CN208165244U - A kind of Quick Release quick fixation structure device of unmanned plane wing and empennage - Google Patents
A kind of Quick Release quick fixation structure device of unmanned plane wing and empennage Download PDFInfo
- Publication number
- CN208165244U CN208165244U CN201820426148.5U CN201820426148U CN208165244U CN 208165244 U CN208165244 U CN 208165244U CN 201820426148 U CN201820426148 U CN 201820426148U CN 208165244 U CN208165244 U CN 208165244U
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- wing
- aluminum component
- fuselage
- quick release
- wing aluminum
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Abstract
The utility model discloses the Quick Release quick fixation structure devices of a kind of unmanned plane wing and empennage,Including the fuselage wing aluminum component being set on fuselage,The wing aluminum component for being arranged on wing and being assembled together with the fuselage wing aluminum component,Carbon pipe after carbon pipe and wing before wing,The fuselage wing aluminum component and wing aluminum component are assembled together to form wing aluminum component structure,There are two the preceding buttons and rear button for disassembling wing aluminum component structure for setting among the wing aluminum component structure upper,The wing aluminum component structure front is provided with the preceding carbon pore for inserting carbon pipe before wing,The preceding carbon pore runs through the fuselage wing aluminum component and wing aluminum component,The wing aluminum component structure rear portion is provided with the rear carbon pore for inserting carbon pipe after wing,The dismantling of the Quick Release quick fixation structure device of the unmanned plane wing and empennage is convenient,Without dismantling and installation the end of a thread,Without the turn of the screw,Dismantling only needs button press can be completed,It can accurate quick location and installation when installation,It saves artificial.
Description
Technical field
The utility model relates to the Quick Release of unmanned plane equipment technical field more particularly to a kind of unmanned plane wing and empennage is fast
Assembling structure device.
Background technique
Unmanned plane is made of wing, fuselage, tailplane, vertical tail etc..In order to facilitate transport often unmanned plane
Several parts, wing, fuselage, horizontal tail etc. are disassembled into, but due to having some electronic equipments such as steering engine, engine, institute on wing
Unavoidably to split simultaneously to these electronic circuits during dismounting, each line that dismantle when splitting in the past is connect
Head, while installing is also to need to dock each the end of a thread, trouble of getting off in this way, often plugging the end of a thread can have damage, and also
A series of a possibility that artificial wrong the end of a thread causes losses.When tradition dismounting unmanned plane, the turn of the screw may be also wanted, screw quantity is very
It is more, cause dismounting project amount it is big, human input is big, waste of resource, and unmanned plane folding solution after, cannot accurately be installed.
Therefore, it is convenient to have been devoted to research and develop a kind of dismantling by those skilled in the art, without dismantling and installation the end of a thread, nothing
Need the turn of the screw, dismantling only needs button press can be completed, when installation can accurate quick location and installation, save artificial unmanned plane machine
The Quick Release quick fixation structure device of the wing and empennage.
Utility model content
The technical problem to be solved by the present invention is to provide a kind of Quick Release quick fixation structure of unmanned plane wing and empennage dresses
It sets, it is convenient that the Quick Release quick fixation structure device of the unmanned plane wing and empennage is disassembled, without dismantling and installation the end of a thread, without twisting spiral shell
Silk, dismantling only need button press can be completed, when installation can accurate quick location and installation, save artificial.
In order to solve the above technical problems, the utility model provides the Quick Release quick fixation structure dress of a kind of unmanned plane wing and empennage
Set, including be set on fuselage fuselage wing aluminum component, be assembled together on setting wing and with the fuselage wing aluminum component
Carbon pipe after carbon pipe and wing before wing aluminum component, wing, the fuselage wing aluminum component and wing aluminum component are assembled together to form wing
Aluminum component structure, there are two the preceding buttons for disassembling wing aluminum component structure to press with after for wing aluminum component structure upper centre setting
Button, the wing aluminum component structure front are provided with the preceding carbon pore for inserting carbon pipe before wing, and the preceding carbon pore is through described
Fuselage wing aluminum component and wing aluminum component, the wing aluminum component structure rear portion are provided with the rear carbon pore for inserting carbon pipe after wing,
Carbon pore runs through the fuselage wing aluminum component and wing aluminum component after described, is provided in the wing aluminum component structure for that will assemble
The preceding fastener system component and the rear catch component of a system that the fuselage wing aluminum component and wing aluminum component completed are locked in together, institute
Fastener system component and the rear catch component of a system are respectively arranged at the front and rear portion of the wing aluminum component structure before stating.
