CN205022848U - Wing speed reduction baffle controlling means - Google Patents
Wing speed reduction baffle controlling means Download PDFInfo
- Publication number
- CN205022848U CN205022848U CN201520778548.9U CN201520778548U CN205022848U CN 205022848 U CN205022848 U CN 205022848U CN 201520778548 U CN201520778548 U CN 201520778548U CN 205022848 U CN205022848 U CN 205022848U
- Authority
- CN
- China
- Prior art keywords
- wing
- baffle
- speed reduction
- baffle plate
- controlling means
- 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 belongs to the technical field of wing baffle operation technique and specifically relates to a wing speed reduction baffle controlling means. A wing speed reduction baffle controlling means, includes wing and baffle, the baffle is fixed on the wing through the pivot activity, be equipped with the tractive motor in the wing, be equipped with the pull rod on the tractive motor, the pull rod is connected with the connecting rod, the connecting rod passes through back shaft swing joint with the baffle, the pull rod passes through connecting axle swing joint with the connecting rod, be equipped with the slide rail in the wing, the connecting axle is installed in the slide rail. This kind of wing speed reduction baffle controlling means when using, can be quick open the baffle, the device simple structure simultaneously, job stabilization, low in manufacturing cost satisfies the user demand.
Description
Technical field
The utility model relates to wing baffle plate operative technique field, especially a kind of wing decelerating barrier control setup.
Background technology
Aircraft, when landing, in order to accelerate slowing effect, all can increase baffle plate on wing, and opening baffle plate when landing increases windage, improves slowing effect, but current baffle plate Unclosing structure is complicated, and productive costs is high.
Utility model content
In order to overcome existing baffle plate device for spreading complex structure, the deficiency that cost is high, the utility model provides a kind of wing decelerating barrier control setup.
The utility model solves the technical scheme that its technical matters adopts: a kind of wing decelerating barrier control setup, comprise wing and baffle plate, described baffle plate is movably fixed on wing by rotating shaft, tractive motor is provided with in described wing, described tractive motor is provided with pull bar, described pull bar is connected with pipe link, and described pipe link is flexibly connected by pivot shaft with baffle plate, and described pull bar is flexibly connected by adapter shaft with pipe link.
According to another embodiment of the present utility model, comprise further, be provided with slide rail in described wing, described adapter shaft is arranged in slide rail.
The beneficial effects of the utility model are, this wing decelerating barrier control setup when in use, can open baffle plate by fast speed, and this apparatus structure is simple simultaneously, and working stability, low cost of manufacture, meets user demand.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the utility model is further illustrated.
Fig. 1 is structural representation of the present utility model;
Fig. 2 is using state figure of the present utility model;
In figure 1, wing, 2, tractive motor, 3, pull bar, 4, rotating shaft, 5, baffle plate, 6, pipe link, 7, adapter shaft, 8, pivot shaft, 9, slide rail.
Detailed description of the invention
If Fig. 1 is structural representation of the present utility model, a kind of wing decelerating barrier control setup, comprise wing 1 and baffle plate 5, described baffle plate 5 is movably fixed on wing 1 by rotating shaft 4, be provided with tractive motor 2 in described wing 1, described tractive motor 2 is provided with pull bar 3, and described pull bar 3 is connected with pipe link 6, described pipe link 6 is flexibly connected by pivot shaft 8 with baffle plate 5, and described pull bar 3 is flexibly connected by adapter shaft 7 with pipe link 6.
According to another embodiment of the present utility model, comprise further, be provided with slide rail 9 in described wing 1, described adapter shaft 7 is arranged in slide rail 9.
This wing decelerating barrier control setup when in use, when needing baffle plate 5 to rise, start tractive motor 2 pull bar 3 is inwardly drawn, make to be flexibly connected pipe link 6 with pull bar 3 under track 9 and baffle plate 5 are connected the effect in joint, baffle plate 5 is risen, baffle plate 5, between pull bar 3 and pipe link 6, form triangle, leg-of-mutton structure is the most stable in geometric figure, improve the stability of baffle plate 5, this apparatus structure is simple, meets user demand.
Claims (2)
1. a wing decelerating barrier control setup, comprise wing (1) and baffle plate (5), described baffle plate (5) is movably fixed on wing (1) by rotating shaft (4), it is characterized in that, tractive motor (2) is provided with in described wing (1), described tractive motor (2) is provided with pull bar (3), described pull bar (3) is connected with pipe link (6), described pipe link (6) is flexibly connected by pivot shaft (8) with baffle plate (5), and described pull bar (3) is flexibly connected by adapter shaft (7) with pipe link (6).
2. wing decelerating barrier control setup according to claim 1, is characterized in that, is provided with slide rail (9) in described wing (1), and described adapter shaft (7) is arranged in slide rail (9).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520778548.9U CN205022848U (en) | 2015-10-10 | 2015-10-10 | Wing speed reduction baffle controlling means |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520778548.9U CN205022848U (en) | 2015-10-10 | 2015-10-10 | Wing speed reduction baffle controlling means |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205022848U true CN205022848U (en) | 2016-02-10 |
Family
ID=55255407
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520778548.9U Expired - Fee Related CN205022848U (en) | 2015-10-10 | 2015-10-10 | Wing speed reduction baffle controlling means |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205022848U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106240802A (en) * | 2016-07-20 | 2016-12-21 | 天津津宇凯创航空科技发展有限公司 | A kind of wing aerodynamic deceleration mechanism |
| CN109606399A (en) * | 2019-01-10 | 2019-04-12 | 宝鸡文理学院 | A kind of Reduction gear for rail transit |
| CN109866915A (en) * | 2019-02-02 | 2019-06-11 | 东北农业大学 | Unmanned autogyro brake gear |
| CN111017191A (en) * | 2019-12-19 | 2020-04-17 | 中国航空工业集团公司西安飞机设计研究所 | Winglet |
-
2015
- 2015-10-10 CN CN201520778548.9U patent/CN205022848U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106240802A (en) * | 2016-07-20 | 2016-12-21 | 天津津宇凯创航空科技发展有限公司 | A kind of wing aerodynamic deceleration mechanism |
| CN109606399A (en) * | 2019-01-10 | 2019-04-12 | 宝鸡文理学院 | A kind of Reduction gear for rail transit |
| CN109606399B (en) * | 2019-01-10 | 2020-07-07 | 宝鸡文理学院 | Speed reduction device for rail transit |
| CN109866915A (en) * | 2019-02-02 | 2019-06-11 | 东北农业大学 | Unmanned autogyro brake gear |
| CN111017191A (en) * | 2019-12-19 | 2020-04-17 | 中国航空工业集团公司西安飞机设计研究所 | Winglet |
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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: 20160210 Termination date: 20161010 |