CN217260675U - Quick detach mechanism, battery and unmanned aerial vehicle - Google Patents
Quick detach mechanism, battery and unmanned aerial vehicle Download PDFInfo
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- CN217260675U CN217260675U CN202220521231.7U CN202220521231U CN217260675U CN 217260675 U CN217260675 U CN 217260675U CN 202220521231 U CN202220521231 U CN 202220521231U CN 217260675 U CN217260675 U CN 217260675U
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
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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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
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Abstract
The embodiment of the application relates to unmanned air vehicle technical field, especially relates to a quick detach mechanism, battery and unmanned aerial vehicle, and wherein, quick detach mechanism includes: casing, latch mechanism, handle and driving piece. The housing has a first surface. Clamping mechanism is including installing in the joint spare of casing, and it has locking position and unblock position, and relative casing, joint spare is more stretched out in the unblock position at the locking position. The handle is rotatably arranged on the shell and can rotate between a first set position and a second set position, the handle is borne on the first surface at the first set position, and a preset included angle is formed between the handle and the first surface at the second set position. The driving piece is installed in the handle for move to second settlement position at the handle from first settlement position and support and push away joint spare, so that joint spare moves to the unblock position from locking position. Through above-mentioned structure, only need adjust the position of joint spare through the handle during use to unblock or locking quick detach mechanism has improved the availability factor.
Description
Technical Field
The embodiment of the application relates to the technical field of unmanned aerial vehicles, especially relates to a quick detach mechanism, battery and unmanned aerial vehicle.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. The 'unmanned aerial vehicle plus' industry is really just needed by the unmanned aerial vehicle; the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief and the like, the application of the unmanned aerial vehicle is greatly expanded, and the developed countries also actively expand the industrial application and develop the unmanned aerial vehicle technology.
Present unmanned aerial vehicle uses the modularized design, and the dismouting all needs to be changed at the in-process that uses to many structures to improve unmanned aerial vehicle's availability factor, for example, change battery, image input equipment, plant protection equipment, remote sensing equipment etc. on the unmanned aerial vehicle. Use the battery as an example, present unmanned aerial vehicle no longer only leans on improving battery energy density and battery capacity to promote the time of endurance, but improves unmanned aerial vehicle time of endurance through changing reserve battery.
In the process of implementing the embodiment of the present application, the inventor finds that: in unmanned aerial vehicle's use, when changing the battery at present, need one hand to press the unlock button on the battery, the battery is pulled out to the other hand, and the change step of battery is complicated, and is inefficient.
SUMMERY OF THE UTILITY MODEL
The embodiment of the application aims at providing a quick detach mechanism, battery and unmanned aerial vehicle to improve the current situation that the change step of present unmanned aerial vehicle battery is complicated, inefficiency.
In order to solve the above technical problem, an embodiment of the present application provides a technical solution that a quick release mechanism is provided, including: casing, latch mechanism, handle and driving piece. The housing has a first surface. The clamping mechanism comprises a clamping piece, the clamping piece is installed on the shell, the clamping piece is provided with a locking position and an unlocking position, and is relative to the shell, the clamping piece is arranged on the locking position, and the unlocking position extends out of the clamping piece. The handle is rotatably arranged on the shell and can rotate between a first set position and a second set position, the handle is borne on the first surface at the first set position, and a preset included angle is formed between the handle and the first surface at the second set position. The driving piece is installed on the handle and used for pushing the clamping piece to the second set position after the handle moves from the first set position, so that the clamping piece moves from the locking position to the unlocking position.
Optionally, the clamping member has a supporting portion, and the driving member includes a supporting portion. The abutting part is used for abutting against the abutting part when the lifting handle moves from the first set position to the second set position, so that the clamping piece moves from the locking position to the unlocking position along the first direction. The first direction extends along a straight line, and the first direction is not perpendicular to the first surface.
Optionally, the abutting portion has a first end and a second end opposite to each other in a second direction, the first end is located downstream of the second end in the second direction, and in the unlocking position, a distance between the abutting portion and the abutting portion in the first direction is gradually reduced from the first end to the second end. The second direction is determined by the handle rotating from the first set position to the second set position.
