GB518670A - Improvements relating to aircraft wing systems - Google Patents
Improvements relating to aircraft wing systemsInfo
- Publication number
- GB518670A GB518670A GB22825/38A GB2282538A GB518670A GB 518670 A GB518670 A GB 518670A GB 22825/38 A GB22825/38 A GB 22825/38A GB 2282538 A GB2282538 A GB 2282538A GB 518670 A GB518670 A GB 518670A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wing
- leading
- pivoted
- trailing
- disposed
- 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
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/146—Adjustable control surfaces or members, e.g. rudders forming slots at an other wing location than the rear or the front
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/28—Adjustable control surfaces or members, e.g. rudders forming slots by flaps at both the front and rear of the wing operating in unison
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/30—Wing lift efficiency
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Fluid-Pressure Circuits (AREA)
Abstract
518,670. Controlling aircraft. STONE, T. H. Aug. 2, 1938, No. 22825. [Class 4] An auxiliary surface or surfaces adapted to be nested on either or both upper and lower surfaces of an aircraft wing is carried by arms pivoted to the wing about an axis disposed nearer to the leading or trailing edge of the wing according to whether the trailing or leading edge of the surface is disposed adjacent the trailing or leading edge of the wing. In one form, the arms 21 are pivoted to brackets carried by the front spar 11 of the wing and a hydraulic jack is pivotally mounted on the rear spar 12 and comprises relatively telescopic cylinders 24A, 24B, 24C and a piston rod 24D pivoted to the surface 17. Either or both ailerons or wing flaps may be disposed rearwardly of the surface. In a modification, an additional auxiliary surface is nested normally against the upper leading surface of the wing. In this case the flaps are separately actuated by jacks disposed horizontally in the wing. In.a further modification, an auxiliary surface on the upper leading surface of the wing is connected through link and lever mechanism with the lower auxiliary surface which is actuated in a manner similar to that shown in Fig. 2.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB22825/38A GB518670A (en) | 1938-08-02 | 1938-08-02 | Improvements relating to aircraft wing systems |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB22825/38A GB518670A (en) | 1938-08-02 | 1938-08-02 | Improvements relating to aircraft wing systems |
Publications (1)
Publication Number | Publication Date |
---|---|
GB518670A true GB518670A (en) | 1940-03-05 |
Family
ID=10185647
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB22825/38A Expired GB518670A (en) | 1938-08-02 | 1938-08-02 | Improvements relating to aircraft wing systems |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB518670A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2538224A (en) * | 1945-11-13 | 1951-01-16 | Daniel R Zuck | Wing with interconnected flap and nose slat |
US2557829A (en) * | 1947-11-07 | 1951-06-19 | Thomas B Lavelle | Aircraft control means |
CN113226921A (en) * | 2018-12-28 | 2021-08-06 | 列奥纳多股份公司 | Aircraft wing |
-
1938
- 1938-08-02 GB GB22825/38A patent/GB518670A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2538224A (en) * | 1945-11-13 | 1951-01-16 | Daniel R Zuck | Wing with interconnected flap and nose slat |
US2557829A (en) * | 1947-11-07 | 1951-06-19 | Thomas B Lavelle | Aircraft control means |
CN113226921A (en) * | 2018-12-28 | 2021-08-06 | 列奥纳多股份公司 | Aircraft wing |
CN113226921B (en) * | 2018-12-28 | 2024-01-23 | 列奥纳多股份公司 | Aircraft wing |
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