Preferentially, Quick Release aviation plug hole location, the Quick Release aviation plug hole location are provided in the wing aluminum component structure
Through the fuselage wing aluminum component and wing aluminum component, it is provided in the Quick Release aviation plug hole location of the fuselage wing aluminum component fast
It tears aviation plug female open, is provided with Quick Release aviation plug male connector in the Quick Release aviation plug hole location of the wing aluminum component.
Preferably, Quick Release aviation plug hole location, the Quick Release aviation plug hole location are provided in the wing aluminum component structure
Through the fuselage wing aluminum component and wing aluminum component, it is provided in the Quick Release aviation plug hole location of the fuselage wing aluminum component fast
It tears aviation plug male connector open, Quick Release aviation plug female is set in the wing aluminum component Quick Release aviation plug hole location.
Preferably, the Quick Release aviation plug male connector and the Quick Release aviation plug female integrated power source line, steering engine line, oil
Door line is in one.
Preferably, the preceding fastener system component includes the preceding button, is set to the fuselage wing aluminum component front
Preceding lock, the preceding spring for being set to the preceding lock lower part, are set on the wing aluminum component and can be used for by the preceding lock
First fastened is raised, offers the first locking slot in first protrusion.
Preferably, the rear catch component of a system includes the rear button, is set to the fuselage wing aluminum component rear portion
Rear catch is set to the rear spring of the rear catch lower part, is set on the wing aluminum component and can be used for by the rear catch
Second fastened is raised, offers the second locking slot in second protrusion.
Preferably, the seam crossing of the fuselage wing aluminum component in the wing aluminum component structure and the wing aluminum component
Front and back end is provided with preceding umbrella rope hanging point and rear umbrella rope hanging point.
Preferably, the Quick Release quick fixation structure device of the unmanned plane wing and empennage further includes the fuselage being set on fuselage
Horizontal tail aluminum component, the horizontal tail aluminum component for being set on empennage and being assembled together with the fuselage horizontal tail aluminum component, horizontal tail carbon pipe, the machine
Body horizontal tail aluminum component and horizontal tail aluminum component are assembled together to form horizontal tail aluminum component structure, are provided in the horizontal tail aluminum component structure for inserting
The horizontal tail carbon pore of horizontal tail carbon pipe, the horizontal tail carbon pore run through the fuselage horizontal tail aluminum component and horizontal tail aluminum component.
After adopting the above structure, the Quick Release quick fixation structure device of unmanned plane wing and empennage, including being set on fuselage
Carbon pipe and wing before the wing aluminum component being assembled together on wing and with fuselage wing aluminum component, wing is arranged in fuselage wing aluminum component
Carbon pipe afterwards, fuselage wing aluminum component and wing aluminum component are assembled together to form wing aluminum component structure, among wing aluminum component structure upper
It is arranged there are two the preceding button and rear button for disassembling wing aluminum component structure, wing aluminum component structure front is provided with for plugging in machine
The preceding carbon pore of carbon pipe before the wing, preceding carbon pore run through fuselage wing aluminum component and wing aluminum component, and wing aluminum component structure rear portion is provided with
For inserting the rear carbon pipe of carbon pipe after wing, rear carbon pore runs through fuselage wing aluminum component and wing aluminum component, sets in wing aluminum component structure
It is equipped with preceding fastener system component and rear catch that fuselage wing aluminum component and wing aluminum component for completing assembly are locked in together
The component of a system, the preceding fastener system component and the rear catch component of a system be respectively arranged at wing aluminum component structure front and after
Portion presses the preceding button and rear button two in the wing aluminum component structure on port wing when unmanned plane wing to be disassembled and empennage
Then a button extracts unmanned plane port wing out, press the preceding button in the wing aluminum component structure on starboard wing and two, rear button
Then button extracts unmanned plane starboard wing out, presses the button in the horizontal tail aluminum component structure in left horizontal tail, then extract unmanned plane out
Left horizontal tail presses the button in the horizontal tail aluminum component structure in right horizontal tail, then extracts the right horizontal tail of unmanned plane out；When unmanned plane to be filled
When wing and empennage, by the preceding carbon pore of the fuselage wing aluminum component of carbon pipe insertion unmanned plane port wing before wing, by carbon after wing
Pipe be inserted into unmanned plane port wing fuselage wing aluminum component rear carbon pore, port wing after carbon pipe before wing and wing carbon pipe to
Unmanned aerial vehicle body promotes, and when port wing is advancing to the position, preceding fastener system component and the rear catch component of a system are automatically by port wing
Fuselage wing aluminum component and wing aluminum component locking, the Quick Release aviation plug female and Quick Release being set in Quick Release aviation plug hole location
Carbon pipe before wing also simultaneously to inserting, is inserted into the preceding carbon pore of the fuselage wing aluminum component of unmanned plane starboard wing by aviation plug male connector,
By after wing carbon pipe insertion unmanned plane starboard wing fuselage wing aluminum component rear carbon pore, starboard wing before wing carbon pipe and machine
Carbon pipe is promoted to unmanned aerial vehicle body after the wing, and when starboard wing is advancing to the position, preceding fastener system component and the rear catch component of a system are certainly
Dynamic fuselage wing aluminum component and wing aluminum component by starboard wing is locked, the Quick Release aviation plug being set in Quick Release aviation plug hole location
Female and Quick Release aviation plug male connector are also simultaneously to slotting, the Quick Release quick fixation structure device dismantling side of the unmanned plane wing and empennage
Just, without dismantling and installation the end of a thread, it is not necessarily to the turn of the screw, dismantling only needs button press can be completed, can be accurately quickly fixed when installation
Position installation is saved artificial.