Optionally, the clamping mechanism further comprises a reset member. The one end that resets is relative the casing is fixed, the other end with the joint spare is connected, it is used for the drive to reset the joint spare certainly the unblock position moves extremely locking position.
Optionally, the clamping mechanism further comprises a base. The base accept in the casing, the one end of piece that resets install in the base, the other end with joint piece butt.
Optionally, the reset member is a spring, and the spring extends along a first direction and is sleeved on the clamping member.
Optionally, the quick release mechanism includes two clamping mechanisms, and the two clamping mechanisms are arranged along the first direction in a mirror image manner. The handle has two end portions oppositely arranged along the first direction, and each end portion is rotatably mounted on the shell. The quick-release mechanism comprises two driving pieces, each driving piece is correspondingly installed at one end part, and each driving piece is used for driving one clamping mechanism.
Optionally, the joint spare is equipped with spacing portion, spacing portion with base sliding connection, spacing portion is used for the restriction the joint spare is in relative in the first direction the displacement of base.
Optionally, the base still is equipped with the guide way, the guide way is followed the first direction sets up, joint spare can be in the guide way is relative the base slides, the guide way is used for preventing the slip of joint spare is skew the first direction.
In order to solve the above technical problem, another technical solution provided in an embodiment of the present application is to provide a battery, where the battery includes the above quick release mechanism, and an electric core, and the electric core is accommodated in the casing.
In order to solve the technical problem, another technical scheme provided by the embodiment of the present application is to provide an unmanned aerial vehicle, which includes the above quick release mechanism, the above battery and an unmanned aerial vehicle body.
The beneficial effects of the embodiment of the application are that: in contrast to the prior art, an embodiment of the present application provides a quick release mechanism, which includes: casing, latch mechanism, handle and driving piece. The housing has a first surface. The clamping mechanism comprises a clamping piece, the clamping piece is installed on the shell, the clamping piece is provided with a locking position and an unlocking position, and is relative to the shell, the clamping piece is arranged on the locking position, and the unlocking position extends out of the clamping piece. The handle is rotatably arranged on the shell and can rotate between a first set position and a second set position, the handle is borne on the first surface at the first set position, and a preset included angle is formed between the handle and the first surface at the second set position. The driving piece is installed on the handle and used for pushing the clamping piece to the second set position after the handle moves from the first set position, so that the clamping piece moves from the locking position to the unlocking position. Through the structure, when the quick release mechanism is used, the position of the clamping piece can be adjusted only through the lifting handle, so that the quick release mechanism is unlocked or locked, and the use efficiency is improved.
Drawings
To more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the following will briefly describe the embodiments. Throughout the drawings, like elements or portions are generally identified by like reference numerals. In the drawings, elements or portions are not necessarily drawn to scale.
Fig. 1 is a schematic view of a drone provided in an embodiment of the present application;
fig. 2 is a perspective view of a quick release mechanism provided in an embodiment of the present application;
FIG. 3 is an exploded view of a quick release mechanism provided in accordance with an embodiment of the present application;
FIG. 4 is a partial schematic view of a quick release mechanism according to an embodiment of the present application;
FIG. 5 is an enlarged view of section A of FIG. 3 according to one embodiment of the present application;
FIG. 6 is an enlarged view of portion B of FIG. 3 according to one embodiment of the present application;
fig. 7 is an enlarged view of a portion C of fig. 3 according to an embodiment of the present disclosure.
Detailed Description
In order to facilitate an understanding of the present application, the present application is described in more detail below with reference to the accompanying drawings and specific embodiments. It will be understood that when an element is referred to as being "secured to" another element, it can be directly on the other element or intervening elements may also be present. When an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may be present. The terms "vertical," "horizontal," "left," "right," "inner," "outer," and the like as used herein are for descriptive purposes only.
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 application belongs. The terminology used in the description of the present application is for the purpose of describing particular embodiments only and is not intended to be limiting of the application. As used herein, the term "and/or" includes any and all combinations of one or more of the associated listed items.
In addition, the technical features mentioned in the different embodiments of the present application described below may be combined with each other as long as they do not conflict with each other.
