CN208233340U - A kind of unmanned plane Quick Release aviation plug device - Google Patents
A kind of unmanned plane Quick Release aviation plug device Download PDFInfo
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- CN208233340U CN208233340U CN201820419447.6U CN201820419447U CN208233340U CN 208233340 U CN208233340 U CN 208233340U CN 201820419447 U CN201820419447 U CN 201820419447U CN 208233340 U CN208233340 U CN 208233340U
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- quick release
- aluminum component
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- aviation plug
- release aviation
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Abstract
The utility model discloses a kind of unmanned plane Quick Release aviation plug devices, including the fuselage wing aluminum component being set on unmanned aerial vehicle body, the wing aluminum component for being set on unmanned plane wing and being assembled together with the fuselage wing aluminum component, the fuselage wing aluminum component and wing aluminum component are assembled together to form wing aluminum component structure, the first Quick Release aviation plug hole location is provided in the wing aluminum component structure, the first Quick Release aviation plug hole location is through the fuselage wing aluminum component and wing aluminum component, the first Quick Release aviation plug female is provided in first Quick Release aviation plug hole location of the fuselage wing aluminum component, the first Quick Release aviation plug male connector is provided in first Quick Release aviation plug hole location of the wing aluminum component, the unmanned plane Quick Release aviation plug device can be more accurate close when resetting after the fuselage of unmanned plane and the end of a thread of wing can be allowed to disassemble Cooperate, automatic engagement, the end of a thread will not be omitted, be tightly fastened with fuselage and wing, precision is high, it is anti-inserted to prevent.
Description
Technical field
The utility model relates to unmanned plane equipment technical field more particularly to a kind of unmanned plane Quick Release aviation plug devices.
Background technique
Unmanned plane is made of fuselage, wing, empennage etc., transports for convenience, unmanned plane is split as to fuselage, left machine respectively
The wing, starboard wing, left horizontal tail, right horizontal tail etc..
During previous unmanned plane dismantling, wing and the fuselage of unmanned plane will be separated, and can leave several the end of a thread, and
And each the end of a thread can need with fuselage to fill the wing of unmanned plane again with interfix, when unmanned plane to be ressembled
It prepares, so just will increase a series of mistake and risk, some line in unmanned aerial vehicle body may be in wing
Some the end of a thread be on not, after the assembly is completed, unmanned plane can not normal use,
Therefore, those skilled in the art has been devoted to research and develop a kind of fuselage of unmanned plane and the end of a thread of wing of can allowing
It can more accurately be fitted close when being reset after dismantling, engage automatically, the end of a thread will not be omitted, being tightly fastened with fuselage and wing, essence
Degree is high, prevents anti-inserted unmanned plane Quick Release aviation plug device.
Utility model content
The technical problem to be solved by the present invention is to provide a kind of unmanned plane Quick Release aviation plug device, the unmanned plane is fast
Tear open aviation plug device can allow unmanned plane fuselage and wing the end of a thread dismantling after reset when can more accurately be fitted close, from
Dynamic engagement, the end of a thread will not be omitted, be tightly fastened with fuselage and wing, precision height, prevent it is anti-inserted.
In order to solve the above technical problems, the utility model provides a kind of unmanned plane Quick Release aviation plug device, including setting
In on unmanned aerial vehicle body fuselage wing aluminum component, be set on unmanned plane wing and be assembled together with the fuselage wing aluminum component
Wing aluminum component, the fuselage wing aluminum component and wing aluminum component be assembled together to form wing aluminum component structure, the wing aluminum component
It is provided with the first Quick Release aviation plug hole location in structure, the first Quick Release aviation plug hole location is through the fuselage wing aluminium
It is female to be provided with the first Quick Release aviation plug in the first Quick Release aviation plug hole location of the fuselage wing aluminum component for part and wing aluminum component
Head is provided with the first Quick Release aviation plug male connector in the first Quick Release aviation plug hole location of the wing aluminum component.
