GB518414A - Improvements in retractable landing gear for aircraft - Google Patents
Improvements in retractable landing gear for aircraftInfo
- Publication number
- GB518414A GB518414A GB24880/38A GB2488038A GB518414A GB 518414 A GB518414 A GB 518414A GB 24880/38 A GB24880/38 A GB 24880/38A GB 2488038 A GB2488038 A GB 2488038A GB 518414 A GB518414 A GB 518414A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shock
- aircraft
- landing gear
- absorbers
- retractable landing
- 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
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
- B64C25/18—Operating mechanisms
- B64C25/20—Operating mechanisms mechanical
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
- B64C25/14—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like fore-and-aft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Fluid-Damping Devices (AREA)
Abstract
518,414. Shock-absorbers. AIREQUIPEMENT. Aug. 24, 1938, Nos. 24880 and 24881. Convention dates, Sept. 10, 1937, and Dec. 7, 1937. [Class 108 (iii)] [Also in Group XXXIII] A shock-absorber for use in aircraft alighting-gear includes a piston 33 having a one-way valve 35. The piston rod 24 is hollow and communicates with a reservoir formed in the bracing connecting two shock-absorbers which carry a landing-wheel. The piston rod passes through a tapered bore in a ring 40.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR518414X | 1937-09-10 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB518414A true GB518414A (en) | 1940-02-27 |
Family
ID=8916173
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB24880/38A Expired GB518414A (en) | 1937-09-10 | 1938-08-24 | Improvements in retractable landing gear for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB518414A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2040096A1 (en) | 2006-05-30 | 2009-03-25 | CNH Belgium N.V. | Foreign object detection system for agricultural harvesting machines |
US10640202B2 (en) | 2014-01-21 | 2020-05-05 | Safran Landing Systems Uk Ltd | Shock absorber assembly |
CN114750933A (en) * | 2022-05-07 | 2022-07-15 | 中国航空工业集团公司沈阳飞机设计研究所 | Miniaturized undercarriage retracting mechanism without damaging aircraft bearing structure |
-
1938
- 1938-08-24 GB GB24880/38A patent/GB518414A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2040096A1 (en) | 2006-05-30 | 2009-03-25 | CNH Belgium N.V. | Foreign object detection system for agricultural harvesting machines |
US10640202B2 (en) | 2014-01-21 | 2020-05-05 | Safran Landing Systems Uk Ltd | Shock absorber assembly |
CN114750933A (en) * | 2022-05-07 | 2022-07-15 | 中国航空工业集团公司沈阳飞机设计研究所 | Miniaturized undercarriage retracting mechanism without damaging aircraft bearing structure |
CN114750933B (en) * | 2022-05-07 | 2022-10-28 | 中国航空工业集团公司沈阳飞机设计研究所 | Miniaturized undercarriage retracting mechanism without damaging aircraft bearing structure |
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