Please refer to fig. 1, which shows a schematic diagram of an unmanned aerial vehicle 1 according to an embodiment of the present application. In order to better explain the specific implementation of the embodiment of the present application, the battery 1000 is taken as an example to be explained below, and the drone 1 includes the battery 1000 and a drone body 2000. Battery 1000 pegs graft in unmanned aerial vehicle fuselage 2000 to be connected with 2000 electricity of unmanned aerial vehicle fuselage, battery 1000 is used for 2000 power supplies of unmanned aerial vehicle fuselage, thereby makes unmanned aerial vehicle 1 can navigate by water, plant protection, shoot, tasks such as survey and drawing. Battery 1000 and unmanned aerial vehicle fuselage 2000 all are equipped with latch device that can mutually support to make battery 1000 detachable install in unmanned aerial vehicle fuselage 2000. The battery 1000 includes a quick release mechanism 100 and a battery core, and the battery core is accommodated in the quick release mechanism 100.
Referring to fig. 2 to fig. 4, a perspective view of the quick release mechanism 100 provided in an embodiment of the present application, an exploded view of the quick release mechanism 100 provided in an embodiment of the present application, and a partial schematic view of the quick release mechanism 100 provided in an embodiment of the present application are respectively shown. The quick release mechanism 100 includes: housing 10, latch mechanism 20, handle 30 and drive member 40. The housing 10 has a first surface 11. Clamping mechanism 20 includes joint spare 21, and joint spare 21 is installed in casing 10, and joint spare 21 has locking position and unblock position, and relative casing 10, joint spare 21 is in the locking position relatively stretch out the setting in unblock position. The handle 30 is rotatably mounted on the housing 10 and can rotate between a first setting position and a second setting position, in the first setting position, the handle 30 is supported on the first surface 11, and in the second setting position, the handle 30 has a predetermined included angle θ relative to the first surface 11. The driving member 40 is mounted on the handle 30 and configured to push the engaging member 21 when the handle 30 moves from the first setting position to the second setting position, so that the engaging member 21 moves from the locking position to the unlocking position. Through the structure, the position of the clamping piece 21 can be adjusted only through the handle 30 when the quick release mechanism 100 is disassembled and assembled, so that the quick release mechanism 100 is unlocked or locked, and the installation efficiency of the quick release mechanism 100 is improved. Optionally, the housing 10 in the embodiment of the present application has a rectangular parallelepiped shape, which is convenient for accommodating and placing the battery, while in other embodiments, the housing 10 may also be a casing with other shapes, such as a cube, a column, a cubic platform, a circular platform, or other irregular shapes. The preset included angle θ in the embodiment of the present application is 90 °, thereby being convenient for taking out or inserting the unmanned aerial vehicle body 2000, and in other embodiments, the preset included angle θ may be any angle from 0 ° to 180 °, for example: 70 ° to 110 ° or 45 ° to 135 °.
It should be noted that the quick release mechanism 100 is not limited to be used in the battery 1000 in practical applications, and may be any structure that needs to be quickly removed and replaced, such as a cover plate position of a body cover.
Further, please refer to fig. 5 and fig. 6, which respectively illustrate an enlarged view of a portion a of fig. 3 provided in one embodiment of the present application and an enlarged view of a portion B of fig. 3 provided in one embodiment of the present application, in combination with other drawings. The clip 21 has an abutting portion 211, and the driving member 40 includes an abutting portion 41. The abutting portion 41 is used for abutting against the abutting portion 211 when the handle 30 moves from the first setting position to the second setting position, so that the clip 21 moves from the locking position to the unlocking position along the first direction F1. The first direction F1 extends along a straight line, and the first direction F1 is not perpendicular to the first surface 11. By rotating the handle 30, the driving member 40 is driven to rotate, and the abutting portion 41 abuts against the abutting portion 211. It will be appreciated that first direction F1 is parallel to first surface 11 in the present embodiment, so that the travel of clip 21 within housing 10 is minimized when clip 21 extends the same length relative to housing 10. In some embodiments, the angle between the first direction F1 in which the clip 21 extends and the first surface 11 is an obtuse angle, so as to further prevent the quick release mechanism 100 from coming off the drone body 2000. Specifically, joint spare 21 is the pothook form setting with unmanned aerial vehicle fuselage 2000 complex part to be convenient for joint spare 21 joint in unmanned aerial vehicle fuselage 2000.
