GB706984A - Improvements in and relating to aircraft - Google Patents
Improvements in and relating to aircraftInfo
- Publication number
- GB706984A GB706984A GB270451A GB270451A GB706984A GB 706984 A GB706984 A GB 706984A GB 270451 A GB270451 A GB 270451A GB 270451 A GB270451 A GB 270451A GB 706984 A GB706984 A GB 706984A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wing
- aircraft
- fuselage
- solids
- revolution
- 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
- B64C3/40—Varying angle of sweep
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mobile Radio Communication Systems (AREA)
Abstract
706,984. Aircraft wings and stabilising surfaces. BOULTON PAUL AIRCRAFT, Ltd. Jan. 30, 1952 [Feb. 2, 1951], No. 2704/51. Class 4 In an aircraft wing or the like, or part thereof, adapted-to be pivotally attached to the aircraft to permit variation of the angle of sweep, the wing or the like is of such a shape near the axis of rotation as to form a solid or solids of revolution about said axis. The wing or stabilizing surface 1 is pivoted at 4 to the fuselage 5, the root portions 8 and 9 being formed as solids of revolution 2 and 3 about the point 4, the respective sections of the solids being determined by the sectional profiles 6, 7 of the wing. at the lines of intersection with the fuselage when the wing is respectively in its fully forward swept and fully rearward swept positions. By this means a uniform clearance and simplified sealing between the root portions of the wing and the openings in the fuselage is ensured.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB270451A GB706984A (en) | 1951-02-02 | 1951-02-02 | Improvements in and relating to aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB270451A GB706984A (en) | 1951-02-02 | 1951-02-02 | Improvements in and relating to aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB706984A true GB706984A (en) | 1954-04-07 |
Family
ID=9744326
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB270451A Expired GB706984A (en) | 1951-02-02 | 1951-02-02 | Improvements in and relating to aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB706984A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4415132A (en) * | 1981-11-25 | 1983-11-15 | The United States Of America As Represented By The Secretary Of The Air Force | Aircraft having variable incidence forward-swept wing |
US9199717B2 (en) | 2009-04-06 | 2015-12-01 | Airbus Operations Gmbh | Center fuselage bellows |
-
1951
- 1951-02-02 GB GB270451A patent/GB706984A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4415132A (en) * | 1981-11-25 | 1983-11-15 | The United States Of America As Represented By The Secretary Of The Air Force | Aircraft having variable incidence forward-swept wing |
US9199717B2 (en) | 2009-04-06 | 2015-12-01 | Airbus Operations Gmbh | Center fuselage bellows |
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