CN206327561U - One kind folds unmanned plane wing shift-forward type development mechanism - Google Patents
One kind folds unmanned plane wing shift-forward type development mechanism Download PDFInfo
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- CN206327561U CN206327561U CN201621443579.XU CN201621443579U CN206327561U CN 206327561 U CN206327561 U CN 206327561U CN 201621443579 U CN201621443579 U CN 201621443579U CN 206327561 U CN206327561 U CN 206327561U
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- wing
- straight line
- mounting bracket
- unmanned plane
- actuating unit
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Abstract
Unmanned plane wing shift-forward type development mechanism is folded the utility model discloses one kind, including mounting bracket and straight line actuating unit, mobile main shaft is installed at the top of mounting bracket, two wing mounting seats are installed on mobile main shaft, trace pin is installed in two wing mounting seats, the position of mounting bracket correspondence trace pin is provided with track groove, straight line actuating unit runs through mounting bracket and its end is connected with mobile main shaft, this folding unmanned plane wing shift-forward type development mechanism, use a kind of straight line actuating unit, wing is set to complete two motions of straight line and rotation, and it is controllable in expansion and folding process, make unmanned plane during flying state steadily reliable, and actuating unit is totally independent of motion, folding and expanding can be carried out with a variety of power.
Description
Technical field
The utility model is related to unmanned air vehicle technique field, is specially a kind of folding unmanned plane wing shift-forward type development mechanism.
Background technology
Folding wings unmanned plane main advantage is small volume, saves space, easy to carry and transport, can effectively utilize nobody
Machine entire length meets wing span to greatest extent, and can use a variety of power set, while meeting folding and requiring
The pocket of unmanned plane is greatly improved, has the advantages that good mobility, good economy performance, adaptability are good, and lacks one at present
Plant the development mechanisms that wing can be made to complete two motions of straight line and rotation.
The content of the invention
The technical problems to be solved in the utility model is to overcome existing defect to fold the reach of unmanned plane wing there is provided one kind
Formula development mechanism, can make wing complete two motions of straight line and rotation, the problem of effectively can solving in background technology.
To achieve the above object, the utility model provides following technical scheme：One kind folds unmanned plane wing shift-forward type exhibition
It is provided with mobile main shaft, mobile main shaft and installs at the top of opening mechanism, including mounting bracket and straight line actuating unit, mounting bracket
Have and trace pin is installed in two wing mounting seats, two wing mounting seats, the position of mounting bracket correspondence trace pin is provided with rail
Mark groove, straight line actuating unit runs through mounting bracket and its end is connected with mobile main shaft.
Compared with prior art, the beneficial effects of the utility model are：This folding unmanned plane wing shift-forward type development mechanism,
Using a kind of straight line actuating unit, wing is set to complete two motions of straight line and rotation, and it is controllable in expansion and folding process, make
Unmanned plane during flying state is steadily reliable, and actuating unit is totally independent of motion, can be folded with a variety of power
Expansion.
Brief description of the drawings
Fig. 1 is the utility model structural representation.
In figure：1 mounting bracket, 2 movement main shafts, 3 track grooves, 4 trace pins, 5 straight line actuating units, 6 wing mounting seats.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of the utility model, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belongs to the scope of the utility model protection.
Referring to Fig. 1, the utility model provides a kind of technical scheme：One kind folds unmanned plane wing shift-forward type unwinder
Structure, including mounting bracket 1 and straight line actuating unit 5, actuating unit is totally independent of motion, can be carried out with a variety of power
Folding and expanding, the top of mounting bracket 1, which is provided with mobile main shaft 2, mobile main shaft 2, is provided with two wing mounting seats 6, passes through
Straight line actuating unit 5 promotes mobile main shaft 2, and mobile main shaft 2 drives wing mounting seat 6 to be moved along a straight line to the direction of motion, two
Trace pin 4 is installed, the position of the correspondence trace pin 4 of mounting bracket 1 is provided with track groove 3, straight line actuating unit in wing mounting seat 6
5 are connected through mounting bracket 1 and its end with moving main shaft 2, and the opposite side of wing mounting seat 6 is as trace pin 5 is in track groove 3
Turning effort is produced in motion, make wing mounting seat 6 linear motion while rotate, deploy wing, reach it is final nobody
The flight angle of machine and position.
When in use：Mobile main shaft 2 is promoted by straight line actuating unit 5, mobile main shaft 2 drives wing mounting seat 6 to fortune
Dynamic direction moves along a straight line, while the opposite side of wing mounting seat 6 is made as trace pin 5 produces rotation in the motion of track groove 3
With, make wing mounting seat 6 linear motion while rotate, deploy wing, reach flight angle and the position of final unmanned plane
Put.
The utility model uses a kind of straight line actuating unit, wing is completed two motions of straight line and rotation, and in exhibition
Open controllable with folding process, make unmanned plane during flying state steadily reliable, and actuating unit is totally independent of motion, can transport
Folding and expanding is carried out with a variety of power.
While there has been shown and described that embodiment of the present utility model, for the ordinary skill in the art,
It is appreciated that these embodiments can be carried out in the case where not departing from principle of the present utility model and spirit a variety of changes, repaiies
Change, replace and modification, scope of the present utility model is defined by the appended claims and the equivalents thereof.
Claims (1)
1. one kind folds unmanned plane wing shift-forward type development mechanism, including mounting bracket（1）With straight line actuating unit（5）, it is special
Levy and be：The mounting bracket（1）Top mobile main shaft is installed（2）, mobile main shaft（2）On the installation of two wings is installed
Seat（6）, two wing mounting seats（6）On trace pin is installed（4）, mounting bracket（1）Correspondence trace pin（4）Position be provided with rail
Mark groove（3）, the straight line actuating unit（5）Through mounting bracket（1）And its end and mobile main shaft（2）Connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621443579.XU CN206327561U (en) | 2016-12-27 | 2016-12-27 | One kind folds unmanned plane wing shift-forward type development mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621443579.XU CN206327561U (en) | 2016-12-27 | 2016-12-27 | One kind folds unmanned plane wing shift-forward type development mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206327561U true CN206327561U (en) | 2017-07-14 |
Family
ID=59293452
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621443579.XU Active CN206327561U (en) | 2016-12-27 | 2016-12-27 | One kind folds unmanned plane wing shift-forward type development mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206327561U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114216647A (en) * | 2021-12-16 | 2022-03-22 | 中国航天空气动力技术研究院 | Rudder wing transient unfolding and folding device for wind tunnel test |
-
2016
- 2016-12-27 CN CN201621443579.XU patent/CN206327561U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114216647A (en) * | 2021-12-16 | 2022-03-22 | 中国航天空气动力技术研究院 | Rudder wing transient unfolding and folding device for wind tunnel test |
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