CN205770107U - Unmanned plane horn quick-disassembly structure - Google Patents
Unmanned plane horn quick-disassembly structure Download PDFInfo
- Publication number
- CN205770107U CN205770107U CN201620466223.1U CN201620466223U CN205770107U CN 205770107 U CN205770107 U CN 205770107U CN 201620466223 U CN201620466223 U CN 201620466223U CN 205770107 U CN205770107 U CN 205770107U
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- CN
- China
- Prior art keywords
- connector
- unmanned plane
- disassembly structure
- postbrachium
- quick
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Abstract
The utility model discloses a kind of unmanned plane horn quick-disassembly structure, for the connection of unmanned plane horn, including the forearm connector cooperated and postbrachium connector；Two sides of described forearm connector are respectively symmetrically and are provided with a buckle that can rotate in forearm connector side, and the lower end of described buckle extends inwardly to form a halfpace；Two sides of described postbrachium connector are all fixed with a step, described in snap through rotation can make described halfpace carry described step.The utility model discloses a kind of unmanned plane horn quick-disassembly structure, it is possible to make the dismounting of horn and lock convenient, improve dismounting efficiency.
Description
Technical field
This utility model is specifically related to a kind of unmanned plane horn quick-disassembly structure.
Background technology
Professional many rotor wing unmanned aerial vehicles horn the most mostly use folding mode to be convenient for carrying, the fewest
Number takes the mode of quick-disassembly structure.Existing horn quick-disassembly structure is to process guide pillar guide pin bushing in the left and right sides
Coming spacing, in the mode that upper and lower both sides screw down, this mode not only needs to tighten multiple screw
Pretty troublesome, and owing to guide pillar guide pin bushing coordinates offset issue to make horn meeting double swerve, impact flight
Performance.
Utility model content
For existing issue, the utility model discloses a kind of unmanned plane horn quick-disassembly structure, it is possible to make
The dismounting of horn and lock convenient, improves dismounting efficiency.
The technical solution of the utility model is as follows:
A kind of unmanned plane horn quick-disassembly structure, for the connection of unmanned plane horn, including cooperate
Forearm connector and postbrachium connector；Two sides of described forearm connector be respectively symmetrically be provided with one can
The buckle rotated in forearm connector side, the lower end of described buckle extends inwardly to form a halfpace；Institute
Two sides stating postbrachium connector are all fixed with a step, described in snap through rotation and can make institute
State halfpace and carry described step.
Preferably, described forearm connector is consistent with the cross sectional shape that postbrachium connects, and described forearm is even
The surface of the postbrachium connector of fitting is equipped with an installation screw.
Preferably, the lower surface of described step is a cambered surface.
The utility model discloses a kind of unmanned plane horn quick-disassembly structure, it is possible to make dismounting and the lock of horn
The most convenient, improve dismounting efficiency.
Accompanying drawing explanation
In order to be illustrated more clearly that the technical scheme in this utility model embodiment, below will be to embodiment
In description, the required accompanying drawing used is briefly described.
Fig. 1 is the structure chart at the first visual angle of unmanned plane horn quick-disassembly structure provided by the utility model；
Fig. 2 is the structure chart at the second visual angle of unmanned plane horn quick-disassembly structure provided by the utility model.
In figure, numeral represents:
1, forearm connector 2, postbrachium connector 3, buckle 4, halfpace 5, step 6, screw.
Detailed description of the invention
Below in conjunction with the accompanying drawing in this utility model embodiment, to the skill in this utility model embodiment
Art scheme is clearly and completely described.
Fig. 1 is to shown in 2, and a kind of unmanned plane horn quick-disassembly structure, for the connection of unmanned plane horn, nothing
Man-machine horn is incident upon in forearm connector 1 and postbrachium connector 2, the two of described forearm connector 1
Individual side is respectively symmetrically and is provided with a buckle 3 that can rotate in forearm connector 1 side, described buckle 3
Lower end extend inwardly to form a halfpace 4；Two sides of described postbrachium connector 2 are all fixed with
One step 5, described buckle 3 can make described halfpace 4 carry described step 5 by rotation.
The cross sectional shape that described forearm connector 1 connects with postbrachium is consistent, and described forearm connector 1
The surface of postbrachium connector 2 be equipped with an installation screw 6.
The lower surface of described step 5 is a cambered surface；When buckle 3 rotates, halfpace 4 contacts step 5
Time, because there being the setting of cambered surface, so can fix more along with the big gradually clamping of the change of spinning force
Firmly.
The utility model discloses a kind of unmanned plane horn quick-disassembly structure, it is possible to make dismounting and the lock of horn
The most convenient, improve dismounting efficiency.
Multiple amendment to these embodiments will be apparent for those skilled in the art
, generic principles defined herein can be in the feelings without departing from spirit or scope of the present utility model
Under condition, realize in other embodiments.
Claims (3)
1. a unmanned plane horn quick-disassembly structure, for the connection of unmanned plane horn, it is characterised in that
Including the forearm connector cooperated and postbrachium connector；Two sides of described forearm connector are divided
Not being arranged with a buckle that can rotate in forearm connector side, the lower end of described buckle extends internally
Form a halfpace；Two sides of described postbrachium connector are all fixed with a step, and described buckle leads to
Crossing rotation can make described halfpace carry described step.
Quick-disassembly structure the most according to claim 1, it is characterised in that described forearm connector and
The cross sectional shape that postbrachium connects is consistent, and the surface of the postbrachium connector of described forearm connector is equipped with
One installation screw.
Quick-disassembly structure the most according to claim 1, it is characterised in that the lower surface of described step
It it is a cambered surface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620466223.1U CN205770107U (en) | 2016-05-19 | 2016-05-19 | Unmanned plane horn quick-disassembly structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620466223.1U CN205770107U (en) | 2016-05-19 | 2016-05-19 | Unmanned plane horn quick-disassembly structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205770107U true CN205770107U (en) | 2016-12-07 |
Family
ID=58116844
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620466223.1U Expired - Fee Related CN205770107U (en) | 2016-05-19 | 2016-05-19 | Unmanned plane horn quick-disassembly structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205770107U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105857565A (en) * | 2016-05-19 | 2016-08-17 | 安翔泰岳（镇江）航空科技有限公司 | Quick detachment structure for unmanned aerial vehicle arms |
-
2016
- 2016-05-19 CN CN201620466223.1U patent/CN205770107U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105857565A (en) * | 2016-05-19 | 2016-08-17 | 安翔泰岳（镇江）航空科技有限公司 | Quick detachment structure for unmanned aerial vehicle arms |
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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 |
Granted publication date: 20161207 Termination date: 20190519 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |