GB530816A - Improvements in and relating to aircraft - Google Patents
Improvements in and relating to aircraftInfo
- Publication number
- GB530816A GB530816A GB19433/39A GB1943339A GB530816A GB 530816 A GB530816 A GB 530816A GB 19433/39 A GB19433/39 A GB 19433/39A GB 1943339 A GB1943339 A GB 1943339A GB 530816 A GB530816 A GB 530816A
- Authority
- GB
- United Kingdom
- Prior art keywords
- vane
- wing
- july
- slots
- aircraft
- 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)
- Air-Flow Control Members (AREA)
Abstract
530,816. Controlling aircraft. JUNKERS FLUGZEUG - UND - MOTOREN - WERKE AKT.-GES. July 4, 1939, No. 19433. Convention date, July 8, 1938. [Class 4] A deflecting vane 2 for braking when nosediving is intersected by slots 3 which afford openings for the flow in the direction of flight when the vane is folded, from the operative position shown in Fig. 1 into the inoperative shown in Fig. 3, on the wall of the wing. The sections 4 of the vane have extensions 5 adapted to pass through slots in the wing and be secured to a common shaft 7.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE530816X | 1938-07-08 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB530816A true GB530816A (en) | 1940-12-20 |
Family
ID=6554674
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB19433/39A Expired GB530816A (en) | 1938-07-08 | 1939-07-04 | Improvements in and relating to aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB530816A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8016248B2 (en) | 2007-08-20 | 2011-09-13 | Airbus Operations Limited | Aircraft wing spoiler arrangement |
-
1939
- 1939-07-04 GB GB19433/39A patent/GB530816A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8016248B2 (en) | 2007-08-20 | 2011-09-13 | Airbus Operations Limited | Aircraft wing spoiler arrangement |
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