CN216805850U - Quick detach structure and unmanned aerial vehicle for unmanned aerial vehicle mounting - Google Patents
Quick detach structure and unmanned aerial vehicle for unmanned aerial vehicle mounting Download PDFInfo
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- CN216805850U CN216805850U CN202123088085.8U CN202123088085U CN216805850U CN 216805850 U CN216805850 U CN 216805850U CN 202123088085 U CN202123088085 U CN 202123088085U CN 216805850 U CN216805850 U CN 216805850U
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- 238000004891 communication Methods 0.000 claims description 23
- 239000000523 sample Substances 0.000 claims description 13
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims description 5
- 238000009434 installation Methods 0.000 abstract description 3
- 230000007547 defect Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 239000000575 pesticide Substances 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
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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
- B64D47/00—Equipment not otherwise provided for
-
- 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
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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Abstract
The utility model belongs to the technical field of unmanned aerial vehicles, and relates to a quick release structure for mounting of an unmanned aerial vehicle, which comprises a quick release module and a quick release base which are matched with each other, wherein a slide rail (1) is arranged on the left outer side surface and the right outer side surface of the quick release module respectively, a lock tongue (2) capable of stretching up and down is arranged at the top of the quick release module, a slide groove (7) is arranged on the left inner side surface and the right inner side surface of the quick release base respectively, a groove (6) is arranged on the inner side surface of the top of the quick release base, the slide rail (1) can be inserted into the slide groove (7) and can slide back and forth in the slide groove (7), and the lock tongue (2) can be buckled in the groove (6) to connect the quick release module and the quick release base together. It can realize quick installation and the dismantlement of unmanned aerial vehicle hanging piece, and simple structure, convenient to use.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicles, and relates to an accessory for an unmanned aerial vehicle, in particular to a quick release structure for mounting of the unmanned aerial vehicle and the unmanned aerial vehicle.
Background
Along with the development of unmanned aerial vehicle technology, unmanned aerial vehicle's range of application is more and more wide. For example, nobody can mount a camera to realize photographing and video recording, various sensors to realize acquisition of various data, a pesticide spraying device to spray pesticides for farmlands and the like, and the like.
To achieve these functions, the drone must mount various mounts, such as cameras, sensors, etc., on the bottom of the drone. This requires that the bottom of the drone must have a structure that can accommodate the mounting of these mounts. Also, since these hangers are frequently disassembled and assembled, it is required that these structures be easily disassembled.
However, the existing structure for mounting the unmanned aerial vehicle generally has the following problems: 1. the disassembly and assembly are troublesome, and a plurality of bolts and the like need to be screwed to realize the assembly and disassembly of the hanging part, so that the use is very inconvenient; 2. the structure is complex, so that the weight is heavy, and the capability of the unmanned aerial vehicle is affected; 3. the existing mounting structure is not suitable for heavy loads.
In view of the above-mentioned technical defect of prior art, the urgent need develops a novel structure for unmanned aerial vehicle carries.
Disclosure of Invention
The utility model aims to overcome the defects in the prior art and provides a quick-release structure for mounting an unmanned aerial vehicle and the unmanned aerial vehicle, which can realize quick mounting and dismounting of a mounting piece of the unmanned aerial vehicle, and is simple in structure and convenient to use.
In order to achieve the above purpose, the utility model provides the following technical scheme:
the utility model provides an unmanned aerial vehicle carries uses rapid disassembly structure, its is including the rapid disassembly module and the quick detach base of mutually supporting, its characterized in that, be equipped with a slide rail, top respectively on the left and right lateral surface of rapid disassembly module and be equipped with the spring bolt that can stretch out and draw back from top to bottom, be equipped with the recess on a spout, the top medial surface respectively on the left medial surface and the right medial surface of quick detach base, the slide rail can insert in the spout and can slide around in the spout, the spring bolt can the buckle be in the recess in order to incite somebody to action quick detach module and quick detach pedestal link together.