It should be noted that, in the above embodiments, mention is made of: relative to the housing 10, the clip 21 extends out of the unlocking position at the locking position. In the embodiment of the present application, the clip member 21 extends out from the locking position to the unlocking position relative to the outer surface of the housing 10; in other embodiments, the clamping member 21 may be recessed, and when the clamping member 21 extends to the unlocking position, the clamping member 21 is flush with the outer surface of the housing 10, so that the quick release mechanism 100 may be pulled out relative to the unmanned aerial vehicle body 2000.
Further, please refer to fig. 6 in combination with other figures. The abutting portion 41 has a first end 411 and a second end 412 opposite to each other along the second direction F2, the first end 411 is located downstream of the second end 412 along the second direction F2, and in the unlocking position, a distance between the abutting portion 211 and the abutting portion 41 along the first direction F1 gradually decreases from the first end 411 to the second end 412. The second direction F2 is a direction defined by the handle 30 rotating from the first setting position to the second setting position. That is, the outer contour of the abutment 41 in the present embodiment is curved, but in some embodiments it may also be a straight bevel, or an arc with a gradually increasing slope. With such a design, the contact position between the abutting portion 211 and the abutting portion 41 moves from the first end 411 to the second end 412, and the distance between the abutting portion 211 and the abutting portion 41 along the first direction F1 gradually decreases, so that the clip 21 slides from the locking position to the unlocking position. It is worth mentioning that the axis of the second direction F2 in the embodiment of the present application is parallel to the first direction F1.
For the above-mentioned latch mechanism 20, please refer to fig. 3, fig. 4 and fig. 7, wherein fig. 7 shows an enlarged view of a portion C of fig. 3 provided in an embodiment of the present application, in combination with other drawings. Latch mechanism 20 further includes a reset member 22. Reset piece 22's one end is fixed relative to casing 10, and the other end is connected with joint 21, and reset piece 22 is used for driving joint 21 and moves to the locking position from the unlocking position. The restoring member 22 in the embodiment of the present application is a compression spring, while the restoring member 22 in other embodiments may be a tension spring or a restoring device composed of a spring and other components. The spring extends along the first direction F1 and is sleeved on the clip 21. The clamping piece 21 is provided with a guide column 213, and the spring is arranged around the guide column 213 to prevent the spring from being separated. In some embodiments, the guiding column 213 may be configured as a hydraulic rod in some embodiments, and when the guiding column 213 is configured as a hydraulic rod, two ends of the guiding column 213 abut against the clamping member 21 and the base 23, respectively, so as to increase the pushing force of the spring.
Referring to fig. 7, an embodiment of the present application is provided, which is shown in combination with other figures. The latch mechanism 20 further includes a base 23. The base 23 is accommodated in the housing 10, and one end of the restoring member 22 is attached to the base 23 and the other end abuts against the engaging member 21. The base 23 is provided with a first avoiding hole 231, a second avoiding hole 232 and a guide groove 233. The guide post 213 penetrates the first avoiding hole 231, so that the guide post 213 is prevented from abutting against the base 23 to prevent the spring from being compressed, and further blocking the sliding of the clamping member 21. Meanwhile, the clamping member 21 is further provided with a limiting portion 212, and the limiting portion 212 is matched with the second avoiding hole 232 to prevent the clamping member 21 from being separated from the base 23 when the spring pushes out the clamping member 21. The guide groove 233 is provided along the first direction F1, the clip member 21 can slide in the guide groove 233 relative to the base 23, and the guide groove 233 serves to prevent the sliding of the clip member 21 from deviating from the first direction F1.
In the embodiments of the present application, please refer to fig. 4 in combination with other figures. The quick release mechanism 100 includes two latch mechanisms 20, and the two latch mechanisms 20 are arranged in a mirror image manner along a first direction F1. The handle 30 has two opposite ends 31 disposed opposite to each other along the first direction F1, and each end 31 is rotatably mounted to the housing 10. The quick release mechanism 100 includes two driving members 40, each driving member 40 is correspondingly installed at one end portion 31, and each driving member 40 is used for driving a clamping mechanism 20. Thereby reinforcing quick detach mechanism 100's joint performance, promoting the stability of quick detach mechanism 100 and unmanned aerial vehicle fuselage 2000's combination. It will be appreciated that the handle 30 may also be provided with gripping cleats and/or gripping grooves.
