GB579789A - A combined shock absorber and retraction jack - Google Patents
A combined shock absorber and retraction jackInfo
- Publication number
- GB579789A GB579789A GB2598/44A GB259844A GB579789A GB 579789 A GB579789 A GB 579789A GB 2598/44 A GB2598/44 A GB 2598/44A GB 259844 A GB259844 A GB 259844A GB 579789 A GB579789 A GB 579789A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shock absorber
- shock
- mounting bracket
- extending
- retraction
- 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
- B64C25/22—Operating mechanisms fluid
-
- 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
- B64C25/60—Oleo legs
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Fluid-Damping Devices (AREA)
Abstract
579,789. Shock-absorbers. DOWTY, G. H. Feb. 11, 1944, Nos. 2598 and 6205. [Class 108 (iii)] [Also in Group XXXIII] An aircraft landing gear embodies a landing element mounting bracket swingable about a transverse pivot, both for shock absorption and retraction movements. which are provided for by a combined shock absorber and retraction unit having a shock absorber plunger 4 extending from one end and a remotely-controllable jack plunger 7 extending from the other end, the outer ends 5, 8 of the plungers having means of connection to the aircraft structure and mounting bracket respectively. The shock absorber comprises a piston 4a with damping ports 4b working in a cylinder 3 filled with a resilient fluid. Specification 568,582, [Group XXIX], is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2598/44A GB579789A (en) | 1944-02-11 | 1944-02-11 | A combined shock absorber and retraction jack |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2598/44A GB579789A (en) | 1944-02-11 | 1944-02-11 | A combined shock absorber and retraction jack |
Publications (1)
Publication Number | Publication Date |
---|---|
GB579789A true GB579789A (en) | 1946-08-15 |
Family
ID=9742388
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2598/44A Expired GB579789A (en) | 1944-02-11 | 1944-02-11 | A combined shock absorber and retraction jack |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB579789A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112389641A (en) * | 2020-10-30 | 2021-02-23 | 哈尔滨飞机工业集团有限责任公司 | Connecting rod transmission type front wheel turning anti-swing mechanism |
-
1944
- 1944-02-11 GB GB2598/44A patent/GB579789A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112389641A (en) * | 2020-10-30 | 2021-02-23 | 哈尔滨飞机工业集团有限责任公司 | Connecting rod transmission type front wheel turning anti-swing mechanism |
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