Detailed description of the invention
Fig. 1 is the overall structure figure of the Quick Release quick fixation structure device of a kind of unmanned plane wing of the utility model and empennage；
Fig. 2 is the wing aluminum component structure of the Quick Release quick fixation structure device of a kind of unmanned plane wing of the utility model and empennage
Structure chart.
Specific embodiment
In order to make the purpose of the utility model, technical solutions and advantages more clearly understood, below in conjunction with attached drawing and implementation
Example, the present invention will be further described in detail.It should be appreciated that specific embodiment described herein is used only for explaining
The utility model is not used to limit the utility model.
Fig. 1 and Fig. 2 is please referred to, Fig. 1 is the Quick Release quick fixation structure device of a kind of unmanned plane wing of the utility model and empennage
Overall structure figure；Fig. 2 is the wing aluminum component of the Quick Release quick fixation structure device of a kind of unmanned plane wing of the utility model and empennage
The structure chart of structure.
Embodiment 1
In the present embodiment, the Quick Release quick fixation structure device of a kind of unmanned plane wing and empennage, including be set on fuselage 1
Fuselage wing aluminum component 32, on setting wing and the wing aluminum component 31, the carbon before wing that are assembled together with fuselage wing aluminum component 32
Carbon pipe 34 after pipe 33 and wing, fuselage wing aluminum component 32 and wing aluminum component 31 are assembled together to form wing aluminum component structure 3, wing
There are two the preceding button 311 and rear button 318 for disassembling wing aluminum component structure, wing aluminium for setting among 3 top of aluminum component structure
3 front of part structure is provided with the preceding carbon pore 313 for inserting carbon pipe 33 before wing, and preceding carbon pore 313 runs through fuselage wing aluminum component
32 and wing aluminum component 31,3 rear portion of wing aluminum component structure is provided with the rear carbon pore 320 for inserting carbon pipe 34 after wing, rear carbon pipe
Fuselage wing aluminum component 32 and wing aluminum component 31 are run through in hole 320, are provided in wing aluminum component structure 3 for that will assemble the fuselage completed
The preceding fastener system component and the rear catch component of a system that wing aluminum component 32 and wing aluminum component 32 are locked in together latch system before described
System component and the rear catch component of a system are respectively arranged at the front and rear portion of wing aluminum component structure 3.
In the present embodiment, Quick Release aviation plug hole location 316, Quick Release aviation plug hole are provided in wing aluminum component structure 3
Position 316 is set in the Quick Release aviation plug hole location 316 of fuselage wing aluminum component 32 through fuselage wing aluminum component 32 and wing aluminum component 31
It is equipped with Quick Release aviation plug female, is provided with Quick Release aviation plug male connector in the Quick Release aviation plug hole location of wing aluminum component 31.
The Quick Release aviation plug male connector and the Quick Release aviation plug female integrated power source line, steering engine line, throttle line in
One.
The preceding fastener system component includes preceding button 311, is set to 32 front of fuselage wing aluminum component preceding lock 314,
The preceding spring 315 of 314 lower parts of lock before being set to, for being set on wing aluminum component 31 and capable of being used to be fastened by preceding lock 314
One is raised, offers the first locking slot in the first protrusion.