Preferably, wherein, still be equipped with a button on the left and right lateral surface of quick detach module respectively, through pressing the button can control the flexible of spring bolt.
Preferably, the quick release module is provided with a lower bracket at the lower part.
Preferably, the quick release module is provided with four lower brackets at the lower part thereof.
Preferably, connecting columns are respectively arranged on the left outer side surface and the right outer side surface of the quick-release base.
Preferably, the quick-release base is provided with two connecting columns on the left outer side surface and the right outer side surface respectively.
Preferably, wherein, be equipped with first electrical interface on the back medial surface of quick detach module, be equipped with the second electrical interface on the back medial surface of quick detach base.
Preferably, the first electrical interface and the second electrical interface are used for realizing communication between an aircraft control system and a mount of the aircraft and supplying power for the mount.
Preferably, wherein the first electrical interface and the second electrical interface use a plurality of pin probes, a plurality of sets of backup of communication and power supply can be realized.
Preferably, the first electrical interface and the second electrical interface use 30pin probes, wherein 8pin probes are used for power supply, 4 sets of backup are provided, and both 12V power supply and 5V power supply are supported; the communication is divided into network communication and CAN communication, the network communication occupies 12pin probes, the CAN communication occupies 6pin probes, and three backup CAN be realized respectively.
Preferably, the slide rail is a T-shaped slide rail or an L-shaped slide rail.
Preferably, the slide rail is a limiting slide rail, and the tail end of the slide rail is provided with a first limiting mechanism.
Preferably, the sliding groove is a limiting sliding groove, and a second limiting mechanism is arranged at the tail end of the sliding groove.
In addition, the utility model also provides an unmanned aerial vehicle which is characterized by comprising a body, a support frame, a battery cabin, a navigation lamp, a motor, a propeller and/or a wing, a power system, a flight control system and the quick-release structure.
Preferably, the number of the propellers is two or more.
Preferably, wherein the wing is a fixed wing, the unmanned aerial vehicle further comprises an empennage propeller.
Preferably, the unmanned aerial vehicle further comprises a cabin, and at least two cabins and at least one central control panel are contained in the cabin.
Preferably, the unmanned aerial vehicle can be simultaneously mounted with one or more quick release structures.
Compared with the prior art, the rapid disassembly structure for mounting the unmanned aerial vehicle and the unmanned aerial vehicle have the following beneficial technical effects:
1. the mounting and dismounting of the hanging piece are simple, bolts do not need to be screwed, and the hanging piece can be mounted and dismounted quickly, so that the use of the hanging piece is very convenient.
2. Its simple structure, weight is little, and is little to unmanned aerial vehicle's influence.
3. The sliding type hanging rack adopts a sliding type structure, can bear larger load weight, and can be adapted to more hanging types.
Drawings
Fig. 1 is a perspective view of a quick release module of the quick release structure for mounting an unmanned aerial vehicle according to the present invention.
Fig. 2 is a front view of the quick release module of the quick release structure for mounting the unmanned aerial vehicle.
Fig. 3 is a perspective view of the quick release base of the quick release structure for mounting an unmanned aerial vehicle according to the present invention.
Fig. 4 is a front view of the quick release base of the quick release structure for mounting the unmanned aerial vehicle.
Fig. 5 is a perspective view of a box body of a quick release module of a quick release structure for mounting an unmanned aerial vehicle according to another embodiment of the utility model.
Fig. 6 is a perspective view of a base body of a quick release base of a quick release structure for mounting an unmanned aerial vehicle according to still another embodiment of the present invention.
Fig. 7 is a schematic view of the rapid disassembly structure for mounting the unmanned aerial vehicle of the utility model.
Detailed Description
The present invention is further described with reference to the following drawings and examples, which are not intended to limit the scope of the present invention.
In the present invention, various words indicating orientations, such as "upper", "lower", "left", "right", "top", "bottom", "front", "rear", etc., are used for convenience of description, and are not intended to limit the scope of the present invention.
The utility model relates to a quick-release structure for mounting an unmanned aerial vehicle, which comprises a quick-release module and a quick-release base which are matched with each other. Unmanned aerial vehicle carries and can realize various unmanned aerial vehicle and carry piece with quick detach structure, for example, quick installation and the dismantlement of camera, sensor, megaphone, detacher etc..
As shown in fig. 1 and 2, a slide rail 1 is respectively arranged on the left outer side surface and the right outer side surface of the quick release module, and a lock tongue 2 capable of extending up and down is arranged at the top of the quick release module. Under normal conditions, the lock tongue 2 extends upwards from the outer side face of the top of the quick release module, and can be retracted into the quick release module under the action of external force. There are many structures for performing such a function, for example, a telescopic spring is provided at a lower portion of the latch bolt 2 and a top cross-section of the latch bolt 2 is inclined. In this way, the bolt 2 can extend out from the top of the quick release module under the elastic force of the telescopic spring. When the quick release module is pulled outwards in the reverse direction, the inclined section can generate a downward force between the inclined section and the inner wall of the groove to overcome the elastic force, so that the lock tongue 2 can be contracted downwards to be disengaged from the groove.
Preferably, a button 3 is further respectively arranged on the left outer side surface and the right outer side surface of the quick release module. The inside of the button 3 is connected with the lower part of the bolt 2 in the quick-release module, so that the bolt 2 can be controlled to stretch and contract by pressing the button 3. That is, by pressing the button 3, the latch bolt 2 can be retracted into the quick release module.
More preferably, a first electrical interface 4 is arranged on the rear outer side surface of the quick release module. And power supply and communication of external mounting are realized through the first electrical interface 4.
Still preferably, the lower part of the quick release module is provided with a lower bracket 5. For example, the lower part of the quick release module is provided with four lower brackets 5. The lower bracket 5 is used for attaching a hanging member, such as a camera, a sensor, a megaphone, a detacher, etc.
As shown in fig. 3 and 4, a sliding groove 7 is respectively arranged on the left inner side surface and the right inner side surface of the quick-release base, and a groove 6 is arranged on the inner side surface of the top.
The slide rail 1 can be inserted into the slide groove 7 and can slide back and forth in the slide groove 7. The bolt 2 can be buckled in the groove 6 to connect the quick release module and the quick release base together.
Therefore, when the quick release module and the quick release base are required to be connected together, the slide rail 1 of the quick release module is aligned to the slide groove 7 of the quick release base, and the buttons 3 on two sides of the quick release module are pressed or not pressed and pushed inwards. After the lock tongue 2 is buckled in the groove 6, the lock tongue cannot be pushed, and cannot automatically exit in the reverse direction. At this point, the installation is complete.
Further, the slide rail 1 is a T-shaped slide rail or an L-shaped slide rail. When the quick release module needs to be detached, namely the quick release module needs to be detached from the quick release base, the buttons 3 on two sides of the quick release module are pressed simultaneously, the lock tongue 2 can return into the quick release module, the quick release module is pulled out towards the outer side, and then the quick release module can be detached. When only one button 3 is pressed, the bolt 2 cannot return into the quick-release module, so that the mounting falling caused by mistaken touch can be prevented.
Preferably, a second electrical interface 8 is arranged on the rear inner side surface of the quick-release base. When the quick release module and the quick release base are mounted together, the first electrical interface 4 and the second electrical interface 8 are opposite to each other, so that power supply and communication for external mounting are realized.
In the utility model, the first electrical interface 4 and the second electrical interface 8 are used for realizing communication between a flight control system of an aircraft and different mounts, and supplying power for the mounts.
Preferably, the first electrical interface 4 and the second electrical interface 8 use a plurality of pin probes, so that a plurality of sets of backup of communication and power supply can be realized.
