GB509574A - Improvements relating to landing gear arrangements of aircraft - Google Patents
Improvements relating to landing gear arrangements of aircraftInfo
- Publication number
- GB509574A GB509574A GB3463338A GB3463338A GB509574A GB 509574 A GB509574 A GB 509574A GB 3463338 A GB3463338 A GB 3463338A GB 3463338 A GB3463338 A GB 3463338A GB 509574 A GB509574 A GB 509574A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- axle
- nose
- landing gear
- gear
- 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)
- Air Bags (AREA)
Abstract
509,574. Aircraft alighting - gear. GENERAL AIRCRAFT,. Ltd., WILLIAMS, D. L. H., and CROCOMBE, F. F. Nov. 28, 1938, No. 34633. [Class 4] In aircraft alighting-gear in which nose and main elements are situated respectively forwardly and rearwardly of the centre of gravity of the aircraft so that the tail of the aircraft is maintained normally clear of the ground, the nose element includes a pair of transversely spaced members supported on a single mounting permitting either or both castering and steering of the elements about an axis lying between the members. In one form, the nose landing gear comprises two wheels 15 supported on a common axle 16 mounted in a member 17 carried by the inner telescoping part 18 of a shock-absorber mounted in the aircraft structure by struts 23. The axle 16 trails behind the axis A, B of the shockabsorber. In a modification, the axle is mounted in a fork and the wheel spacing may be varied by changing a spacing member between the wheels. Specification .505,109 is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3463338A GB509574A (en) | 1938-11-28 | 1938-11-28 | Improvements relating to landing gear arrangements of aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3463338A GB509574A (en) | 1938-11-28 | 1938-11-28 | Improvements relating to landing gear arrangements of aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB509574A true GB509574A (en) | 1939-07-18 |
Family
ID=10368079
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3463338A Expired GB509574A (en) | 1938-11-28 | 1938-11-28 | Improvements relating to landing gear arrangements of aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB509574A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2421914A (en) * | 1942-06-08 | 1947-06-10 | Boeing Aircraft Co | Nose wheel |
US2538388A (en) * | 1949-08-02 | 1951-01-16 | Sievers George | Cross-wind landing gear for airplanes |
US2606726A (en) * | 1949-07-13 | 1952-08-12 | Henry M Henion | Aircraft landing gear construction |
-
1938
- 1938-11-28 GB GB3463338A patent/GB509574A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2421914A (en) * | 1942-06-08 | 1947-06-10 | Boeing Aircraft Co | Nose wheel |
US2606726A (en) * | 1949-07-13 | 1952-08-12 | Henry M Henion | Aircraft landing gear construction |
US2538388A (en) * | 1949-08-02 | 1951-01-16 | Sievers George | Cross-wind landing gear for airplanes |
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