GB351061A - Improvements in or relating to control surfaces for aircraft - Google Patents
Improvements in or relating to control surfaces for aircraftInfo
- Publication number
- GB351061A GB351061A GB9150/30A GB915030A GB351061A GB 351061 A GB351061 A GB 351061A GB 9150/30 A GB9150/30 A GB 9150/30A GB 915030 A GB915030 A GB 915030A GB 351061 A GB351061 A GB 351061A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aileron
- wing
- pivoted
- ailerons
- effected
- 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
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
351,061. Aeroplane controls. FAIREY AVIATION CO., Ltd., Cranford Lane, Hayes, Middlesex, and LOBELLE, M. J. O., Studio B, Anhalt Road, Battersea, London. March 21,1930, No. 9150. [Class 4.] In aeroplanes employing ailerons of the type described in Specification 194,753, means are provided for moving the pivotal axes of the ailerons transversely of the general plane of the wing. An aileron b is shown pivoted at a to one arm c of a two-armed lever c, d pivoted at e to the lower edge of the trailing end of a wing f. Normal operation of the aileron is effected by the rod and lever mechanism k, m, o and movement of the aileron axis is effected by camber control gear operating a leading screw h passing through a nut g pivoted to the arm d. The arrangement is such that in no circumstances can use of the camber control gear cause the leading edge of the aileron b to project above the upper surface of the wing f.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB9150/30A GB351061A (en) | 1930-03-21 | 1930-03-21 | Improvements in or relating to control surfaces for aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB9150/30A GB351061A (en) | 1930-03-21 | 1930-03-21 | Improvements in or relating to control surfaces for aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB351061A true GB351061A (en) | 1931-06-22 |
Family
ID=9866347
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB9150/30A Expired GB351061A (en) | 1930-03-21 | 1930-03-21 | Improvements in or relating to control surfaces for aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB351061A (en) |
-
1930
- 1930-03-21 GB GB9150/30A patent/GB351061A/en not_active Expired
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