Preferably, the unmanned plane Quick Release aviation plug device further includes the fuselage horizontal tail aluminum component being set on fuselage, sets
The horizontal tail aluminum component for being placed on wing and 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 second Quick Release aviation plug hole location is provided in the wing aluminum component structure, it is described
Second Quick Release aviation plug hole location runs through the fuselage horizontal tail aluminum component and horizontal tail aluminum component, the second Quick Release of the fuselage horizontal tail aluminum component
The second Quick Release aviation plug female is provided in aviation plug hole location, in the second Quick Release aviation plug hole location of the horizontal tail aluminum component
It is provided with the second Quick Release aviation plug male connector.
Preferably, the first Quick Release aviation plug male connector includes the first plug front and the first plug connector rear, and described the
The first plate washer is provided among one plug front and first plug connector rear, the first plate washer edge offers several use
Before the first mounting-positioning holes that the first Quick Release aviation plug male connector is assemblied in the wing aluminum component, first plug
The cross section in portion is in ladder type, and described first, which inserts procephalic centre, offers several the end of a thread pin holes, first plug front
The two sides of the end of a thread pin holes open up there are two for engaging the engagement groove of positioning automatically with the first Quick Release aviation plug female,
First plug connector rear offers wiring slot.
Preferably, the first Quick Release aviation plug female includes the second plug front and the second plug connector rear, and described the
The second plate washer is provided among two plug fronts and second plug connector rear, the second gear plate edge offers several use
It is positioned in the second installation that the first Quick Release aviation plug female is assemblied in the fuselage wing aluminum component, second plug
The cross section of front is in the ladder type groove profile of intermediate hollow out, and described second, which inserts procephalic centre, offers several the end of a thread contact pins, institute
State the two sides that second inserts procephalic the end of a thread contact pin open up there are two for the first Quick Release aviation plug male connector automatically engage calmly
The engagement pillar of position, second plug connector rear offer wiring slot.
Preferably, the feature " is provided with the first Quick Release boat in the first Quick Release aviation plug hole location of fuselage wing aluminum component
Blind plug female is provided with the first Quick Release aviation plug male connector in the first Quick Release aviation plug hole location of the wing aluminum component " it replaces
It is changed to and " is provided with the first Quick Release aviation plug male connector, the wing in the first Quick Release aviation plug hole location of fuselage wing aluminum component
The first Quick Release aviation plug female is provided in first Quick Release aviation plug hole location of aluminum component ".
Preferably, the second Quick Release aviation plug male connector includes third plug front and third plug connector rear, and described
Third plate washer is provided among three plug fronts and the third plug connector rear, the third gear plate edge offers several use
In the second Quick Release aviation plug male connector is assemblied in the third mounting-positioning holes on the horizontal tail aluminum component, the third plug
The cross section of front is in ladder type, and the third inserts procephalic centre and offers several the end of a thread pin holes, before the third plug
The two sides of the end of a thread pin holes in portion open up that there are two recessed for the engagement that engages positioning automatically with the second Quick Release aviation plug female
Slot, the third plug connector rear offer wiring slot.
Preferably, the second Quick Release aviation plug female includes the 4th plug front and the 4th plug connector rear, and described the
Fourth speed plate is provided among four plug fronts and the 4th plug connector rear, the fourth speed plate edge offers several use
It is positioned in the 4th installation that the second Quick Release aviation plug female is assemblied on the fuselage horizontal tail aluminum component, the described 4th inserts
Procephalic cross section is in the ladder type groove profile of intermediate hollow out, and the described 4th, which inserts procephalic centre, offers several the end of a thread contact pins,
Described 4th two sides for inserting procephalic the end of a thread contact pin are used to engage automatically with the second Quick Release aviation plug male connector there are two opening up
The engagement pillar of positioning, the 4th plug connector rear offer wiring slot.