The quick release mechanism 100 provided in the embodiment of the present application includes: housing 10, latch mechanism 20, handle 30 and drive member 40. The housing 10 has a first surface 11. Clamping mechanism 20 includes joint spare 21, and joint spare 21 is installed in casing 10, and joint spare 21 has locking position and unblock position, and relative casing 10, joint spare 21 is in the locking position relatively stretch out the setting in unblock position. The handle 30 is rotatably mounted on the housing 10 and can rotate between a first setting position and a second setting position, in the first setting position, the handle 30 is supported on the first surface 11, and in the second setting position, the handle 30 has a predetermined included angle θ relative to the first surface 11. The driving element 40 is mounted on the handle 30, and is configured to push the clip element 21 against the handle 30 from the first setting position to the second setting position, so that the clip element 21 moves from the locking position to the unlocking position. Through the structure, the position of the clamping piece 21 can be adjusted only through the handle 30 when the quick release mechanism 100 is disassembled and assembled, so that the quick release mechanism 100 is unlocked or locked, and the installation efficiency of the quick release mechanism 100 is improved.
Based on the same inventive concept, the present application further provides a battery 1000, where the battery 1000 includes a quick release mechanism 100 and a battery core. The quick release mechanism 100 has the same structure as the quick release mechanism 100 described in the above embodiments, and therefore, the description thereof is omitted. This battery 1000 can improve the current situation that the change step of present unmanned aerial vehicle battery is complicated, inefficiency.
Based on the same inventive concept, the application also provides an unmanned aerial vehicle 1, and the unmanned aerial vehicle 1 comprises a quick release mechanism 100, a battery 1000 with the quick release mechanism 100 and a battery core, and an unmanned aerial vehicle body 2000. The battery 1000 and the quick release mechanism 100 have the same structure as the battery 1000 and the quick release mechanism 100 described in the above embodiments, and are not described herein again. This unmanned aerial vehicle 1 can improve the current situation that the change step of present unmanned aerial vehicle battery is complicated, inefficiency.
The above embodiments are merely examples, and not intended to limit the scope of the present application, and all modifications, equivalents, and flow charts using the contents of the specification and drawings of the present application, or those directly or indirectly applied to other related arts, are included in the scope of the present application. Those of ordinary skill in the art will understand that: the technical solutions described in the foregoing embodiments may still be modified, or some technical features may be equivalently replaced; and these modifications or substitutions do not depart from the scope of the technical solutions of the embodiments of the present application.
Claims (11)
1. A quick release mechanism, characterized in that, quick release mechanism includes:
a housing having a first surface;
the clamping mechanism comprises a clamping piece, the clamping piece is arranged on the shell and provided with a locking position and an unlocking position, and the clamping piece is arranged in a manner of extending out of the locking position and the unlocking position relative to the shell;
the lifting handle is rotatably arranged on the shell and can rotate between a first set position and a second set position, the lifting handle is borne on the first surface at the first set position, and a preset included angle is formed between the lifting handle and the first surface at the second set position;
the driving piece is installed on the lifting handle and used for enabling the lifting handle to move from the first set position to the second set position to push against the clamping piece, so that the clamping piece can move from the locking position to the unlocking position.
2. The quick release mechanism of claim 1 wherein the snap-in member has an abutment portion and the driving member includes an abutment portion;
the abutting part is used for abutting against the abutting part when the handle moves from the first set position to the second set position so as to enable the clamping piece to move from the locking position to the unlocking position along the first direction;
the first direction extends along a straight line, and the first direction is not perpendicular to the first surface.
3. The quick release mechanism according to claim 2, wherein the abutting portion has a first end and a second end opposite to each other in a second direction, the first end is located downstream of the second end in the second direction, and in the unlocking position, a distance between the abutting portion and the abutting portion in the first direction is gradually reduced from the first end to the second end;
the second direction is determined by the handle rotating from the first set position to the second set position.
