GB535319A - An improvement in steering controls for use with retractable undercarriage landing wheels - Google Patents
An improvement in steering controls for use with retractable undercarriage landing wheelsInfo
- Publication number
- GB535319A GB535319A GB2937539A GB2937539A GB535319A GB 535319 A GB535319 A GB 535319A GB 2937539 A GB2937539 A GB 2937539A GB 2937539 A GB2937539 A GB 2937539A GB 535319 A GB535319 A GB 535319A
- Authority
- GB
- United Kingdom
- Prior art keywords
- link
- yoke
- improvement
- landing wheels
- trunnions
- 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
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/50—Steerable undercarriages; Shimmy-damping
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Steering-Linkage Mechanisms And Four-Wheel Steering (AREA)
Abstract
535,319. Aircraft landing carriages. O'NIONS, A. E. Nov. 4, 1939, No. 29375. [Class 4] A device for steering the landing wheels of retractable undercarriages which becomes operative without any additional manipulation by the pilot as the undercarriage is lowered comprises a link H movable by the usual rudder bar, the link being connected by a ball joint to a yoke A pivoted on trunnions, on the undercarriage leg, normally in the longitudinal plane of the aircraft. The leg is pivoted in a member E which can be turned about a transverse axis to raise the wheel out of use. During this movement the yoke A is turned into a vertical plane after which movements of the link H merely turn the yoke about it trunnions. The link H is guided by a bearing C so that the ball joint is maintained at a constant level to ensure the centring of the wheel as it is raised. The link H is connected as shown to the rudder-bar I.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2937539A GB535319A (en) | 1939-11-04 | 1939-11-04 | An improvement in steering controls for use with retractable undercarriage landing wheels |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2937539A GB535319A (en) | 1939-11-04 | 1939-11-04 | An improvement in steering controls for use with retractable undercarriage landing wheels |
Publications (1)
Publication Number | Publication Date |
---|---|
GB535319A true GB535319A (en) | 1941-04-04 |
Family
ID=10290546
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2937539A Expired GB535319A (en) | 1939-11-04 | 1939-11-04 | An improvement in steering controls for use with retractable undercarriage landing wheels |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB535319A (en) |
-
1939
- 1939-11-04 GB GB2937539A patent/GB535319A/en not_active Expired
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