The rear catch component of a system includes rear button 318, the rear catch 321 for being set to 32 rear portion of fuselage wing aluminum component,
It is set to the rear spring 322 of 321 lower part of rear catch, be set on wing aluminum component 31 and can be used for is convex by the second of rear catch fastening
It rises, offers the second locking slot in second protrusion.
In the present embodiment, before the seam crossing of the fuselage wing aluminum component 32 of wing aluminum component structure 3 and wing aluminum component 31
Rear end is provided with preceding umbrella rope hanging point and rear umbrella rope hanging point.
In the present embodiment, the Quick Release quick fixation structure device of the unmanned plane wing and empennage further includes being set to fuselage 1
On fuselage horizontal tail aluminum component 91, the horizontal tail aluminum component 92, flat that is set on empennage and is assembled together with the fuselage horizontal tail aluminum component
Tail carbon pipe 93, fuselage horizontal tail aluminum component 91 and horizontal tail aluminum component 92 are assembled together to form horizontal tail aluminum component structure 9, horizontal tail aluminum component structure 9
On be provided with horizontal tail carbon pore for inserting horizontal tail carbon pipe, the horizontal tail carbon pore runs through fuselage horizontal tail aluminum component 91 and horizontal tail aluminum component
92。
Embodiment 2
In the present embodiment, the structure of the Quick Release aviation plug hole location 316 of wing aluminum component structure 3 replaces with：Wing aluminum component
It is provided with Quick Release aviation plug hole location in structure 3, Quick Release aviation plug hole location is through fuselage wing aluminum component 32 and wing aluminum component
31, Quick Release aviation plug male connector, the Quick Release of wing aluminum component 31 are provided in the Quick Release aviation plug hole location of fuselage wing aluminum component 32
Quick Release aviation plug female is provided in aviation plug hole location.
After using the above structure, the Quick Release quick fixation structure device of unmanned plane wing and empennage, including be set on fuselage 1
Fuselage wing aluminum component 32, on setting wing and the wing aluminum component 31, the carbon before wing that are assembled together with fuselage wing aluminum component 32
Carbon pipe 34 after pipe 33 and wing, fuselage wing aluminum component 32 and wing aluminum component 31 are assembled together to form wing aluminum component structure 3, wing
There are two the preceding button 311 and rear button 318 for disassembling wing aluminum component structure, wing aluminium for setting among 3 top of aluminum component structure
3 front of part structure is provided with the preceding carbon pore 313 for inserting carbon pipe 33 before wing, and preceding carbon pore 313 runs through fuselage wing aluminum component
32 and wing aluminum component 31,3 rear portion of wing aluminum component structure is provided with the rear carbon pore 320 for inserting carbon pipe 34 after wing, rear carbon pipe
Fuselage wing aluminum component 32 and wing aluminum component 31 are run through in hole 320, are provided in wing aluminum component structure 3 for that will assemble the fuselage completed
The preceding fastener system component and the rear catch component of a system that wing aluminum component 32 and wing aluminum component 32 are locked in together latch system before described
System component and the rear catch component of a system are respectively arranged at the front and rear portion of wing aluminum component structure 3, when unmanned plane wing to be disassembled
When with empennage, 318 two buttons of preceding button 311 and rear button in the wing aluminum component structure 3 on port wing 2 are pressed, are then taken out
Unmanned plane port wing out presses 318 two buttons of preceding button 311 and rear button in the wing aluminum component structure 3 on starboard wing 6,
Then it extracts unmanned plane starboard wing out, presses the button in the horizontal tail aluminum component structure 3 in left horizontal tail 8, then extract a left side for unmanned plane out
Horizontal tail 8 presses the button in the horizontal tail aluminum component structure in right horizontal tail 12, then extracts the right horizontal tail 12 of unmanned plane out；When nothing to be filled
When man-machine wing and empennage, carbon pipe 33 before wing is inserted into the preceding carbon pore 313 of the fuselage wing aluminum component of unmanned plane port wing 2,
Carbon pipe 34 after wing is inserted into the rear carbon pore 320 of the fuselage wing aluminum component 32 of unmanned plane port wing, port wing 2 before wing
After carbon pipe 33 and wing carbon pipe 34 to unmanned aerial vehicle body 1 promote, when port wing 2 is advancing to the position, preceding fastener system component and after
Fastener system component automatically locks the fuselage wing aluminum component 32 and wing aluminum component 31 of port wing 2, is set to Quick Release aviation plug
Carbon pipe 33 before wing is inserted into nothing also simultaneously to inserting by Quick Release aviation plug female and Quick Release aviation plug male connector in hole location 316
Carbon pipe 34 after wing is inserted into the fuselage of unmanned plane starboard wing 6 by the preceding carbon pore 313 of the fuselage wing aluminum component of man-machine starboard wing 6
The rear carbon pore 320 of wing aluminum component, starboard wing 6, carbon pipe 34 is promoted to unmanned aerial vehicle body 1 after carbon pipe 33 before wing and wing,
When starboard wing 6 is advancing to the position, preceding fastener system component and the rear catch component of a system are automatically by the fuselage wing aluminum component of starboard wing 6
32 and wing aluminum component 31 lock, be set to Quick Release aviation plug female in Quick Release aviation plug hole location 316 and Quick Release aviation inserted
Head male connector is also simultaneously to inserting, and it is convenient that the Quick Release quick fixation structure device of the unmanned plane wing and empennage is disassembled, without dismantling and installation
The end of a thread is not necessarily to the turn of the screw, and dismantling only needs button press can be completed, when installation can accurate quick location and installation, save artificial.
