GB527802A - Improvements relating to folding wing aircraft - Google Patents
Improvements relating to folding wing aircraftInfo
- Publication number
- GB527802A GB527802A GB11933/39A GB1193339A GB527802A GB 527802 A GB527802 A GB 527802A GB 11933/39 A GB11933/39 A GB 11933/39A GB 1193339 A GB1193339 A GB 1193339A GB 527802 A GB527802 A GB 527802A
- Authority
- GB
- United Kingdom
- Prior art keywords
- main
- aircraft
- wings
- folding wing
- wing aircraft
- 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)
- Extensible Doors And Revolving Doors (AREA)
Abstract
527,802. Folding wing aircraft. GENERAL AIRCRAFT, Ltd., WILLIAMS, D. L. H., and CROCOMBE, F. F. April 20, 1939, No. 11933. [Class 4] An aircraft structure embodying an undercarriage of the tricycle type has the main wings arranged to be folded in the forward sense. Fig. 4 shows a form in which a pusher airscrew 10<1> is located at the rear of the fuselage 12, 6 being the main landing wheels and 7 the nose landing wheel. The wings 8 fold forwards, a light frame work 13 carrying the control surfaces 14, 15; each main wing may carry a power unit and screw. In Fig. 3 the main wings fold about the points 9 and are in two parts pivoted at 11. Specification 506,528 is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB11933/39A GB527802A (en) | 1939-04-20 | 1939-04-20 | Improvements relating to folding wing aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB11933/39A GB527802A (en) | 1939-04-20 | 1939-04-20 | Improvements relating to folding wing aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB527802A true GB527802A (en) | 1940-10-16 |
Family
ID=9995313
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB11933/39A Expired GB527802A (en) | 1939-04-20 | 1939-04-20 | Improvements relating to folding wing aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB527802A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2379915A (en) * | 2001-07-03 | 2003-03-26 | Bae Systems Plc | Unmanned aerial vehicle (UAV) with detachable wings |
EP3411294B1 (en) * | 2016-02-01 | 2023-08-02 | Tudor Crossfelt, LLP | Folding beam for swinging wing |
-
1939
- 1939-04-20 GB GB11933/39A patent/GB527802A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2379915A (en) * | 2001-07-03 | 2003-03-26 | Bae Systems Plc | Unmanned aerial vehicle (UAV) with detachable wings |
GB2379915B (en) * | 2001-07-03 | 2004-11-10 | Bae Systems Plc | An aircraft |
US6817573B2 (en) | 2001-07-03 | 2004-11-16 | Bae Systems Plc | Aircraft |
EP3411294B1 (en) * | 2016-02-01 | 2023-08-02 | Tudor Crossfelt, LLP | Folding beam for swinging wing |
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