GB2243126B - A method and device for stabilization of a flying apparatus having forward swept wing - Google Patents
A method and device for stabilization of a flying apparatus having forward swept wingInfo
- Publication number
- GB2243126B GB2243126B GB9105833A GB9105833A GB2243126B GB 2243126 B GB2243126 B GB 2243126B GB 9105833 A GB9105833 A GB 9105833A GB 9105833 A GB9105833 A GB 9105833A GB 2243126 B GB2243126 B GB 2243126B
- Authority
- GB
- United Kingdom
- Prior art keywords
- stabilization
- flying apparatus
- swept wing
- forward swept
- 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 - Fee Related
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/06—Fins
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/10—Shape of wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/02—Initiating means
- B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Automation & Control Theory (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB909010849A GB9010849D0 (en) | 1989-04-04 | 1990-04-02 | A method and device for stabilization of a flying apparatus having forword swept wings |
Publications (3)
Publication Number | Publication Date |
---|---|
GB9105833D0 GB9105833D0 (en) | 1991-05-01 |
GB2243126A GB2243126A (en) | 1991-10-23 |
GB2243126B true GB2243126B (en) | 1994-12-21 |
Family
ID=10676005
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9105833A Expired - Fee Related GB2243126B (en) | 1990-04-02 | 1991-02-19 | A method and device for stabilization of a flying apparatus having forward swept wing |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2243126B (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7455264B2 (en) * | 1997-08-26 | 2008-11-25 | Mcdonnell Douglas Corporation | Reconfiguration control system for an aircraft wing |
ES2373812B1 (en) * | 2008-12-17 | 2012-12-18 | Airbus Operations, S.L. | AIRCRAFT HORIZONTAL STABILIZING SURFACE. |
RU2632550C1 (en) * | 2016-10-28 | 2017-10-05 | Публичное акционерное общество "Авиационная холдинговая компания "Сухой" | Aircraft |
-
1991
- 1991-02-19 GB GB9105833A patent/GB2243126B/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
GB9105833D0 (en) | 1991-05-01 |
GB2243126A (en) | 1991-10-23 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19990219 |