CN2499336Y - Regualtion airplane wing controlled by cable - Google Patents
Regualtion airplane wing controlled by cable Download PDFInfo
- Publication number
- CN2499336Y CN2499336Y CN 01249361 CN01249361U CN2499336Y CN 2499336 Y CN2499336 Y CN 2499336Y CN 01249361 CN01249361 CN 01249361 CN 01249361 U CN01249361 U CN 01249361U CN 2499336 Y CN2499336 Y CN 2499336Y
- Authority
- CN
- China
- Prior art keywords
- cable
- wing
- controlled
- regualtion
- airplane wing
- 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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- Toys (AREA)
- Fluid-Pressure Circuits (AREA)
Abstract
A regulation airplane wing controlled by cable has the end provided with a tightwire-controlled element. The utility model has a simple structure, reliability and light weight and is suitable for miniature aircraft.
Description
The utility model belongs to the wing of aircraft.
At present the wing of aircraft is regulated and is generally adopted electronic, the pneumatic or hydraulic actuator of electron steering, though degree of automation height, precise control, the actuating unit relative complex has increased the possible origination point that lost efficacy, and has also increased the weight of aircraft.
The purpose of this utility model provides a kind of adjusting wing simple in structure, reliable, lightweight.
All there is the point of connection of controlling cable wire the aerofoil both sides that cable-controlled is regulated wing, and point of connection connects the control cable wire.The aerofoil of straining, regulate when the below cable wire loosens wing when the top cable wire upwarps, otherwise the square steel rope is strained instantly, the aerofoil of adjusting wing pressed down when the top cable wire loosened, and the stressed effect of adjusting wing is played in the wing surface angle variation.
Owing to cable wire control is the simplest Machinery Control System, wing structure is simple, and system is reliable to the point of connection that only needs the two sides, and it is convenient to make, keep in repair, check; After having omitted complex control system, the weight of wing control system has also alleviated.
The advantage that cable-controlled is regulated wing is:
1, simple in structure, reliable, it is convenient to make, keep in repair, check.
2, can alleviate the weight of wing control system.
Accompanying drawing 1 is regulated the unadjusted cutaway view of wing for cable-controlled, and 1 is cable wire among the figure, and 2 is fixed wing, and 3 for regulating wing, and 4 is pulley, and 5 are rotating shaft, and 6 is the point of connection of cable wire.
Accompanying drawing 2 is regulated cutaway view after wing is regulated for cable-controlled.
In sum, cable-controlled is regulated the common adjusting machine that wing can substitute aircraft The wing is particularly suitable for small aircraft.
Claims (1)
1, a kind of adjusting wing is characterized in that all there is the point of connection of control cable wire the aerofoil both sides.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 01249361 CN2499336Y (en) | 2001-07-30 | 2001-07-30 | Regualtion airplane wing controlled by cable |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 01249361 CN2499336Y (en) | 2001-07-30 | 2001-07-30 | Regualtion airplane wing controlled by cable |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2499336Y true CN2499336Y (en) | 2002-07-10 |
Family
ID=33659782
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 01249361 Expired - Fee Related CN2499336Y (en) | 2001-07-30 | 2001-07-30 | Regualtion airplane wing controlled by cable |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2499336Y (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101857084A (en) * | 2010-06-10 | 2010-10-13 | 西北工业大学 | Transmission mechanism of telescopic morphing wing |
| CN103847954A (en) * | 2014-01-29 | 2014-06-11 | 江村 | Telescopic wing |
-
2001
- 2001-07-30 CN CN 01249361 patent/CN2499336Y/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101857084A (en) * | 2010-06-10 | 2010-10-13 | 西北工业大学 | Transmission mechanism of telescopic morphing wing |
| CN103847954A (en) * | 2014-01-29 | 2014-06-11 | 江村 | Telescopic wing |
| CN103847954B (en) * | 2014-01-29 | 2015-10-07 | 江村 | Telescopic wing |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |