GB286313A - Improvements in or relating to aeroplane landing gear - Google Patents
Improvements in or relating to aeroplane landing gearInfo
- Publication number
- GB286313A GB286313A GB6712/28A GB671228A GB286313A GB 286313 A GB286313 A GB 286313A GB 6712/28 A GB6712/28 A GB 6712/28A GB 671228 A GB671228 A GB 671228A GB 286313 A GB286313 A GB 286313A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blocks
- secured
- section member
- aeroplane
- pilot
- 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
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
Abstract
286,313. Curtiss Aeroplane & Motor Co., Inc., (Assignees of Beisel, R. B.). March 4, 1927, [Convention date]. Blocks acting on drums; fluid-pressure. - An aeroplane landing gear has disc wheels with offset rims which enclose expanding block brakes applied by hydraulic pressure controlled from the pilot's seat. The under-carriage struts are secured to a member 35 having parallel cheeks 36 supporting blocks 37 which slide under the restraint of oleo and rubber disc shock absorbers in channel members 32 secured to the side plates 29 of an H- section member having a bearing 26 for the wheel spindle 18. Brake blocks 65 pivoted at 66 to a fitting at the lower end of the central H-section member act upon the cylindrical part 16 of the wheel rim when their upper ends are urged apart by two plungers 64 in a cylinder 63 supplied with fluid from a cylinder near the pilot's seat. The blocks are guided by projections 71 on brackets 57 secured to the H-section member and are held off by springs 70.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US286313XA | 1927-03-04 | 1927-03-04 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB286313A true GB286313A (en) | 1928-11-01 |
Family
ID=21844556
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB6712/28A Expired GB286313A (en) | 1927-03-04 | 1928-03-03 | Improvements in or relating to aeroplane landing gear |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB286313A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2423687A1 (en) * | 1978-04-17 | 1979-11-16 | Krupp Ag Huettenwerke | RAILWAY WHEEL EQUIPPED WITH RESONANCE ABSORBERS |
US8714473B2 (en) | 2003-04-07 | 2014-05-06 | Airbus Uk Limited | Landing gear |
US8882043B2 (en) | 2003-04-07 | 2014-11-11 | Airbus Uk Limited | Landing gear assembly |
-
1928
- 1928-03-03 GB GB6712/28A patent/GB286313A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2423687A1 (en) * | 1978-04-17 | 1979-11-16 | Krupp Ag Huettenwerke | RAILWAY WHEEL EQUIPPED WITH RESONANCE ABSORBERS |
US8714473B2 (en) | 2003-04-07 | 2014-05-06 | Airbus Uk Limited | Landing gear |
US8746615B2 (en) | 2003-04-07 | 2014-06-10 | Airbus Operations Limited | Landing gear |
US8882043B2 (en) | 2003-04-07 | 2014-11-11 | Airbus Uk Limited | Landing gear assembly |
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