GB496003A - Improvements in or relating to folding wing aircraft - Google Patents
Improvements in or relating to folding wing aircraftInfo
- Publication number
- GB496003A GB496003A GB33094/37A GB3309437A GB496003A GB 496003 A GB496003 A GB 496003A GB 33094/37 A GB33094/37 A GB 33094/37A GB 3309437 A GB3309437 A GB 3309437A GB 496003 A GB496003 A GB 496003A
- Authority
- GB
- United Kingdom
- Prior art keywords
- folding
- wing aircraft
- link
- links
- wing
- 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)
- Air Bags (AREA)
Abstract
496,003. Folding-wing aircraft. FAIREY AVIATION CO., Ltd., and TROTTER, J. C. Nov. 30, 1937, No. 33094. [Class 4] In a folding-wing aircraft in which parts of the trailing marginal portions of the wings are adapted to be folded over or under the main parts of the wings, the folding means comprise means arranged to exert a force on a pair of links pivotally connected together at one end and pivotally connected to main wing and folding part respectively at their other ends. As applied to a folding-wing aircraft such as described in Specification 484,622, a link o, Fig. 3, is pivoted at q to folding part e, a link n is pivoted at p to main wing part c and the other ends of the links are connected to a nut m on a screwed shaft j adapted to be rotated by turning an external handle g which may be detachable. A hydraulic jack may replace the screw jack and the piston-rod may be connected at a point on link n adjacent the common pivot of the links n, o.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB33094/37A GB496003A (en) | 1937-11-30 | 1937-11-30 | Improvements in or relating to folding wing aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB33094/37A GB496003A (en) | 1937-11-30 | 1937-11-30 | Improvements in or relating to folding wing aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB496003A true GB496003A (en) | 1938-11-23 |
Family
ID=10348480
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB33094/37A Expired GB496003A (en) | 1937-11-30 | 1937-11-30 | Improvements in or relating to folding wing aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB496003A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| RU2798618C1 (en) * | 2022-12-28 | 2023-06-23 | Публичное акционерное общество "Объединенная авиастроительная корпорация" (ПАО "ОАК") | Aircraft with high transportability |
-
1937
- 1937-11-30 GB GB33094/37A patent/GB496003A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| RU2798618C1 (en) * | 2022-12-28 | 2023-06-23 | Публичное акционерное общество "Объединенная авиастроительная корпорация" (ПАО "ОАК") | Aircraft with high transportability |
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