GB562651A - Improvements in or relating to aircraft landing gear - Google Patents
Improvements in or relating to aircraft landing gearInfo
- Publication number
- GB562651A GB562651A GB1710442A GB1710442A GB562651A GB 562651 A GB562651 A GB 562651A GB 1710442 A GB1710442 A GB 1710442A GB 1710442 A GB1710442 A GB 1710442A GB 562651 A GB562651 A GB 562651A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wheel
- windstream
- aircraft
- wheels
- relating
- 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
- B64C25/40—Alighting gear characterised by elements which contact the ground or similar surface the elements being rotated before touch-down
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Tires In General (AREA)
Abstract
562,651. Aircraft landing wheels. CLARK, A. H. Dec. 1, 1942, No. 17104. [Class 4] [Also in Group XXXIV] Rotation of aircrafi landing wheels by the windstream, prior tc landing so as to reduce the wear on the tyres when the aircraft touches down, is effected by forming the tyres with cups 4 or with tapering projections. The upper part of the wheel may be shielded to prevent the windstream from acting on that part of the wheel. According to the Provisional Specification, hinged vanes may be fitted to the sides of the wheel so as to be opened by the windstream or by spring at the lower part of the wheel and closed at the upper part or the wheels may be rotated by electric, hydraulic or spring motors or by the engines of the aircraft.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1710442A GB562651A (en) | 1942-12-01 | 1942-12-01 | Improvements in or relating to aircraft landing gear |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1710442A GB562651A (en) | 1942-12-01 | 1942-12-01 | Improvements in or relating to aircraft landing gear |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB562651A true GB562651A (en) | 1944-07-11 |
Family
ID=10089322
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1710442A Expired GB562651A (en) | 1942-12-01 | 1942-12-01 | Improvements in or relating to aircraft landing gear |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB562651A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2193932A (en) * | 1986-08-14 | 1988-02-24 | Peter John Evans | Tyres for aircraft landing gear |
| GB2247659A (en) * | 1990-09-10 | 1992-03-11 | Gerard Ian Hamilton | Aircraft wheel with means to rotate it |
| US20160059955A1 (en) * | 2014-08-26 | 2016-03-03 | Daito Press Mfg. Co., Ltd. | Aircraft tire |
| US10597147B2 (en) | 2016-08-10 | 2020-03-24 | Daito Press Mfg. Co., Ltd. | Aircraft tire |
-
1942
- 1942-12-01 GB GB1710442A patent/GB562651A/en not_active Expired
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2193932A (en) * | 1986-08-14 | 1988-02-24 | Peter John Evans | Tyres for aircraft landing gear |
| GB2247659A (en) * | 1990-09-10 | 1992-03-11 | Gerard Ian Hamilton | Aircraft wheel with means to rotate it |
| US20160059955A1 (en) * | 2014-08-26 | 2016-03-03 | Daito Press Mfg. Co., Ltd. | Aircraft tire |
| US9731817B2 (en) * | 2014-08-26 | 2017-08-15 | Daito Press Mfg. Co., Ltd. | Aircraft tire |
| US10597147B2 (en) | 2016-08-10 | 2020-03-24 | Daito Press Mfg. Co., Ltd. | Aircraft tire |
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