Preferably, the feature " it is fast to be provided with second in the second Quick Release aviation plug hole location of the fuselage horizontal tail aluminum component
It tears aviation plug female open, it is public that the second Quick Release aviation plug is provided in the second Quick Release aviation plug hole location of the horizontal tail aluminum component
" replace with " it is provided with the second Quick Release aviation plug male connector in the second Quick Release aviation plug hole location of the fuselage horizontal tail aluminum component,
The second Quick Release aviation plug female is provided in second Quick Release aviation plug hole location of the horizontal tail aluminum component.".
Preferably, the first Quick Release aviation plug male connector and the first Quick Release aviation plug female integrated power source line,
Steering engine line, throttle line are in one.
Preferably, the second Quick Release aviation plug male connector and the second Quick Release aviation plug female integrated power source line,
Steering engine line, throttle line are in one.
After using the above structure, a kind of unmanned plane Quick Release aviation plug device, including being set on unmanned aerial vehicle body
Fuselage wing aluminum component, the wing aluminum component for being set on unmanned plane wing and being assembled together with the fuselage wing aluminum component, fuselage
Wing aluminum component and wing aluminum component are assembled together to form wing aluminum component structure, and the first Quick Release aviation is provided in wing aluminum component structure
Plug hole location, the first Quick Release aviation plug hole location is through the fuselage wing aluminum component and wing aluminum component 31, fuselage wing aluminum component
The first Quick Release aviation plug hole location on be provided with the first Quick Release aviation plug female, the first Quick Release aviation plug of wing aluminum component
The first Quick Release aviation plug male connector is provided in hole location.When unmanned plane wing to be filled and when empennage, wing along carbon pipe to nobody
Machine fuselage promotes, and when port wing is advancing to the position, automatically locks the fuselage wing aluminum component of wing and wing aluminum component, is set to the
The first Quick Release aviation plug female 34 and the first Quick Release aviation plug male connector in one Quick Release aviation plug hole location also simultaneously to inserting,
First plug front 334 is accurately engaged with the second plug front, and the end of a thread pin holes are accurately engaged with the end of a thread contact pin, and the unmanned plane is fast
Tear open aviation plug device can allow unmanned plane fuselage and wing the end of a thread dismantling after reset when can more accurately be fitted close, from
Dynamic engagement, the end of a thread will not be omitted, be tightly fastened with fuselage and wing, precision height, prevent it is anti-inserted.
Detailed description of the invention
Fig. 1 is a kind of overall structure figure of unmanned plane Quick Release aviation plug device of the utility model；
Fig. 2 is a kind of assembly structure figure of the wing section of unmanned plane Quick Release aviation plug device of the utility model；
Fig. 3 is a kind of Quick Release aviation plug male connector of unmanned plane Quick Release aviation plug device of the utility model and the knot of female
Composition.
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 a kind of overall structure figure of unmanned plane Quick Release aviation plug device of the utility model；
Fig. 2 is a kind of assembly structure figure of the wing section of unmanned plane Quick Release aviation plug device of the utility model.
Embodiment 1
In the present embodiment, a kind of unmanned plane Quick Release aviation plug device, including the fuselage being set on unmanned aerial vehicle body 1
Wing aluminum component 32, the wing aluminum component 31 for being set on unmanned plane wing 2 and being assembled together with the fuselage wing aluminum component 32, machine
Body wing aluminum component 32 and wing aluminum component 31 are assembled together to form wing aluminum component structure 3, are provided with first in wing aluminum component structure 3
Quick Release aviation plug hole location 316, the first Quick Release aviation plug hole location 316 is through the fuselage wing aluminum component 32 and wing aluminum component
31, the first Quick Release aviation plug female 34, wing are provided in the first Quick Release aviation plug hole location 316 of fuselage wing aluminum component 32
The first Quick Release aviation plug male connector 33 is provided in first Quick Release aviation plug hole location 316 of aluminum component 31.
