GB451469A - Improvements in or relating to the supporting surfaces of aeroplanes - Google Patents
Improvements in or relating to the supporting surfaces of aeroplanesInfo
- Publication number
- GB451469A GB451469A GB28625/35A GB2862535A GB451469A GB 451469 A GB451469 A GB 451469A GB 28625/35 A GB28625/35 A GB 28625/35A GB 2862535 A GB2862535 A GB 2862535A GB 451469 A GB451469 A GB 451469A
- Authority
- GB
- United Kingdom
- Prior art keywords
- flaps
- wing
- flap
- aeroplane
- themselves
- 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
- B64C5/00—Stabilising surfaces
- B64C5/08—Stabilising surfaces mounted on, or supported by, wings
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Mobile Radio Communication Systems (AREA)
- Radio Relay Systems (AREA)
Abstract
451,469. Controlling aircraft. LUMIERE, H., 96, Cours Albert Thomas, Lyons, France. Oct. 16, 1935, No. 28625. Convention date, Jan. 19. [Class 4] Each wing of an aeroplane is provided with a flap or flaps 3 mounted on the upper and/or under wing-surface and each hinged on a longitudinal axis, the flap or flaps on one wing being symmetrically arranged relatively to the flap or flaps on the opposite wing so that when the flaps are brought simultaneously to the operative position perpendicular to the wing surfaces thev canalize the air between themselves or between the sides of the fuselage and themselves to increase the supporting power of the aeroplane. As shown, the flaps 3, which normally are flush with the wings 1, co-operate with flaps or ailerons &c. 5 hinged on axes at right-angles to the axes of the flaps 3, the flaps 3, 5 being operated by the same or different mechanism. In a modification, a single flap 5 extends between the flaps 3.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR451469X | 1935-01-19 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB451469A true GB451469A (en) | 1936-08-06 |
Family
ID=8900897
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB28625/35A Expired GB451469A (en) | 1935-01-19 | 1935-10-16 | Improvements in or relating to the supporting surfaces of aeroplanes |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB451469A (en) |
-
1935
- 1935-10-16 GB GB28625/35A patent/GB451469A/en not_active Expired
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