GB417161A - Improvements in or relating to means for controlling aircraft - Google Patents
Improvements in or relating to means for controlling aircraftInfo
- Publication number
- GB417161A GB417161A GB3221833A GB3221833A GB417161A GB 417161 A GB417161 A GB 417161A GB 3221833 A GB3221833 A GB 3221833A GB 3221833 A GB3221833 A GB 3221833A GB 417161 A GB417161 A GB 417161A
- Authority
- GB
- United Kingdom
- Prior art keywords
- lever
- link
- flap
- pivoted
- actuated
- 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
- B64C9/10—Adjustable control surfaces or members, e.g. rudders one surface adjusted by movement of another, e.g. servo tabs
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
Abstract
417,161. Controlling aircraft. FAIREY AVIATION CO., Ltd., Cranford Lane, Hayes, and WILLIAMS, D. L. H., Hillside, Swakeley's Road, Ickenham, both in Middlesex. Nov. 18, 1933, No. 32218. [Class 4.] Control means for aircraft include a servo. flap e actuated by a link and lever system which includes a lever jh pivoted on a member d rigidly secured to a main control surface a so that a load applied to the lever jh is also applied to the surface a. As shown, the short arm h of the lever is actuated through a link m and the flap e pivoted to the elevator is operated by the long arm j of the lever through a link n, one end of which is connected in one of a number of holes o in the lever to facilitate adjustment.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3221833A GB417161A (en) | 1933-11-18 | 1933-11-18 | Improvements in or relating to means for controlling aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3221833A GB417161A (en) | 1933-11-18 | 1933-11-18 | Improvements in or relating to means for controlling aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB417161A true GB417161A (en) | 1934-09-28 |
Family
ID=10335142
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3221833A Expired GB417161A (en) | 1933-11-18 | 1933-11-18 | Improvements in or relating to means for controlling aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB417161A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2961986A (en) * | 1955-04-19 | 1960-11-29 | William H Rochill | Steering control for outboard motors |
-
1933
- 1933-11-18 GB GB3221833A patent/GB417161A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2961986A (en) * | 1955-04-19 | 1960-11-29 | William H Rochill | Steering control for outboard motors |
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