GB792360A - Improvements relating to aircraft - Google Patents
Improvements relating to aircraftInfo
- Publication number
- GB792360A GB792360A GB176154A GB176154A GB792360A GB 792360 A GB792360 A GB 792360A GB 176154 A GB176154 A GB 176154A GB 176154 A GB176154 A GB 176154A GB 792360 A GB792360 A GB 792360A
- Authority
- GB
- United Kingdom
- Prior art keywords
- booster
- control
- fulcrum
- flap
- lever
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/32—Air braking surfaces
- B64C9/326—Air braking surfaces associated with fuselages
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/32—Air braking surfaces
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
- Mechanical Control Devices (AREA)
Abstract
792,360. Controlling aircraft. FAIREY AVIATION CO., Ltd. April 20, 1955 [April 20, 1955], No. 1761/54. Class 4. Movement of airbrake flaps 15 produces compensating adjustment of control surfaces 1. The surface 1 is normally displaced by a manually operated link 9, lever 7, link 8 and a hydrobooster 2. Through a second hydro-booster 13, actuation of the flap 15 by a manual control 16 produces movement of the fulcrum 6 of the lever 7, thereby modifying the control that this lever effects on the surface 1. Fig. 2 (not shown) illustrates the use of the second booster 13 to actuate the flap 15 and to move the fulcrum 6, whilst Fig. 3 (not shown) illustrates the coupling of the manual controls of surfaces 1 and 15 so that only one booster is employed. Where the control surface 1 is remote from the flap 15, Fig. 4, potentiometers 31, 35 may be arranged to provide a signal controlling the booster 13 and thus moving the fulcrum 6. Hydraulic pneumatic or electrical means may be employed in place of the mechanical linkage arranged to compound the movements of surfaces 1 and 15. The servomotors may be electrical.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB176154A GB792360A (en) | 1954-01-20 | 1954-01-20 | Improvements relating to aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB176154A GB792360A (en) | 1954-01-20 | 1954-01-20 | Improvements relating to aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB792360A true GB792360A (en) | 1958-03-26 |
Family
ID=9727519
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB176154A Expired GB792360A (en) | 1954-01-20 | 1954-01-20 | Improvements relating to aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB792360A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3396597A (en) * | 1966-01-17 | 1968-08-13 | United Aircraft Corp | Flight control linkage for aircraft |
| CN109367763A (en) * | 2018-12-12 | 2019-02-22 | 湖南山河科技股份有限公司 | A kind of mechanical side lever operating mechanism |
-
1954
- 1954-01-20 GB GB176154A patent/GB792360A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3396597A (en) * | 1966-01-17 | 1968-08-13 | United Aircraft Corp | Flight control linkage for aircraft |
| CN109367763A (en) * | 2018-12-12 | 2019-02-22 | 湖南山河科技股份有限公司 | A kind of mechanical side lever operating mechanism |
| CN109367763B (en) * | 2018-12-12 | 2024-06-11 | 山河星航实业股份有限公司 | Mechanical side lever operating mechanism |
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