It should be understood that cannot therefore limit the utility model the above is only the preferred embodiment of the utility model
The scope of the patents, equivalent structure or equivalent flow shift made by using the description of the utility model and the drawings, or it is straight
It connects or is used in other related technical areas indirectly, be also included in the patent protection scope of the utility model.
Claims (8)
1. the Quick Release quick fixation structure device of a kind of unmanned plane wing and empennage, which is characterized in that including the machine being set on fuselage
Carbon pipe and machine before the wing aluminum component being assembled together on wing and with the fuselage wing aluminum component, wing is arranged in body wing aluminum component
Carbon pipe after the wing, the fuselage wing aluminum component and wing aluminum component are assembled together to form wing aluminum component structure, the wing aluminum component knot
There are two the preceding button and rear button for disassembling wing aluminum component structure, the wing aluminum component structure fronts for setting among structure top
It is provided with the preceding carbon pore for inserting carbon pipe before wing, the preceding carbon pore runs through the fuselage wing aluminum component and wing aluminum component,
The wing aluminum component structure rear portion is provided with the rear carbon pore for inserting carbon pipe after wing, it is described after carbon pore run through the fuselage
Wing aluminum component and wing aluminum component, be provided in the wing aluminum component structure for will assemble the fuselage wing aluminum component completed and
The preceding fastener system component and the rear catch component of a system that wing aluminum component is locked in together, the preceding fastener system component and rear catch
The component of a system is respectively arranged at the front and rear portion of the wing aluminum component structure.
2. the Quick Release quick fixation structure device of unmanned plane wing according to claim 1 and empennage, it is characterised in that：The machine
It is provided with Quick Release aviation plug hole location in wing aluminum component structure, the Quick Release aviation plug hole location is through the fuselage wing aluminum component
And wing aluminum component, Quick Release aviation plug female, the machine are provided in the Quick Release aviation plug hole location of the fuselage wing aluminum component
Quick Release aviation plug male connector is provided in the Quick Release aviation plug hole location of wing aluminum component.
3. the Quick Release quick fixation structure device of unmanned plane wing according to claim 1 and empennage, it is characterised in that：The machine
It is provided with Quick Release aviation plug hole location in wing aluminum component structure, the Quick Release aviation plug hole location is through the fuselage wing aluminum component
And wing aluminum component, Quick Release aviation plug male connector, the machine are provided in the Quick Release aviation plug hole location of the fuselage wing aluminum component
Quick Release aviation plug female is set in wing aluminum component Quick Release aviation plug hole location.
4. the Quick Release quick fixation structure device of unmanned plane wing according to claim 2 or 3 and empennage, it is characterised in that：Institute
Quick Release aviation plug male connector and the Quick Release aviation plug female integrated power source line, steering engine line, throttle line are stated in one.
5. the Quick Release quick fixation structure device of unmanned plane wing according to claim 1 and empennage, it is characterised in that：Before described
Fastener system component includes the preceding button, the preceding lock for being set to the fuselage wing aluminum component front, is set to the preceding lock
The preceding spring for detaining portion, the first protrusion for being set on the wing aluminum component and capable of being used to be fastened by the preceding lock, described the
The first locking slot is offered in one protrusion.
6. the Quick Release quick fixation structure device of unmanned plane wing according to claim 1 and empennage, it is characterised in that：After described
Fastener system component includes the rear button, the rear catch for being set to the fuselage wing aluminum component rear portion, is set to the rear lock
The rear spring for detaining portion, the second protrusion for being set on the wing aluminum component and capable of being used to be fastened by the rear catch, described the
The second locking slot is offered in two protrusions.