First Quick Release aviation plug male connector 33 includes the first plug front 334 and the first plug connector rear 331, before the first plug
The first plate washer 332 is provided among portion 334 and the first plug connector rear 331,332 edge of the first plate washer offers several be used for
First Quick Release aviation plug male connector 33 is assemblied in the first mounting-positioning holes of wing aluminum component 31, the cross of the first plug front 334
Section is in ladder type, and the centre of the first plug front 334 offers several the end of a thread pin holes 333, the end of a thread of the first plug front 334
The two sides of pin holes 333 open up that there are two be used for and the first Quick Release aviation plug female 34 engage the engagement groove positioned automatically
335, the first plug connector rear 331 offers wiring slot.
Referring again to Fig. 3, the first Quick Release aviation plug female 34 includes the second plug front 342 and the second plug connector rear
341, the second plate washer 345 is provided among the second plug front 342 and the second plug connector rear 341, and 345 edge of the second plate washer is opened
It is positioned equipped with several the second installations for the first Quick Release aviation plug female 34 to be assemblied in fuselage wing aluminum component 32, second inserts
The cross section of head front 342 is in the ladder type groove profile of intermediate hollow out, and the centre of the second plug front 342 offers several the end of a thread contact pins
343, the two sides of the end of a thread contact pin 343 of the second plug front 342 open up there are two be used for and the first Quick Release aviation plug male connector 33
The engagement pillar 344 of automatic engagement positioning, the second plug connector rear 341 offer wiring slot.
First Quick Release aviation plug male connector 33 and 34 integrated power source line of the first Quick Release aviation plug female, steering engine line,
Throttle line is in one.
Embodiment 2
On the basis of embodiment 1, feature " is provided in the first Quick Release aviation plug hole location of fuselage wing aluminum component 32
First Quick Release aviation plug female 34 is provided with the first Quick Release boat in first Quick Release aviation plug hole location 316 of wing aluminum component 31
Blind plug male connector 33 ", which replaces with, " is provided with the first Quick Release boat in the first Quick Release aviation plug hole location 316 of fuselage wing aluminum component 32
Blind plug male connector 33 is provided with the first Quick Release aviation plug female in first Quick Release aviation plug hole location 316 of wing aluminum component 31
34”。
Embodiment 3
Unmanned plane Quick Release aviation plug device further includes the fuselage horizontal tail aluminum component 91 being set on fuselage 1, is set to empennage 8
Horizontal tail aluminum component 92 that is upper and being assembled together with fuselage horizontal tail aluminum component 91, fuselage horizontal tail aluminum component 91 and horizontal tail aluminum component 92 are assemblied in one
It rises and forms horizontal tail aluminum component structure 9, the second Quick Release aviation plug hole location, the second Quick Release boat are provided in horizontal tail aluminum component structure 9
Blind plug hole location runs through fuselage horizontal tail aluminum component 91 and horizontal tail aluminum component 92, the second Quick Release aviation plug hole location of fuselage horizontal tail aluminum component 91
On be provided with the second Quick Release aviation plug female 34, it is fast that second is provided in the second Quick Release aviation plug hole location of horizontal tail aluminum component 92
Tear aviation plug male connector 33 open.
Second Quick Release aviation plug male connector 33 includes third plug front 334 and third plug connector rear 331, before third plug
It is provided with third plate washer among portion 334 and the third plug connector rear 331,332 edge of third plate washer offers several be used for
Second Quick Release aviation plug male connector 33 is assemblied in the third mounting-positioning holes on horizontal tail aluminum component 92, third plug front 334
Cross section is in ladder type, and the centre of third plug front 334 offers several the end of a thread pin holes 333, the line of third plug front 334
The two sides of head pin holes 333 open up that there are two be used for and the second Quick Release aviation plug female 34 engage the engagement groove positioned automatically
335, third plug connector rear 331 offers wiring slot.
