GB417487A - Improvements in or relating to the control surfaces of aircraft - Google Patents
Improvements in or relating to the control surfaces of aircraftInfo
- Publication number
- GB417487A GB417487A GB3212733A GB3212733A GB417487A GB 417487 A GB417487 A GB 417487A GB 3212733 A GB3212733 A GB 3212733A GB 3212733 A GB3212733 A GB 3212733A GB 417487 A GB417487 A GB 417487A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aileron
- camber
- cable
- depressed
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/44—Varying camber
- B64C3/50—Varying camber by leading or trailing edge flaps
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
417,487. Aeroplane controls. FAIREY AVIATION CO., Ltd., Cranford Lane, Hayes, Middlesex, and BROWN, A. C., 109, Cleveland Road, Ealing, London. Nov. 17, 1933, No. 32127. [Class 4.] In order to maintain the hinge moments of a combined pair of aircraft ailerons as low as possible each aileron is constructed so that when it is depressed to increase the camber of the wing its own camber is simultaneously increased. As shown this is effected by making the aileron in two parts a, b hinged together at e, the leading portion a being adapted to be depressed whenever the aileron as a whole is depressed about the hinges c at the rear ends of brackets d. The dipping of the portion a is effected by a link t connected to a non-rotatable nut r working on a threaded rod k, at the upper end of which is a pulley m actuated by a cable n that passes into the wing structure at a point in line with the axis c. A cable o which serves to vary the camber of the wing is associated with the cable n through a gearing-up pulley p, q.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3212733A GB417487A (en) | 1933-11-17 | 1933-11-17 | Improvements in or relating to the control surfaces of aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3212733A GB417487A (en) | 1933-11-17 | 1933-11-17 | Improvements in or relating to the control surfaces of aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB417487A true GB417487A (en) | 1934-10-05 |
Family
ID=10333686
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB3212733A Expired GB417487A (en) | 1933-11-17 | 1933-11-17 | Improvements in or relating to the control surfaces of aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB417487A (en) |
-
1933
- 1933-11-17 GB GB3212733A patent/GB417487A/en not_active Expired
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