CN205022850U - Aircraft auxiliary engine wing slider - Google Patents
Aircraft auxiliary engine wing slider Download PDFInfo
- Publication number
- CN205022850U CN205022850U CN201520778390.5U CN201520778390U CN205022850U CN 205022850 U CN205022850 U CN 205022850U CN 201520778390 U CN201520778390 U CN 201520778390U CN 205022850 U CN205022850 U CN 205022850U
- Authority
- CN
- China
- Prior art keywords
- wing
- auxiliary engine
- aircraft
- slave
- slider
- 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 controlling means technique and specifically relates to an aircraft auxiliary engine wing slider. An aircraft auxiliary engine wing slider, includes the host computer wing, be equipped with driving motor in the host computer wing, driving motor connects the drive wheel, the drive wheel with be connected by the drive belt from the driving wheel between, the drive belt below is equipped with the auxiliary engine wing, be connected by the fixed block between the auxiliary engine wing and the drive belt, be equipped with the pulley between the auxiliary engine wing and the host computer wing. This kind of aircraft auxiliary engine wing slider is when using, and completion that can be quick is to the adjustment of the auxiliary engine wing to controller construction is simple, satisfies the user demand.
Description
Technical field
The utility model relates to wing control setup technical field, especially a kind of aircraft slave wing carriage.
Background technology
In the process of airplane operation, need between host wing and the slave wing with the use of, but the current operation slave wing, when operation, operating unit is comparatively complicated, takes up an area comparatively large, can not meet operational requirements.
Utility model content
In order to overcome the deficiency of existing slave wing operating unit complexity, the utility model provides a kind of aircraft slave wing carriage.
The utility model solves the technical scheme that its technical matters adopts: a kind of aircraft slave wing carriage, comprise host wing, drive motor is provided with in described host wing, described drive motor connects drive wheel, described drive wheel is connected by driving band with between flower wheel, be provided with the slave wing below described driving band, the described slave wing is connected by fixed block with between driving band.
According to another embodiment of the present utility model, comprise further, between the described slave wing and host wing, be provided with pulley.
The beneficial effects of the utility model are, this aircraft slave wing carriage when in use, can complete adjustment to the slave wing by fast speed, and control setup structure is simple, 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;
In figure 1, host wing, 2, the slave wing, 3, drive motor, 4, drive wheel, 5, flower wheel, 6, driving band, 7, fixed block, 8, pulley.
Detailed description of the invention
If Fig. 1 is structural representation of the present utility model, a kind of aircraft slave wing carriage, comprise host wing 1, drive motor 3 is provided with in described host wing 1, described drive motor 3 connects drive wheel 4, described drive wheel 4 is connected by driving band 6 with between flower wheel 5, is provided with the slave wing 2 below described driving band 6, and the described slave wing 2 is connected by fixed block 7 with between driving band 6.
According to another embodiment of the present utility model, comprise further, between the described slave wing 2 and host wing 1, be provided with pulley 8.
This aircraft slave wing carriage when in use, when needing to operate the slave wing 2, starting drive motor 3 drives drive wheel 4 to run, under the effect of drive wheel 4, flower wheel 5 and driving band 6, drive the slave wing 2 fixing with driving band 6 to move forward and backward, pulley 8 between the slave wing 2 and host wing 1 facilitates the slave wing 2 to move, whole apparatus structure is simple, and simple operation, meets user demand.
Claims (2)
1. an aircraft slave wing carriage, comprise host wing (1), it is characterized in that, drive motor (3) is provided with in described host wing (1), described drive motor (3) connects drive wheel (4), be connected by driving band (6) between described drive wheel (4) with flower wheel (5), described driving band (6) below is provided with the slave wing (2), and the described slave wing (2) is connected by fixed block (7) with between driving band (6).
2. aircraft slave wing carriage according to claim 1, is characterized in that, is provided with pulley (8) between the described slave wing (2) and host wing (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520778390.5U CN205022850U (en) | 2015-10-10 | 2015-10-10 | Aircraft auxiliary engine wing slider |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520778390.5U CN205022850U (en) | 2015-10-10 | 2015-10-10 | Aircraft auxiliary engine wing slider |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205022850U true CN205022850U (en) | 2016-02-10 |
Family
ID=55255409
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520778390.5U Expired - Fee Related CN205022850U (en) | 2015-10-10 | 2015-10-10 | Aircraft auxiliary engine wing slider |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205022850U (en) |
-
2015
- 2015-10-10 CN CN201520778390.5U patent/CN205022850U/en not_active Expired - Fee Related
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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 |