Second Quick Release aviation plug female 34 includes the 4th plug front 342 and the 4th plug connector rear 341, before the 4th plug
Fourth speed plate 345 is provided among portion 342 and the 4th plug connector rear 341,345 edge of fourth speed plate offers several be used for
Second Quick Release aviation plug female 34 is assemblied in the 4th installation positioning on fuselage horizontal tail aluminum component 32, the 4th plug front 342
Cross section be in intermediate hollow out ladder type groove profile, the centre of the 4th plug front 342 offers several the end of a thread contact pins 343, the 4th
The two sides of the end of a thread contact pin 343 of plug front 342 open up fixed there are two being used to engage automatically with the second Quick Release aviation plug male connector
The engagement pillar of position, the 4th plug connector rear offer wiring slot.
First Quick Release aviation plug female 34 includes the second plug front 342 and the second plug connector rear 341, before the second plug
The second plate washer 345 is provided among portion 342 and the second plug connector rear 341,345 edge of the second plate washer offers several be used for
First Quick Release aviation plug female 34 is assemblied in the second installation positioning of fuselage wing aluminum component 32, the second plug front 342
Cross section is in the ladder type groove profile of intermediate hollow out, and the centre of the second plug front 342 offers several the end of a thread contact pins 343, and second inserts
The two sides of the end of a thread contact pin 343 of head front 342 open up fixed there are two being used to engage automatically with the first Quick Release aviation plug male connector 33
The engagement pillar 344 of position, the second plug connector rear 341 offer wiring slot.
34 integrated power source line of second Quick Release aviation plug male connector 33 and the second Quick Release aviation plug female, steering engine line, throttle
Line is in one.
Embodiment 4
On the basis of embodiment 3, the feature " is arranged in the second Quick Release aviation plug hole location of fuselage horizontal tail aluminum component 91
There is the second Quick Release aviation plug female 34, is provided with the second Quick Release aviation in the second Quick Release aviation plug hole location of horizontal tail aluminum component 92
Plug male connector 33 ", which replaces with, " to be provided with the second Quick Release aviation to insert in the second Quick Release aviation plug hole location of fuselage horizontal tail aluminum component 91
Head male connector 33, is provided with the second Quick Release aviation plug female 34 in the second Quick Release aviation plug hole location of horizontal tail aluminum component 92."
After using the above structure, a kind of unmanned plane Quick Release aviation plug device, including being set on unmanned aerial vehicle body
Fuselage wing aluminum component 32, the wing aluminum component for being set on unmanned plane wing and being assembled together with the fuselage wing aluminum component 32
31, fuselage wing aluminum component 32 and wing aluminum component 31 are assembled together to form wing aluminum component structure 3, are arranged in wing aluminum component structure 3
There is the first Quick Release aviation plug hole location 316, the first Quick Release aviation plug hole location 316 is through the fuselage wing aluminum component 32 and machine
Wing aluminum component 31 is provided with the first Quick Release aviation plug female in first Quick Release aviation plug hole location 316 of fuselage wing aluminum component 32
34, the first Quick Release aviation plug male connector 33 is provided in the first Quick Release aviation plug hole location 316 of wing aluminum component 31.When nothing to be filled
When man-machine wing and empennage, wing is promoted along carbon pipe to unmanned aerial vehicle body 1, when port wing is advancing to the position, automatically by wing
Fuselage wing aluminum component 32 and wing aluminum component 31 lock, be set in the first Quick Release aviation plug hole location 316 the first Quick Release boat
Blind plug female 34 and the first Quick Release aviation plug male connector 33 are also simultaneously to slotting, the first plug front 334 and the second plug front
342 accurate engagements, the end of a thread pin holes 333 are accurately engaged with the end of a thread contact pin 343, which can allow
It can more accurately be fitted close, engage automatically, line will not be omitted when being reset after the fuselage 1 of unmanned plane and the dismantling of the end of a thread of wing
Head, be tightly fastened with fuselage and wing, precision height, prevent it is anti-inserted.
