GB533112A - Improvements in steering means for aircraft landing gear - Google Patents
Improvements in steering means for aircraft landing gearInfo
- Publication number
- GB533112A GB533112A GB2753539A GB2753539A GB533112A GB 533112 A GB533112 A GB 533112A GB 2753539 A GB2753539 A GB 2753539A GB 2753539 A GB2753539 A GB 2753539A GB 533112 A GB533112 A GB 533112A
- Authority
- GB
- United Kingdom
- Prior art keywords
- leg
- rotatable
- aircraft
- fixed
- steering
- 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)
- Vehicle Step Arrangements And Article Storage (AREA)
Abstract
533,112. Aircraft landing-gear. GENERAL AIRCRAFT, Ltd., and LEATHER, G. B. Oct. 9, 1939, No. 27535. [Class 4] A steerable alighting-gear for aircraft has a leg with one or more parts fixed against rotation about the leg axis, and one or more parts rotatable for steering, the steerable part being connected with the stationary part by control means partaking also of movements of the leg under landing and shock-absorbing loads. As shown in Fig. 1, the lower member 7 of a telescopic leg is rotatable in a fixed upper part 6 and carries a wheel 10, skid, endless track &c. capable of being steered. Tracking links 12, 13 are pivoted to the lower part of the leg and to a collar 11 which is rotatable on the fixed part 6 and has an arm 18 between which and arms 17 on the part 6 a double-acting jack 19 is pivoted. In the form shown in Fig. 4, the collar 11 has a forked part 24 for engagement by a lever 22 for steering the wheel-carrying part 26. The fixed part 28 has a pivot 27 about which the leg is swung for retraction. When the leg is retracted, the lever 22 becomes disengaged from the forked part 24.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2753539A GB533112A (en) | 1939-10-09 | 1939-10-09 | Improvements in steering means for aircraft landing gear |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2753539A GB533112A (en) | 1939-10-09 | 1939-10-09 | Improvements in steering means for aircraft landing gear |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB533112A true GB533112A (en) | 1941-02-06 |
Family
ID=10261161
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2753539A Expired GB533112A (en) | 1939-10-09 | 1939-10-09 | Improvements in steering means for aircraft landing gear |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB533112A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2624534A (en) * | 1948-01-26 | 1953-01-06 | Geisse John Harlin | Airplane cross-wind undercarriage |
| US2779556A (en) * | 1955-01-13 | 1957-01-29 | Cleveland Pneumatic Tool Co | Hydraulic steering mechanism for aircraft landing gear |
-
1939
- 1939-10-09 GB GB2753539A patent/GB533112A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2624534A (en) * | 1948-01-26 | 1953-01-06 | Geisse John Harlin | Airplane cross-wind undercarriage |
| US2779556A (en) * | 1955-01-13 | 1957-01-29 | Cleveland Pneumatic Tool Co | Hydraulic steering mechanism for aircraft landing gear |
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