compartment structure of claim 1, wherein the housing includes a receiving cavity in which the battery is placed, the housing cover completely covering the receiving cavity when the housing cover is fittingly mounted to the housing.
3. The battery compartment structure of claim 1, wherein the opening edge of the housing is protruded outward to form a flange, and the flange is tightly attached to the bottom wall of the housing cover when the housing cover is fittingly mounted on the housing.
4. The battery compartment structure of claim 1, wherein the retaining member comprises a latch hook disposed on a bottom wall within the first end of the housing cover.
5. The battery compartment structure of claim 1, wherein the locking seat comprises a push-type door lock switch, the outer surface of the first end of the housing is recessed to form a mounting groove, the push-type door lock switch is disposed in the mounting groove, and when the housing cover is mounted on the housing, the locking hook of the locking member is inserted into the mounting groove and fastened to the push-type door lock switch.
6. The battery compartment structure of claim 1 or 5, wherein the number of the locking members and the locking seats is 2.
7. The battery compartment structure of claim 1, wherein the resilient connection mechanism comprises: stiff end, torsional spring and rotation end, wherein, the stiff end set up in on the first end lateral wall of casing, and outside extension forms the erection column, correspond on the first end lateral wall of casing rotation end department is formed with the dead slot, the first end of rotation end is formed with the lantern ring, lantern ring cover is located on the erection column, the second end of rotation end passes the dead slot and with the interior diapire of cap is connected, the torsional spring cover is located on the erection column, and first end with the stiff end is connected and the second end with the rotation end is connected, the rotation end is in move and realize in the dead slot the casing with opening and shutting of cap.
8. The battery compartment structure of claim 7, wherein the fixing end is provided with a first fixing hole, and the first end of the torsion spring is inserted into the first fixing hole.
9. The battery compartment structure of claim 7, wherein the rotating end is provided with a second fixing hole, and the second end of the torsion spring is inserted into the second fixing hole.
10. A drone, characterized in that it comprises a battery compartment structure according to any one of claims 1 to 9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022738529.7U CN213936418U (en) | 2020-11-24 | 2020-11-24 | Battery compartment structure and unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022738529.7U CN213936418U (en) | 2020-11-24 | 2020-11-24 | Battery compartment structure and unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213936418U true CN213936418U (en) | 2021-08-10 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022738529.7U Expired - Fee Related CN213936418U (en) | 2020-11-24 | 2020-11-24 | Battery compartment structure and unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213936418U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113772435A (en) * | 2021-08-26 | 2021-12-10 | 深圳市德兰明海科技有限公司 | Flip subassembly and energy storage product |
| 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 |
-
2020
- 2020-11-24 CN CN202022738529.7U patent/CN213936418U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113772435A (en) * | 2021-08-26 | 2021-12-10 | 深圳市德兰明海科技有限公司 | Flip subassembly and energy storage product |
| 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 |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210810 Termination date: 20211124 |
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| CF01 | Termination of patent right due to non-payment of annual fee |