Specifically, the first electrical interface 4 and the second electrical interface 8 have a 30pin probe contact, 8 pins are used for power supply, 4 groups of backup support 12V and 5V power supply, and the functions of mounting an overlarge load and increasing output current can be effectively solved while 4 groups of backup support; the communication is divided into network communication and CAN communication, 12PINPin is used for a network port, 6 PINPin is used for CAN, three backups are respectively performed, for different mounting, the required communication protocols are different, and the electrical interface of the utility model CAN realize mounting compatible with different protocol types.
In addition, connecting columns 9 are respectively arranged on the left outer side surface and the right outer side surface of the quick-release base. For example, two connecting columns 9 are respectively arranged on the left outer side surface and the right outer side surface of the quick-release base. The connecting column 9 is used for connecting to a hanging rack. The hanging and carrying frame is connected to the bottom of the unmanned aerial vehicle. Like this, can with the quick detach base is installed on unmanned aerial vehicle.
In this embodiment, the slide rail 1 is a common general slide rail. The chute 7 is a common chute.
In addition, fig. 5 is a perspective view of a box body of a quick release module of a quick release structure for mounting an unmanned aerial vehicle according to another embodiment of the utility model. For simplicity, fig. 5 does not show the latch, the button and the first electrical interface, but only shows the case of the quick release module.
As shown in fig. 5, in this embodiment, the sliding rail 1 is a limiting sliding rail, and a first limiting mechanism 1.1 is arranged at the end of the limiting sliding rail, that is, the end far away from the first electrical interface.
Fig. 6 is a perspective view showing a base body of a quick release base of a quick release structure for mounting an unmanned aerial vehicle according to still another embodiment of the present invention. Wherein the second electrical interface is not shown in fig. 6 for the sake of simplicity.
In this embodiment, as shown in fig. 6, the sliding groove 7 is a limiting sliding groove, and a second limiting mechanism 7.1 is arranged at the end of the sliding groove, i.e. the end far away from the second electrical interface.
Fig. 1 shows a common mounted quick release module, the slide rail of which can be inserted into a common base slide groove or into a limit slide groove with the second limit mechanism 7.1; while the sliding rail with all the first limiting means 1.1 can only be inserted into a common base runner. The aim at that sets up like this combines the flight state that has the unmanned aerial vehicle of carry, and the string position of its aircraft nose direction can not be overweight, therefore will have stop gear's base as the front end (be close to the aircraft nose promptly) string position, with ordinary base as the rear end string position to the quick detach module that will carry the gross weight of needs only carries at the rear end of aircraft (be close to the tail) string position, thereby guarantees unmanned aerial vehicle's safe flight.
Fig. 7 shows a schematic view of the rapid disassembly structure for mounting the unmanned aerial vehicle. As shown in fig. 7, the first quick release module a1 can be connected to a mounting bracket of the sensor D through a lower bracket of a lower portion thereof, thereby connecting the sensor D to the first quick release module a 1. The second quick release module a2 may be connected to a mounting bracket of the camera E by a lower bracket of a lower portion thereof, thereby connecting the camera E to the second quick release module a 2. Meanwhile, the first and second quick release bases B1 and B2 are connected to the first and second hangers C1 and C2 through connecting columns at both sides thereof. Wherein the first hanging carriage C1 and the second hanging carriage C2 are connected at the bottom of the unmanned aerial vehicle.
Then, the first quick release module a1 is inserted into the first quick release base B1, and the second quick release module a2 is inserted into the second quick release base B2. From this, just can install sensor D and camera E on unmanned aerial vehicle fast.
The quick release module can be carried on one or more than one unmanned aerial vehicle,
the quick-release structure for mounting the unmanned aerial vehicle is simple to mount and dismount, bolts do not need to be screwed, and the mounting part can be rapidly mounted and dismounted, so that the quick-release structure for mounting the unmanned aerial vehicle is very convenient to use. Simultaneously, its simple structure, weight is little, and is little to unmanned aerial vehicle's influence.
