GB519532A - Improvements relating to operating gear for aircraft controls - Google Patents
Improvements relating to operating gear for aircraft controlsInfo
- Publication number
- GB519532A GB519532A GB26731/38A GB2673138A GB519532A GB 519532 A GB519532 A GB 519532A GB 26731/38 A GB26731/38 A GB 26731/38A GB 2673138 A GB2673138 A GB 2673138A GB 519532 A GB519532 A GB 519532A
- Authority
- GB
- United Kingdom
- Prior art keywords
- improvements relating
- operating gear
- aircraft controls
- operated
- tubular members
- 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
- B64C13/24—Transmitting means
- B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
- B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
- B64C13/30—Transmitting means without power amplification or where power amplification is irrelevant mechanical using cable, chain, or rod mechanisms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/54—Varying in area
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Toys (AREA)
Abstract
519,532. Controlling aircraft. REID & SIGRIST, Ltd., and BOWER, C. Sept. 13, 1938, No. 26731. [Class 4] Control surfaces such as landing flaps and ailerons are mounted on tubular members by which they are operated and one of which passes through the other. As shown, the tubular members 16, 20 on which the landing flap and aileron are mounted, project into the fuselage and are provided with crank arms 18, 19 which are operated by screw and nut mechanism 33, 35 and by a link 25 both actuated from a distance. The members 16, 20 are carried by spaced bearings on the wing. The setting of the arm 18 is shown on an indicator 36.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB26731/38A GB519532A (en) | 1938-09-13 | 1938-09-13 | Improvements relating to operating gear for aircraft controls |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB26731/38A GB519532A (en) | 1938-09-13 | 1938-09-13 | Improvements relating to operating gear for aircraft controls |
Publications (1)
Publication Number | Publication Date |
---|---|
GB519532A true GB519532A (en) | 1940-03-29 |
Family
ID=10248346
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB26731/38A Expired GB519532A (en) | 1938-09-13 | 1938-09-13 | Improvements relating to operating gear for aircraft controls |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB519532A (en) |
-
1938
- 1938-09-13 GB GB26731/38A patent/GB519532A/en not_active Expired
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