GB448827A - Improvements in or relating to control surfaces for aircraft - Google Patents
Improvements in or relating to control surfaces for aircraftInfo
- Publication number
- GB448827A GB448827A GB35188/35A GB3518835A GB448827A GB 448827 A GB448827 A GB 448827A GB 35188/35 A GB35188/35 A GB 35188/35A GB 3518835 A GB3518835 A GB 3518835A GB 448827 A GB448827 A GB 448827A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- elevators
- relating
- control surfaces
- hellington
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Elevator Control (AREA)
Abstract
448,827. Controlling aircraft. McMAHON, A., 28, Hellington Street, Edinburgh. Dec. 19, 1935, No. 35188. [Class 4] Aircraft controls comprise a right circular conical member 3 carrying tail planes 1 and elevators 4 set at a transverse dihedral angle and rotatably connected to the rear of the fuselage by ball bearings 9. As shown, the elevators 4 are adjustable through known linkage, the member 3 is provided with a sleeve 14 having friction rollers 10 and stops are provided to limit its movement. The member 3 is rotated by cables 13.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB35188/35A GB448827A (en) | 1935-12-19 | 1935-12-19 | Improvements in or relating to control surfaces for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB35188/35A GB448827A (en) | 1935-12-19 | 1935-12-19 | Improvements in or relating to control surfaces for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB448827A true GB448827A (en) | 1936-06-16 |
Family
ID=10374867
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB35188/35A Expired GB448827A (en) | 1935-12-19 | 1935-12-19 | Improvements in or relating to control surfaces for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB448827A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2424889A (en) * | 1943-08-20 | 1947-07-29 | Tracy S Holmes | Airplane control system |
US2480040A (en) * | 1943-12-06 | 1949-08-23 | Wilbur A E Mitchell | Aircraft control surfaces |
US2500689A (en) * | 1945-02-05 | 1950-03-14 | Lockheed Aircraft Corp | Coupled control surface for aircraft |
-
1935
- 1935-12-19 GB GB35188/35A patent/GB448827A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2424889A (en) * | 1943-08-20 | 1947-07-29 | Tracy S Holmes | Airplane control system |
US2480040A (en) * | 1943-12-06 | 1949-08-23 | Wilbur A E Mitchell | Aircraft control surfaces |
US2500689A (en) * | 1945-02-05 | 1950-03-14 | Lockheed Aircraft Corp | Coupled control surface for aircraft |
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