In the utility model, the rapid disassembly structure for mounting the unmanned aerial vehicle can be applied to various unmanned aerial vehicles. For example, in one type of drone, the drone includes a fuselage, a support frame, a battery compartment, a navigation light, a motor, a propeller and/or a wing, a power system, a flight control system, and a quick release structure of the present invention.
Wherein, when unmanned aerial vehicle includes the screw, preferably, the screw is two and more.
And, when the unmanned aerial vehicle includes a wing, preferably, the wing is a fixed wing, and the unmanned aerial vehicle further includes an empennage propeller.
Furthermore, the drone may also include a cockpit. Wherein, the cabin comprises at least two cabins and at least one central control panel.
The above examples of the present invention are merely examples for clearly illustrating the present invention and are not intended to limit the embodiments of the present invention. Other variations and modifications will be apparent to persons skilled in the art in light of the above description. Not all embodiments are exhaustive. All obvious changes and modifications which are obvious to the technical scheme of the utility model are covered by the protection scope of the utility model.
Claims (18)
1. The utility model provides an unmanned aerial vehicle carries uses rapid disassembly structure, its is including mutually supporting rapid disassembly module and rapid disassembly base, a serial communication port, be equipped with one slide rail (1), top respectively on the left and right lateral surface of rapid disassembly module and be equipped with spring bolt (2) that can stretch out and draw back from top to bottom, be equipped with on the left medial surface of rapid disassembly base and the right medial surface respectively one spout (7), the top medial surface on be equipped with recess (6), slide rail (1) can insert in spout (7) and can slide around in spout (7), spring bolt (2) can the buckle be in order to incite somebody to action in recess (6) rapid disassembly module and rapid disassembly base link together.
2. The rapid disassembly structure for unmanned aerial vehicle mounting according to claim 1, wherein a button (3) is further arranged on each of the left outer side surface and the right outer side surface of the rapid disassembly module, and the bolt (2) can be controlled to stretch by pressing the button (3).
3. The rapid disassembly structure for unmanned aerial vehicle mounting according to claim 1, wherein a lower bracket (5) is provided at a lower portion of the rapid disassembly module.
4. The rapid disassembly structure for unmanned aerial vehicle mounting according to claim 3, wherein the lower portion of the rapid disassembly module is provided with four lower brackets (5).
5. The rapid disassembly structure for unmanned aerial vehicle mounting according to claim 1, wherein connecting columns (9) are respectively arranged on the left outer side surface and the right outer side surface of the rapid disassembly base.
6. The rapid disassembly structure for unmanned aerial vehicle mounting according to claim 5, wherein two connecting columns (9) are respectively arranged on the left outer side surface and the right outer side surface of the rapid disassembly base.
7. The rapid disassembly structure for unmanned aerial vehicle mounting according to claim 1, wherein a first electrical interface (4) is arranged on a rear outer side surface of the rapid disassembly module, and a second electrical interface (8) is arranged on a rear inner side surface of the rapid disassembly base.
8. The rapid release structure for unmanned aerial vehicle mounting according to claim 7, wherein the first electrical interface (4) and the second electrical interface (8) are used for realizing communication between a flight control system of an aircraft and mounting and supplying power to mounting.
9. The rapid disassembly structure for unmanned aerial vehicle mounting according to claim 8, wherein the first electrical interface (4) and the second electrical interface (8) use a plurality of pin probes, and multiple sets of backup of communication and power supply can be realized.
10. The rapid disassembly structure for unmanned aerial vehicle mounting according to claim 9, wherein the first electrical interface (4) and the second electrical interface (8) use 30pin probes, wherein 8pin probes are used for power supply, 4 sets of backup probes are provided, and both support 12V power supply and 5V power supply; the communication is divided into network communication and CAN communication, the network communication occupies 12pin probes, the CAN communication occupies 6pin probes, and three backup CAN be realized respectively.
11. The rapid disassembly structure for unmanned aerial vehicle mounting according to claim 1, wherein the slide rail (1) is a T-shaped slide rail or an L-shaped slide rail.