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 (10)
1. a kind of unmanned plane Quick Release aviation plug device, which is characterized in that including the fuselage wing being set on unmanned aerial vehicle body
Aluminum component, the wing aluminum component for being set on unmanned plane wing and being assembled together with the fuselage wing aluminum component, the fuselage wing
Aluminum component and wing aluminum component are assembled together to form wing aluminum component structure, and the first Quick Release aviation is provided in the wing aluminum component structure
Plug hole location, the first Quick Release aviation plug hole location is through the fuselage wing aluminum component and wing aluminum component, the fuselage machine
The first Quick Release aviation plug female is provided in first Quick Release aviation plug hole location of wing aluminum component, the first of the wing aluminum component is fast
It tears open and is provided with the first Quick Release aviation plug male connector in aviation plug hole location.
2. unmanned plane Quick Release aviation plug device according to claim 1, which is characterized in that the unmanned plane Quick Release aviation
Plug device further includes the fuselage horizontal tail aluminum component being set on fuselage, is set on wing and assembles with the fuselage horizontal tail aluminum component
Horizontal tail aluminum component together, the fuselage horizontal tail aluminum component and horizontal tail aluminum component are assembled together to form horizontal tail aluminum component structure, the machine
The second Quick Release aviation plug hole location is provided in wing aluminum component structure, the second Quick Release aviation plug hole location is flat through the fuselage
Tail aluminum component and horizontal tail aluminum component are provided with the second Quick Release aviation in the second Quick Release aviation plug hole location of the fuselage horizontal tail aluminum component and insert
Head female, is provided with the second Quick Release aviation plug male connector in the second Quick Release aviation plug hole location of the horizontal tail aluminum component.
3. unmanned plane Quick Release aviation plug device according to claim 1, it is characterised in that: the first Quick Release aviation is inserted
Head male connector includes the first plug front and the first plug connector rear, is set among first plug front and first plug connector rear
It is equipped with the first plate washer, the first plate washer edge offers several for the first Quick Release aviation plug male connector to be assemblied in
First mounting-positioning holes of the wing aluminum component, described first inserts procephalic cross section in ladder type, first plug front
Centre offer several the end of a thread pin holes, the described first two sides for inserting procephalic the end of a thread pin holes open up there are two for
First Quick Release aviation plug female engages the engagement groove of positioning automatically, and first plug connector rear offers wiring slot.
4. unmanned plane Quick Release aviation plug device according to claim 1, it is characterised in that: the first Quick Release aviation is inserted
Head female includes the second plug front and the second plug connector rear, is set among second plug front and second plug connector rear
It is equipped with the second plate washer, the second gear plate edge offers several for the first Quick Release aviation plug female to be assemblied in
Second installation positioning of the fuselage wing aluminum component, described second inserts the ladder type groove profile that procephalic cross section is in intermediate hollow out,
Described second, which inserts procephalic centre, offers several the end of a thread contact pins, and the described second two sides for inserting procephalic the end of a thread contact pin open up
There are two the engagement pillar for engaging positioning automatically with the first Quick Release aviation plug male connector, second plug connector rear is offered
Wiring slot.
5. unmanned plane Quick Release aviation plug device according to claim 2, it is characterised in that: the second Quick Release aviation is inserted
Head male connector includes third plug front and third plug connector rear, is set among third plug front and the third plug connector rear
It is equipped with third plate washer, the third gear plate edge offers several for the second Quick Release aviation plug male connector to be assemblied in
Third mounting-positioning holes on the horizontal tail aluminum component, the third insert procephalic cross section in ladder type, before the third plug
The centre in portion offers several the end of a thread pin holes, and the two sides that the third inserts procephalic the end of a thread pin holes open up that there are two be used for
Engage the engagement groove of positioning automatically with the second Quick Release aviation plug female, the third plug connector rear offers wiring slot.