7. the Quick Release quick fixation structure device of unmanned plane wing according to claim 1 and empennage, it is characterised in that：Described
Umbrella rope is hung before the front and back end of the seam crossing of the fuselage wing aluminum component and the wing aluminum component in wing aluminum component structure is provided with
Point and rear umbrella rope hanging point.
8. the Quick Release quick fixation structure device of unmanned plane wing according to claim 1 and empennage, which is characterized in that the nothing
The Quick Release quick fixation structure device of man-machine wing and empennage further includes the fuselage horizontal tail aluminum component being set on fuselage, is set on empennage
And horizontal tail aluminum component, the horizontal tail carbon pipe being assembled together with the fuselage horizontal tail aluminum component, the fuselage horizontal tail aluminum component and horizontal tail aluminum component
It is assembled together to form horizontal tail aluminum component structure, the horizontal tail carbon pipe for inserting horizontal tail carbon pipe is provided in the horizontal tail aluminum component structure
Hole, the horizontal tail carbon pore run through the fuselage horizontal tail aluminum component and horizontal tail aluminum component.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820426148.5U CN208165244U (en) | 2018-03-27 | 2018-03-27 | A kind of Quick Release quick fixation structure device of unmanned plane wing and empennage |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820426148.5U CN208165244U (en) | 2018-03-27 | 2018-03-27 | A kind of Quick Release quick fixation structure device of unmanned plane wing and empennage |
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| Publication Number | Publication Date |
|---|---|
| CN208165244U true CN208165244U (en) | 2018-11-30 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820426148.5U Active CN208165244U (en) | 2018-03-27 | 2018-03-27 | A kind of Quick Release quick fixation structure device of unmanned plane wing and empennage |
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| CN (1) | CN208165244U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108382564A (en) * | 2018-03-27 | 2018-08-10 | 山西迪奥普科技有限公司 | A kind of Quick Release quick fixation structure device and method of unmanned plane wing and empennage |
| WO2020134235A1 (en) * | 2018-12-28 | 2020-07-02 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle and wing assembly thereof |
-
2018
- 2018-03-27 CN CN201820426148.5U patent/CN208165244U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108382564A (en) * | 2018-03-27 | 2018-08-10 | 山西迪奥普科技有限公司 | A kind of Quick Release quick fixation structure device and method of unmanned plane wing and empennage |
| WO2020134235A1 (en) * | 2018-12-28 | 2020-07-02 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle and wing assembly thereof |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A structure device for quick disassembly and quick assembly of UAV wing and tail Effective date of registration: 20210125 Granted publication date: 20181130 Pledgee: Shanxi Financing Reinsurance Group Co.,Ltd. Pledgor: SHANXI DOP TECHNOLOGY Co.,Ltd.|SHENZHEN DI AOPU UAV Co.,Ltd. Registration number: Y2021980000704 |
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| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20210601 Granted publication date: 20181130 Pledgee: Shanxi Financing Reinsurance Group Co.,Ltd. Pledgor: SHANXI DOP TECHNOLOGY Co.,Ltd.|SHENZHEN DI AOPU UAV Co.,Ltd. Registration number: Y2021980000704 |
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| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 030000 room 313, No. 249, Changzhi Road, high tech Zone, Taiyuan, Shanxi Patentee after: SHANXI DOP TECHNOLOGY Co.,Ltd. Patentee after: Shenzhen Diop UAV Co.,Ltd. Address before: 030000 room 313, No. 249, Changzhi Road, high tech Zone, Taiyuan, Shanxi Patentee before: SHANXI DOP TECHNOLOGY Co.,Ltd. Patentee before: SHENZHEN DI AOPU UAV Co.,Ltd. |
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| CP01 | Change in the name or title of a patent holder | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A quick disassembly and quick assembly structure device for UAV wing and tail Effective date of registration: 20210830 Granted publication date: 20181130 Pledgee: Shanxi Financing Guarantee Co.,Ltd. Pledgor: SHANXI DOP TECHNOLOGY Co.,Ltd. Registration number: Y2021140000031 |
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| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20220905 Granted publication date: 20181130 Pledgee: Shanxi Financing Guarantee Co.,Ltd. Pledgor: SHANXI DOP TECHNOLOGY CO.,LTD. Registration number: Y2021140000031 |
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| PC01 | Cancellation of the registration of the contract for pledge of patent right |