GB534106A - Improvements in or relating to means for aligning folding wings for aircraft - Google Patents
Improvements in or relating to means for aligning folding wings for aircraftInfo
- Publication number
- GB534106A GB534106A GB32569/39A GB3256939A GB534106A GB 534106 A GB534106 A GB 534106A GB 32569/39 A GB32569/39 A GB 32569/39A GB 3256939 A GB3256939 A GB 3256939A GB 534106 A GB534106 A GB 534106A
- Authority
- GB
- United Kingdom
- Prior art keywords
- joint
- aircraft
- lever
- folding
- 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
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/56—Folding or collapsing to reduce overall dimensions of aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Retarders (AREA)
- Mobile Radio Communication Systems (AREA)
- Agricultural Machines (AREA)
Abstract
534,106. Aircraft with folding wings. FAIRY AVIATION CO., Ltd., and GREENFIELD, W. W. Dec. 20, 1939, No. 32569. [Class 4] A folding wing for aircraft fitted with a known lever e at the leading edge of the stub wing to engage a pin p on the folding part to prevent vertical sag at the joint before engagement of the locking bolts, has a similar lever d pivoted to the stub wing to engage a pin m, offset from the joint, on a bracket k on the folding part to prevent sag about a fore-and-aft axis in the plane of the joint. The lever d is spring urged towards a stop j when the joint is open.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB32569/39A GB534106A (en) | 1939-12-20 | 1939-12-20 | Improvements in or relating to means for aligning folding wings for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB32569/39A GB534106A (en) | 1939-12-20 | 1939-12-20 | Improvements in or relating to means for aligning folding wings for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB534106A true GB534106A (en) | 1941-02-27 |
Family
ID=10340671
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB32569/39A Expired GB534106A (en) | 1939-12-20 | 1939-12-20 | Improvements in or relating to means for aligning folding wings for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB534106A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2544278A1 (en) * | 1983-04-14 | 1984-10-19 | Serleg | Device for rapid assembly and disassembly of elements of aerodynes |
CN109606634A (en) * | 2018-11-22 | 2019-04-12 | 成都飞机工业(集团)有限责任公司 | A kind of twin axle wingfold mechanism |
CN116986032A (en) * | 2023-09-21 | 2023-11-03 | 成都纵横大鹏无人机科技有限公司 | Folding wing and unmanned aerial vehicle |
-
1939
- 1939-12-20 GB GB32569/39A patent/GB534106A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2544278A1 (en) * | 1983-04-14 | 1984-10-19 | Serleg | Device for rapid assembly and disassembly of elements of aerodynes |
CN109606634A (en) * | 2018-11-22 | 2019-04-12 | 成都飞机工业(集团)有限责任公司 | A kind of twin axle wingfold mechanism |
CN109606634B (en) * | 2018-11-22 | 2022-04-08 | 成都飞机工业(集团)有限责任公司 | Double-shaft wing folding mechanism |
CN116986032A (en) * | 2023-09-21 | 2023-11-03 | 成都纵横大鹏无人机科技有限公司 | Folding wing and unmanned aerial vehicle |
CN116986032B (en) * | 2023-09-21 | 2023-12-15 | 成都纵横大鹏无人机科技有限公司 | Folding wing and unmanned aerial vehicle |
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