6. unmanned plane Quick Release aviation plug device according to claim 2, it is characterised in that: the second Quick Release aviation is inserted
Head female includes the 4th plug front and the 4th plug connector rear, is set among the 4th plug front and the 4th plug connector rear
It is equipped with fourth speed plate, the fourth speed plate edge offers several for the second Quick Release aviation plug female to be assemblied in
The 4th installation positioning on the fuselage horizontal tail aluminum component, the described 4th inserts the ladder-type trough that procephalic cross section is in intermediate hollow out
Type, the described 4th, which inserts procephalic centre, offers several the end of a thread contact pins, and the described 4th inserts the two sides of procephalic the end of a thread contact pin
It opens up there are two the engagement pillar for engaging positioning automatically with the second Quick Release aviation plug male connector, the 4th plug connector rear is opened
Equipped with wiring slot.
7. unmanned plane Quick Release aviation plug device according to claim 2, it is characterised in that: the fuselage horizontal tail aluminum component
The second Quick Release aviation plug male connector is provided in second Quick Release aviation plug hole location, the second Quick Release aviation of the horizontal tail aluminum component is inserted
The second Quick Release aviation plug female is provided on head bore position.
8. unmanned plane Quick Release aviation plug device according to claim 1, it is characterised in that: the first Quick Release aviation is inserted
Head male connector and the first Quick Release aviation plug female integrated power source line, steering engine line, throttle line are in one.
9. unmanned plane Quick Release aviation plug device according to claim 2, it is characterised in that: the second Quick Release aviation is inserted
Head male connector and the second Quick Release aviation plug female integrated power source line, steering engine line, throttle line are in one.
10. a kind of unmanned plane Quick Release aviation plug device, which is characterized in that including the fuselage wing being set on unmanned aerial vehicle body
Aluminum component, the wing aluminum component for being set on unmanned plane wing and being assembled together with the fuselage wing aluminum component, the fuselage wing
Aluminum component and wing aluminum component are assembled together to form wing aluminum component structure, and the first Quick Release aviation is provided in the wing aluminum component structure
Plug hole location, the first Quick Release aviation plug hole location is through the fuselage wing aluminum component and wing aluminum component, the fuselage machine
The first Quick Release aviation plug male connector is provided in first Quick Release aviation plug hole location of wing aluminum component, the first of the wing aluminum component is fast
It tears open and is provided with the first Quick Release aviation plug female in aviation plug hole location.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820419447.6U CN208233340U (en) | 2018-03-27 | 2018-03-27 | A kind of unmanned plane Quick Release aviation plug device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820419447.6U CN208233340U (en) | 2018-03-27 | 2018-03-27 | A kind of unmanned plane Quick Release aviation plug device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208233340U true CN208233340U (en) | 2018-12-14 |
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| CN201820419447.6U Active CN208233340U (en) | 2018-03-27 | 2018-03-27 | A kind of unmanned plane Quick Release aviation plug device |
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| CN (1) | CN208233340U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109665101A (en) * | 2019-01-07 | 2019-04-23 | 浙江自贸区协同科技有限公司 | A kind of modularization head |
-
2018
- 2018-03-27 CN CN201820419447.6U patent/CN208233340U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109665101A (en) * | 2019-01-07 | 2019-04-23 | 浙江自贸区协同科技有限公司 | A kind of modularization head |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address |
Address after: 518035 Room 201, building a, No. 1, Qianwan 1st Road, Qianhai Shenzhen Hong Kong cooperation zone, Nanshan street, Nanshan District, Shenzhen, Guangdong Province settled in Shenzhen Qianhai business secretary Co., Ltd Patentee after: Shenzhen Diop UAV Co.,Ltd. Address before: 518000 Room 201, building A, No. 1, Qian Wan Road, Qianhai Shenzhen Hong Kong cooperation zone, Shenzhen, Guangdong (Shenzhen Qianhai business secretary Co., Ltd.) Patentee before: SHENZHEN DI AOPU UAV Co.,Ltd. |
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| CP03 | Change of name, title or address |