CN205661647U - Be applied to folding mechanism on unmanned aerial vehicle horn - Google Patents
Be applied to folding mechanism on unmanned aerial vehicle horn Download PDFInfo
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- CN205661647U CN205661647U CN201620556985.0U CN201620556985U CN205661647U CN 205661647 U CN205661647 U CN 205661647U CN 201620556985 U CN201620556985 U CN 201620556985U CN 205661647 U CN205661647 U CN 205661647U
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Abstract
The utility model discloses a be applied to folding mechanism on unmanned aerial vehicle horn, including aluminum alloy mechanical component I, aluminum alloy mechanical component II, aluminum alloy mechanical component III, aluminum alloy mechanical component IV, stainless steel shaft I, stainless steel shaft II, stainless steel shaft III, aluminum alloy couple, unmanned aerial vehicle horn, integration base I, base II unifies, its characterized in that: aluminum alloy mechanical component I articulates through stainless steel shaft II and aluminum alloy mechanical component III, aluminum alloy mechanical component II is through stainless steel shaft I and I activity hinge joint of aluminum alloy mechanical component, aluminum alloy mechanical component IV is through stainless steel shaft III and III activity hinge joint of aluminum alloy mechanical component, the aluminum alloy couple is fixed on II surfaces of aluminum alloy mechanical component, the utility model discloses an it is simply small and exquisite, set up easily in a flexible way, do not need the help of instrument just can to expand and pack up, area is little when packing up, the development rate is fast, reachs the operation post and just can expand to carry on the operation fast.
Description
Technical field
This utility model relates to unmanned plane horn field, a kind of fold mechanism being applied on unmanned plane horn.
Background technology
In prior art, most unmanned planes are longer because of its horn, receive oversize, do not possess and launch easily and pack up
Ability.
The collapsible unmanned plane used on the market is when carrying out the design and the manufacture that fold, and scheme more typically is by rotor
The wing arm of type unmanned plane is bolted with main frame, when needing to launch wing arm, and loose bolts, promote wing arm with bolt as axle center
Horizontally rotating to the position vertical with main body surface, then fastening bolt completes rotor expansion.The automatic degree of this scheme is the highest,
Need to complete manually to fold, organize work, it is impossible to realize the rapid deployment of wing arm.
On the other hand, now with fold mechanism the method for buckle-type also can be used to fold, but set
Buckle is scarcely very flexible, and needs the cooperation of instrument to realize launching and packing up.
Utility model content
The purpose of this utility model is to provide a kind of fold mechanism being applied on unmanned plane horn, and it can effectively solve
Certainly problem present in background technology.
For achieving the above object, the following technical scheme of this utility model offer: a kind of folding being applied on unmanned plane horn
Folded mechanism, including aluminium alloy component I (1), aluminium alloy component II (2), aluminium alloy component III (3), aluminium alloy component
IV (4), stainless steel shaft I (5), stainless steel shaft II (6), stainless steel shaft III (7), aluminium alloy hook (8), unmanned plane horn (9)；Institute
State unmanned plane horn (9) and be installed in aluminium alloy component I (1) and the two ends of aluminium alloy component II；It is characterized in that: described aluminum
Alloy machine component I (1) is hinged with aluminium alloy component III (3) by stainless steel shaft II (6)；Described aluminium alloy component II (2)
It is movably hinged with aluminium alloy component I (1) by stainless steel shaft I (5)；Described aluminium alloy component IV (4) passes through stainless steel shaft
III (7) is movably hinged with aluminium alloy component III (3)；Described aluminium alloy hook (8) is fixed on aluminium alloy component II (2) table
Face；Described integrated base I (10) and integrated base II (11) are fixedly connected on aluminium alloy component I (1).
Further, described aluminium alloy component I (1) is movably hinged with aluminium alloy component II (2), and range of activity is 0 degree
Between 90 degree.
Further, the draw angle scope of described aluminium alloy component III (3) 86 degree 8 points 49 seconds to 87 degree 10 points 6 seconds
Between, the tensile elongation scope of its distance between axles is between 17.8 centimetres to 18.1 centimetres.
Compared with prior art, the beneficial effects of the utility model are: this fold mechanism is the smallest and the most exquisite, arrange light spirit
Live, make the expansion of unmanned plane horn and pack up quick, it is not necessary to the help of instrument；When packing up, floor space is little, can make unmanned plane
Volume, convenient operation is reduced when packed and transported；Development rate is fast, arrives setting and just can carry out operation with rapid deployment.
Accompanying drawing explanation
Fig. 1 is the right view that this utility model launches；
Fig. 2 is the right view that this utility model is packed up；
Fig. 3 is the overall structure figure that this utility model launches；
Fig. 4 is the overall structure figure that this utility model is packed up；
In reference: 1-aluminium alloy component I；2-aluminium alloy component II；3-aluminium alloy component III；4-aluminium alloy
Mechanism member IV；5. stainless steel shaft I；6-stainless steel shaft II；7-stainless steel shaft III；8-aluminium alloy is linked up with；9-unmanned plane horn.
Detailed description of the invention
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of this utility model rather than whole
Embodiment.Based on the embodiment in this utility model, those of ordinary skill in the art are not under making creative work premise
The all other embodiments obtained, broadly fall into the scope of this utility model protection.
