GB627121A - Aircraft with folding wings - Google Patents
Aircraft with folding wingsInfo
- Publication number
- GB627121A GB627121A GB1493/47A GB149347A GB627121A GB 627121 A GB627121 A GB 627121A GB 1493/47 A GB1493/47 A GB 1493/47A GB 149347 A GB149347 A GB 149347A GB 627121 A GB627121 A GB 627121A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wings
- wing portion
- hinge
- folding
- fixed
- 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)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
627,121. Folding wings for aeroplanes. SOC. NATIONALE DE CONSTRUCTIONS AERONAUTIQUES DU NORD. April 29, 1947, No. 11493. Convention date, Nov. 14, 1946. [Class 4] In an aircraft with folding wings, the movable portions 5 are connected to the fixed portions 4 by hinges whose axes X-X<SP>1</SP> are inclined and located in the longitudinal plane of the main spars 6, 8 of the wings. In the form shown, the hinge axes converge downwardly, the wing portion in front of each hinge being of stepped shape DEFG in plan, while the upper surface of the fixed wing portion 4 to the rear of the hinge is formed with a recess 9 to allow the passage of the lower edge 10 of the rear portion of the movable wing portion 5 during folding and unfolding. The undersurface of the fixed portion is formed with a horizontal extension 11 for supporting the wing portion 5, while the latter carries a flap 12 covering the recess 9 when the wing is extended. The wings may be operated by hydraulic or electric jacks 14, and remotely controlled locking devices 17, 18 may be employed for securing the wings in their extended position.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR627121X | 1946-11-14 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB627121A true GB627121A (en) | 1949-07-28 |
Family
ID=8988832
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1493/47A Expired GB627121A (en) | 1946-11-14 | 1947-04-29 | Aircraft with folding wings |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB627121A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6347507B1 (en) | 1992-09-14 | 2002-02-19 | Ramgen Power Systems, Inc. | Method and apparatus for power generation using rotating ramjets |
CN103448903A (en) * | 2012-05-31 | 2013-12-18 | 空中客车营运有限公司 | Method of coupling aerofoil surface structures and an aerofoil assembly |
WO2015150835A1 (en) * | 2014-04-04 | 2015-10-08 | Airbus Operations Limited | An aircraft comprising a foldable aerodynamic structure and a method of manufacturing a foldable aerodynamic structure for an aircraft |
GB2551185A (en) * | 2016-06-09 | 2017-12-13 | Airbus Operations Ltd | An interface between an outer end of a wing and a moveable wing tip device |
GB2568738A (en) * | 2017-11-27 | 2019-05-29 | Airbus Operations Ltd | An improved interface between an outer end of a wing and a moveable wing tip device |
GB2568737A (en) * | 2017-11-27 | 2019-05-29 | Airbus Operations Ltd | A curved interface between an outer end of a wing and a moveable wing tip device |
GB2572150A (en) * | 2018-03-19 | 2019-09-25 | Airbus Operations Ltd | A moveable wing tip device an outer end of a wing, and interface therebetween |
-
1947
- 1947-04-29 GB GB1493/47A patent/GB627121A/en not_active Expired
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6347507B1 (en) | 1992-09-14 | 2002-02-19 | Ramgen Power Systems, Inc. | Method and apparatus for power generation using rotating ramjets |
CN103448903A (en) * | 2012-05-31 | 2013-12-18 | 空中客车营运有限公司 | Method of coupling aerofoil surface structures and an aerofoil assembly |
US9096304B2 (en) | 2012-05-31 | 2015-08-04 | Airbus Operations Limited | Method of coupling aerofoil surface structures and an aerofoil assembly |
EP2669187A3 (en) * | 2012-05-31 | 2017-04-19 | Airbus Operations Limited | Method of coupling aerofoil surface structures and an aerofoil assembly |
US10583909B2 (en) | 2014-04-04 | 2020-03-10 | Airbus Operations Limited | Aircraft comprising a foldable aerodynamic structure and a method of manufacturing a foldable aerodynamic structure for an aircraft |
WO2015150835A1 (en) * | 2014-04-04 | 2015-10-08 | Airbus Operations Limited | An aircraft comprising a foldable aerodynamic structure and a method of manufacturing a foldable aerodynamic structure for an aircraft |
KR20160141791A (en) * | 2014-04-04 | 2016-12-09 | 에어버스 오퍼레이션즈 리미티드 | An aircraft comprising a foldable aerodynamic structure and a method of manufacturing a foldable aerodynamic structure for an aircraft |
KR102307498B1 (en) * | 2014-04-04 | 2021-09-29 | 에어버스 오퍼레이션즈 리미티드 | An aircraft comprising a foldable aerodynamic structure and a method of manufacturing a foldable aerodynamic structure for an aircraft |
GB2551185A (en) * | 2016-06-09 | 2017-12-13 | Airbus Operations Ltd | An interface between an outer end of a wing and a moveable wing tip device |
US10669006B2 (en) | 2016-06-09 | 2020-06-02 | Airbus Operations Limited | Interface between an outer end of a wing and a moveable wing tip device |
GB2568737A (en) * | 2017-11-27 | 2019-05-29 | Airbus Operations Ltd | A curved interface between an outer end of a wing and a moveable wing tip device |
US11052990B2 (en) | 2017-11-27 | 2021-07-06 | Airbus Operations Limited | Interface between an outer end of a wing and a moveable wing tip device |
GB2568738A (en) * | 2017-11-27 | 2019-05-29 | Airbus Operations Ltd | An improved interface between an outer end of a wing and a moveable wing tip device |
US11142298B2 (en) | 2017-11-27 | 2021-10-12 | Airbus Operations Limited | Curved interface between an outer end of a wing and a moveable wing tip device |
GB2572150A (en) * | 2018-03-19 | 2019-09-25 | Airbus Operations Ltd | A moveable wing tip device an outer end of a wing, and interface therebetween |
US11192630B2 (en) | 2018-03-19 | 2021-12-07 | Airbus Operations Limited | Moveable wing tip device, an outer end of a wing, and interface therebetween |
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