4. The quick release mechanism of claim 2 wherein the clamping mechanism further comprises a reset member;
the one end that resets is relative the casing is fixed, the other end with the joint spare is connected, it is used for the drive to reset the joint spare certainly the unblock position moves extremely locking position.
5. The quick release mechanism of claim 4 wherein the clamping mechanism further comprises a base;
the base accept in the casing, the one end of piece that resets install in the base, the other end with joint piece butt.
6. The quick release mechanism of claim 4 wherein the reset member is a spring, the spring extends along the first direction and is sleeved on the snap member.
7. The quick release mechanism of any one of claims 2 to 6, comprising two snap mechanisms arranged in a mirror image along the first direction;
the handle is provided with two end parts which are oppositely arranged along the first direction, and each end part is rotatably arranged on the shell;
the quick-release mechanism comprises two driving pieces, each driving piece is correspondingly installed at one end part, and each driving piece is used for driving one clamping mechanism.
8. The quick release mechanism of claim 5,
the joint spare is equipped with spacing portion, spacing portion with base sliding connection, spacing portion is used for the restriction the joint spare is in relative in the first direction the displacement of base.
9. The quick release mechanism of claim 5,
the base still is equipped with the guide way, the guide way is followed the first direction sets up, joint spare can be relative in the guide way the base slides, the guide way is used for preventing the skew of sliding of joint spare the first direction.
10. A battery, comprising: the quick release mechanism of any one of claims 1-9, and a battery cell housed within the housing.
11. An unmanned aerial vehicle, comprising:
the quick release mechanism of any one of claims 1-9; and/or the presence of a gas in the atmosphere,
the battery of claim 10, and a drone fuselage.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220521231.7U CN217260675U (en) | 2022-03-10 | 2022-03-10 | Quick detach mechanism, battery and unmanned aerial vehicle |
| PCT/CN2023/077818 WO2023169217A1 (en) | 2022-03-10 | 2023-02-23 | Quick release mechanism, battery and unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220521231.7U CN217260675U (en) | 2022-03-10 | 2022-03-10 | Quick detach mechanism, battery and unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217260675U true CN217260675U (en) | 2022-08-23 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220521231.7U Active CN217260675U (en) | 2022-03-10 | 2022-03-10 | Quick detach mechanism, battery and unmanned aerial vehicle |
Country Status (2)
| Country | Link |
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| CN (1) | CN217260675U (en) |
| WO (1) | WO2023169217A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2023169217A1 (en) * | 2022-03-10 | 2023-09-14 | 深圳市道通智能航空技术股份有限公司 | Quick release mechanism, battery and unmanned aerial vehicle |
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| US10431780B2 (en) * | 2016-02-04 | 2019-10-01 | Cps Technology Holdings Llc | Lead-acid battery cover with handle retention |
| CN209045620U (en) * | 2018-05-23 | 2019-06-28 | 莱克电气股份有限公司 | Battery pack |
| CN208986071U (en) * | 2018-12-05 | 2019-06-14 | 成都纵横大鹏无人机科技有限公司 | A kind of Quick Release shell and battery |
| CN213716969U (en) * | 2020-12-04 | 2021-07-16 | 天津小鲨鱼智能科技有限公司 | Locking mechanism, battery pack and surfboard |
| CN214589114U (en) * | 2021-04-14 | 2021-11-02 | 厦门大恒科技有限公司 | Locking handle mechanism of rack power |
| CN217260675U (en) * | 2022-03-10 | 2022-08-23 | 深圳市道通智能航空技术股份有限公司 | Quick detach mechanism, battery and unmanned aerial vehicle |
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2022
- 2022-03-10 CN CN202220521231.7U patent/CN217260675U/en active Active
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2023
- 2023-02-23 WO PCT/CN2023/077818 patent/WO2023169217A1/en unknown
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2023169217A1 (en) * | 2022-03-10 | 2023-09-14 | 深圳市道通智能航空技术股份有限公司 | Quick release mechanism, battery and unmanned aerial vehicle |
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| Publication number | Publication date |
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| WO2023169217A1 (en) | 2023-09-14 |
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