12. The rapid disassembly structure for unmanned aerial vehicle mounting according to claim 1, wherein the slide rail (1) is a limiting slide rail, and a first limiting mechanism (1.1) is arranged at a tail end of the slide rail.
13. The rapid disassembly structure for unmanned aerial vehicle mounting according to claim 1, wherein the sliding groove (7) is a limiting sliding groove, and a second limiting mechanism (7.1) is disposed at a tail end of the sliding groove.
14. An unmanned aerial vehicle comprising a fuselage, a support frame, a battery compartment, a navigation light, a motor, a propeller and/or a wing, a power system, a flight control system, and the rapid release structure of any one of claims 1-13.
15. The drone of claim 14, wherein the propellers are two or more.
16. The drone of claim 14, wherein the wing is a fixed wing, the drone further comprising an empennage propeller.
17. The drone of any one of claims 14-16, further comprising a cockpit containing at least two bays and at least one center control panel.
18. An unmanned aerial vehicle according to any one of claims 14 to 16, wherein one or more rapid release structures according to any one of claims 1 to 13 can be mounted on the unmanned aerial vehicle at the same time.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123088085.8U CN216805850U (en) | 2021-12-09 | 2021-12-09 | Quick detach structure and unmanned aerial vehicle for unmanned aerial vehicle mounting |
| PCT/CN2022/130645 WO2023103686A1 (en) | 2021-12-09 | 2022-11-08 | Quick release structure for mounting on unmanned aerial vehicle , and unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123088085.8U CN216805850U (en) | 2021-12-09 | 2021-12-09 | Quick detach structure and unmanned aerial vehicle for unmanned aerial vehicle mounting |
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| Publication Number | Publication Date |
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| CN216805850U true CN216805850U (en) | 2022-06-24 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202123088085.8U Active CN216805850U (en) | 2021-12-09 | 2021-12-09 | Quick detach structure and unmanned aerial vehicle for unmanned aerial vehicle mounting |
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| Country | Link |
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| CN (1) | CN216805850U (en) |
| WO (1) | WO2023103686A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2023103686A1 (en) * | 2021-12-09 | 2023-06-15 | 亿航智能设备（广州）有限公司 | Quick release structure for mounting on unmanned aerial vehicle , and unmanned aerial vehicle |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205633085U (en) * | 2016-04-28 | 2016-10-12 | 深圳市龙云创新航空科技有限公司 | Instrument quick replacement mounting structure is exempted from to external module of unmanned aerial vehicle |
| EP3557112B1 (en) * | 2018-04-19 | 2020-09-02 | EBN Technology Corp. | Fast detachable placement seat structure for display |
| CN209008869U (en) * | 2018-08-10 | 2019-06-21 | 浙江科比特科技有限公司 | Unmanned plane gondola mounting structure and unmanned machine equipment |
| CN212099373U (en) * | 2020-05-20 | 2020-12-08 | 福建信息职业技术学院 | Unmanned aerial vehicle carries quick detach mechanism |
| CN113682486A (en) * | 2021-07-07 | 2021-11-23 | 浙江科比特创新科技有限公司 | Cloud platform rapid disassembly structure and unmanned aerial vehicle thereof |
| CN216805850U (en) * | 2021-12-09 | 2022-06-24 | 亿航智能设备（广州）有限公司 | Quick detach structure and unmanned aerial vehicle for unmanned aerial vehicle mounting |
-
2021
- 2021-12-09 CN CN202123088085.8U patent/CN216805850U/en active Active
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2022
- 2022-11-08 WO PCT/CN2022/130645 patent/WO2023103686A1/en unknown
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2023103686A1 (en) * | 2021-12-09 | 2023-06-15 | 亿航智能设备（广州）有限公司 | Quick release structure for mounting on unmanned aerial vehicle , and unmanned aerial vehicle |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2023103686A1 (en) | 2023-06-15 |
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