Referring to Fig. 1, Fig. 2, Fig. 3, Fig. 4, this utility model provides a kind of technical scheme: one is applied to unmanned plane horn
On fold mechanism, including aluminium alloy component I, aluminium alloy component II, aluminium alloy component III, aluminium alloy component IV,
Stainless steel shaft I, stainless steel shaft II, stainless steel shaft III, aluminium alloy hook, unmanned plane horn；Aluminium alloy component I passes through rustless steel
Axle II is hinged with aluminium alloy component III；Aluminium alloy component II is movably hinged with aluminium alloy component I by stainless steel shaft I,
And its range of activity is 0 degree to 90 degree, it addition, aluminium alloy hook is fixed on the surface of aluminium alloy component II；Aluminium alloy mechanism
Part IV is movably hinged with aluminium alloy component III by stainless steel shaft III, and its range of activity is 0 degree to 180 degree；In edge,
Unmanned plane horn is installed in aluminium alloy component I and the two ends of aluminium alloy component II；Integrated base I and integrated base II
It is fixedly connected on aluminium alloy component I.
Of the present utility model when design: being configured with four aluminum alloy junction components, three stainless steel shafts, also an aluminum closes
Gold hook；Wherein the interface of aluminium alloy component I 1 and aluminium alloy component II 2 can attaching unmanned plane horn；When operation, draw
Dynamic aluminium alloy component IV 4, is closer to aluminium alloy component II 2, is buckled in aluminium alloy hook upper 8, wherein, aluminium alloy component
III 3 have must be elastic, before fastening, its angle be 86 degree 8 points 49 seconds, and its distance between axles is 17.8 centimetres, after fastening its
Angle be 87 degree 10 points 6 seconds, and its distance between axles is 18.1 centimetres, and it this is slightly distorted so that aluminium alloy component I 1
Firmly buckle with aluminium alloy component II 2, it is achieved wing expansion action；Otherwise, lift aluminium alloy component IV 4, can be light
Loose allows it separate with aluminium alloy hook 8, now, and the angle before aluminium alloy component III 3 reduction, it is achieved wing is packed up dynamic
Make.
Compared with prior art, the beneficial effects of the utility model are: this fold mechanism is the smallest and the most exquisite, arrange light spirit
Live, make the expansion of unmanned plane horn and pack up quick, it is not necessary to the help of instrument；When packing up, floor space is little, can make unmanned plane
Volume, convenient operation is reduced when packed and transported；Development rate is fast, arrives setting and just can carry out operation with rapid deployment.
Embodiment the most of the present utility model, for the ordinary skill in the art,
It is appreciated that in the case of without departing from principle of the present utility model and spirit and these embodiments can be carried out multiple change, repair
Changing, replace and modification, scope of the present utility model is defined by the appended claims and the equivalents thereof.
Claims (3)
1. it is applied to the fold mechanism on unmanned plane horn, including aluminium alloy component I (1), aluminium alloy component II
(2), aluminium alloy component III (3), aluminium alloy component IV (4), stainless steel shaft I (5), stainless steel shaft II (6), stainless steel shaft III
(7), aluminium alloy hook (8), unmanned plane horn (9), integrated base I (10), integrated base II (11)；Described unmanned plane machine
Arm (9) is installed in aluminium alloy component I (1) and the two ends of aluminium alloy component II (2)；It is characterized in that: described aluminium alloy
Component I (1) is hinged with aluminium alloy component III (3) by stainless steel shaft II (6)；Described aluminium alloy component II (2) is not by
Rust steel axle I (5) is movably hinged with aluminium alloy component I (1)；Described aluminium alloy component IV (4) by stainless steel shaft III (7) with
Aluminium alloy component III (3) is movably hinged；Described aluminium alloy hook (8) is fixed on aluminium alloy component II (2) surface；Described one
Body pedestal I (10) and integrated base II (11) are fixedly connected on aluminium alloy component I (1).
A kind of fold mechanism being applied on unmanned plane horn the most according to claim 1, it is characterised in that: described aluminum closes
JINJI component I (1) is movably hinged with aluminium alloy component II (2), and range of activity is between 0 degree to 90 degree.
A kind of fold mechanism being applied on unmanned plane horn the most according to claim 1, it is characterised in that: described aluminum closes
The draw angle scope of JINJI component III (3) at 86 degree 8 points between 49 seconds to 87 degree 10 points 6 seconds, the tensile elongation of its distance between axles
Scope is between 17.8 centimetres to 18.1 centimetres.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620556985.0U CN205661647U (en) | 2016-06-07 | 2016-06-07 | Be applied to folding mechanism on unmanned aerial vehicle horn |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620556985.0U CN205661647U (en) | 2016-06-07 | 2016-06-07 | Be applied to folding mechanism on unmanned aerial vehicle horn |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205661647U true CN205661647U (en) | 2016-10-26 |
Family
ID=57156931
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620556985.0U Expired - Fee Related CN205661647U (en) | 2016-06-07 | 2016-06-07 | Be applied to folding mechanism on unmanned aerial vehicle horn |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205661647U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107097931A (en) * | 2017-05-11 | 2017-08-29 | 珠海天晴航空航天科技有限公司 | A kind of unmanned plane horn folding device |
| CN107697265A (en) * | 2017-09-11 | 2018-02-16 | 珠海天晴航空航天科技有限公司 | A kind of fuselage wing attachment structure and locking device |
-
2016
- 2016-06-07 CN CN201620556985.0U patent/CN205661647U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107097931A (en) * | 2017-05-11 | 2017-08-29 | 珠海天晴航空航天科技有限公司 | A kind of unmanned plane horn folding device |
| CN107697265A (en) * | 2017-09-11 | 2018-02-16 | 珠海天晴航空航天科技有限公司 | A kind of fuselage wing attachment structure and locking device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20161026 Termination date: 20180607 |