GB605604A - Aerodynamic brake for aircraft - Google Patents
Aerodynamic brake for aircraftInfo
- Publication number
- GB605604A GB605604A GB35264/45A GB3526445A GB605604A GB 605604 A GB605604 A GB 605604A GB 35264/45 A GB35264/45 A GB 35264/45A GB 3526445 A GB3526445 A GB 3526445A GB 605604 A GB605604 A GB 605604A
- Authority
- GB
- United Kingdom
- Prior art keywords
- plates
- aerodynamic brake
- aircraft
- operated
- 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
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/32—Air braking surfaces
- B64C9/323—Air braking surfaces associated with wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/32—Air braking surfaces
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Braking Arrangements (AREA)
Abstract
605,604. Controlling aircraft. DUPUIS, J. R. G. Dec. 31, 1945, No. 35264. Convention date, Feb. 27. [Class 4] An aerodynamic brake comprises a pair of plates 1, 2 on each wing, the plates 1 being mounted on the undersurface towards the inboard ends and the plates 2 on the upper surface towards the wing tips. The plates may be flat, or of part-cylindrical form as shown, mounted on spring-loaded crank arms 3, 4 operated by rods 7, 8. The relative dimensions and extents of movement of the plates are arranged so that for braking in horizontal flight an increase of lift is obtained with constant pitching moment. For lateral control purposes the upper members 2 may be operated differentially as spoilers.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR605604X | 1945-02-27 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB605604A true GB605604A (en) | 1948-07-27 |
Family
ID=8974094
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB35264/45A Expired GB605604A (en) | 1945-02-27 | 1945-12-31 | Aerodynamic brake for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB605604A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2621005A1 (en) * | 1987-09-26 | 1989-03-31 | Messerschmitt Boelkow Blohm | AIRCRAFT WHICH DEPTH CONTROL ORDERS DO NOT, IN PARTICULAR FLOORS, FLYING WINGS OR THE LIKE |
GB2512318A (en) * | 2013-03-26 | 2014-10-01 | Eads Uk Ltd | Lift-reducing apparatus for aircraft wings |
-
1945
- 1945-12-31 GB GB35264/45A patent/GB605604A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2621005A1 (en) * | 1987-09-26 | 1989-03-31 | Messerschmitt Boelkow Blohm | AIRCRAFT WHICH DEPTH CONTROL ORDERS DO NOT, IN PARTICULAR FLOORS, FLYING WINGS OR THE LIKE |
US4955958A (en) * | 1987-09-26 | 1990-09-11 | Mbb Gmbh | Aircraft |
GB2512318A (en) * | 2013-03-26 | 2014-10-01 | Eads Uk Ltd | Lift-reducing apparatus for aircraft wings |
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