BR8706925A - Conjunto para chapeletas que operam aerodinamicamente em asas de sustentacao de aeronaves,especialmente chapeletas dobraveis - Google Patents
Conjunto para chapeletas que operam aerodinamicamente em asas de sustentacao de aeronaves,especialmente chapeletas dobraveisInfo
- Publication number
- BR8706925A BR8706925A BR8706925A BR8706925A BR8706925A BR 8706925 A BR8706925 A BR 8706925A BR 8706925 A BR8706925 A BR 8706925A BR 8706925 A BR8706925 A BR 8706925A BR 8706925 A BR8706925 A BR 8706925A
- Authority
- BR
- Brazil
- Prior art keywords
- chapelets
- support wings
- aircraft support
- especially folding
- aerodynamically
- Prior art date
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
- B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
- B64C9/18—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by single flaps
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
- Check Valves (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19863643808 DE3643808A1 (de) | 1986-12-20 | 1986-12-20 | Einrichtung fuer aerodynamisch arbeitende klappen an flugzeugtragfluegeln, insbesondere spaltklappen |
Publications (1)
Publication Number | Publication Date |
---|---|
BR8706925A true BR8706925A (pt) | 1988-07-26 |
Family
ID=6316808
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR8706925A BR8706925A (pt) | 1986-12-20 | 1987-12-18 | Conjunto para chapeletas que operam aerodinamicamente em asas de sustentacao de aeronaves,especialmente chapeletas dobraveis |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP0272396B1 (pt) |
BR (1) | BR8706925A (pt) |
DE (1) | DE3643808A1 (pt) |
ES (1) | ES2031102T3 (pt) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102006036464B4 (de) | 2006-08-04 | 2009-08-20 | Airbus Deutschland Gmbh | Hochauftriebssystem für ein Flugzeug |
GB0708334D0 (en) | 2007-04-30 | 2007-06-06 | Airbus Uk Ltd | Method and apparatus for deploying an auxiliary airfoil |
CN112478133B (zh) * | 2020-12-02 | 2023-07-21 | 中国航空工业集团公司沈阳飞机设计研究所 | 一种耦合连杆驱动机构及其机翼折叠整流盖板开合结构 |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE672401C (de) * | 1936-06-20 | 1939-03-02 | Joseph Ksoll | Fluegelklappe fuer Flugzeugtragfluegel |
GB517895A (en) * | 1938-08-17 | 1940-02-12 | Fairey Aviat Co Ltd | Improvements in or relating to lifting surfaces of aircraft |
DE2914974C2 (de) * | 1979-04-12 | 1985-09-12 | Dornier Gmbh, 7990 Friedrichshafen | Kombinierte Auftriebs- bzw. Steuerklappe, insbesondere an der Hinterkante von Flugzeugtragflügeln |
US4605187A (en) * | 1984-03-09 | 1986-08-12 | The Boeing Company | Wing flap mechanism |
-
1986
- 1986-12-20 DE DE19863643808 patent/DE3643808A1/de active Granted
-
1987
- 1987-10-13 EP EP19870114933 patent/EP0272396B1/de not_active Expired - Lifetime
- 1987-10-13 ES ES87114933T patent/ES2031102T3/es not_active Expired - Lifetime
- 1987-12-18 BR BR8706925A patent/BR8706925A/pt not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
EP0272396A3 (en) | 1989-12-06 |
DE3643808C2 (pt) | 1989-03-16 |
DE3643808A1 (de) | 1988-06-30 |
EP0272396A2 (de) | 1988-06-29 |
EP0272396B1 (de) | 1992-03-04 |
ES2031102T3 (es) | 1992-12-01 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
MM | Lapse due to non-payment of fees (art. 50) |