GB2296696B - Aerofoil - Google Patents
AerofoilInfo
- Publication number
- GB2296696B GB2296696B GB9526236A GB9526236A GB2296696B GB 2296696 B GB2296696 B GB 2296696B GB 9526236 A GB9526236 A GB 9526236A GB 9526236 A GB9526236 A GB 9526236A GB 2296696 B GB2296696 B GB 2296696B
- Authority
- GB
- United Kingdom
- Prior art keywords
- aerofoil
- 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 - Lifetime
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/44—Varying camber
- B64C3/48—Varying camber by relatively-movable parts of wing structures
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE4446031A DE4446031C2 (de) | 1994-12-23 | 1994-12-23 | Tragflügel mit Mitteln zum Verändern des Profils |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| GB9526236D0 GB9526236D0 (en) | 1996-02-21 |
| GB2296696A GB2296696A (en) | 1996-07-10 |
| GB2296696B true GB2296696B (en) | 1998-12-16 |
Family
ID=6536753
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB9526236A Expired - Lifetime GB2296696B (en) | 1994-12-23 | 1995-12-21 | Aerofoil |
Country Status (3)
| Country | Link |
|---|---|
| DE (1) | DE4446031C2 (de) |
| FR (1) | FR2728534B1 (de) |
| GB (1) | GB2296696B (de) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113148110A (zh) * | 2021-05-28 | 2021-07-23 | 西北工业大学 | 一种基于激波控制鼓包的机翼变形装置和宽速域高超声速飞行器 |
| WO2022170733A1 (zh) * | 2021-02-10 | 2022-08-18 | 上海交通大学 | 一种减阻装置 |
Families Citing this family (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB9814122D0 (en) * | 1998-07-01 | 1998-08-26 | Secr Defence | Aerofoil having improved buffet performance |
| DE19858872C2 (de) | 1998-12-19 | 2001-02-08 | Daimler Chrysler Ag | Adaptiver Flugzeugtragflügel |
| DK174261B1 (da) * | 2000-09-29 | 2002-10-21 | Bonus Energy As | Anordning til brug ved regulering af luftstrømning omkring en vindmøllevinge |
| DE10155119B4 (de) * | 2001-11-09 | 2006-12-28 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Aktuator |
| DE102004011030B4 (de) | 2004-03-04 | 2006-04-13 | Siemens Ag | Verkleidung mit integriertem Polymeraktor zur Verformung derselben |
| GB0803722D0 (en) * | 2008-02-29 | 2008-04-09 | Airbus Uk Ltd | Shock bump |
| GB0803730D0 (en) * | 2008-02-29 | 2008-04-09 | Airbus Uk Ltd | Shock bump array |
| GB0803727D0 (en) * | 2008-02-29 | 2008-04-09 | Airbus Uk Ltd | Aerodynamic structure with series of shock bumps |
| GB0803719D0 (en) | 2008-02-29 | 2008-04-09 | Airbus Uk Ltd | Aerodynamic structure with asymmetrical shock bump |
| GB0803724D0 (en) | 2008-02-29 | 2008-04-09 | Airbus Uk | Aerodynamic structure with non-uniformly spaced shock bumps |
| GB0910955D0 (en) | 2009-06-25 | 2009-08-05 | Rolls Royce Plc | Adjustable camber aerofoil |
| EP4054933B1 (de) | 2019-11-06 | 2024-06-26 | Airbus Operations GmbH | Flugzeufströmungskörper mit selektiv ansteuerbarer stosserzeugenden konturausbeulungen |
| EP3842336B1 (de) * | 2019-12-27 | 2023-06-28 | Bombardier Inc. | Variable flügelvorderkantenwölbung |
| JP2021130375A (ja) * | 2020-02-19 | 2021-09-09 | 三菱重工業株式会社 | 衝撃波抑制装置及び航空機 |
| RU2738149C1 (ru) * | 2020-03-12 | 2020-12-08 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Петербургский государственный университет путей сообщения Императора Александра I" | Кузов вагона трубопроводного транспорта |
| CN114084342B (zh) * | 2021-12-09 | 2023-12-12 | 重庆邮电大学 | 一种基于压电纤维复合材料的柔性变形机翼控制系统 |
| CN115946842B (zh) * | 2023-03-10 | 2023-05-26 | 中国空气动力研究与发展中心计算空气动力研究所 | 一种飞行器的减阻装置及飞行器 |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4232844A (en) * | 1978-01-03 | 1980-11-11 | The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland | Aerofoil with composite tip section having skewed fibres |
| DE4007694A1 (de) * | 1990-03-10 | 1991-09-12 | Deutsche Forsch Luft Raumfahrt | Tragfluegel mit veraenderbarem profil im hinteren tragfluegelbereich |
| WO1993002915A1 (en) * | 1991-08-01 | 1993-02-18 | The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland | Aerofoil with variable geometry expansion surface |
| WO1994026588A1 (en) * | 1993-05-06 | 1994-11-24 | Grumman Aerospace Corporation | Apparatus and method for controlling the shape of structures |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2277723A2 (fr) * | 1974-07-12 | 1976-02-06 | Morin Bernard | Avion a grand rapport vitesse normale/vitesse d'atterrissage |
| US4296900A (en) * | 1979-04-23 | 1981-10-27 | Vought Corporation | Airfoil construction |
| DE3320481A1 (de) * | 1983-06-07 | 1984-12-13 | Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt e.V., 5000 Köln | Verfahren und vorrichtung zur beeinflussung der stroemung an aerodynamischen profilen |
| US4582278A (en) * | 1985-02-15 | 1986-04-15 | Northrop Corporation | Air foil having adjustable shape |
| US5374011A (en) * | 1991-11-13 | 1994-12-20 | Massachusetts Institute Of Technology | Multivariable adaptive surface control |
-
1994
- 1994-12-23 DE DE4446031A patent/DE4446031C2/de not_active Expired - Fee Related
-
1995
- 1995-12-21 GB GB9526236A patent/GB2296696B/en not_active Expired - Lifetime
- 1995-12-22 FR FR9515422A patent/FR2728534B1/fr not_active Expired - Fee Related
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4232844A (en) * | 1978-01-03 | 1980-11-11 | The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland | Aerofoil with composite tip section having skewed fibres |
| DE4007694A1 (de) * | 1990-03-10 | 1991-09-12 | Deutsche Forsch Luft Raumfahrt | Tragfluegel mit veraenderbarem profil im hinteren tragfluegelbereich |
| WO1993002915A1 (en) * | 1991-08-01 | 1993-02-18 | The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland | Aerofoil with variable geometry expansion surface |
| WO1994026588A1 (en) * | 1993-05-06 | 1994-11-24 | Grumman Aerospace Corporation | Apparatus and method for controlling the shape of structures |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2022170733A1 (zh) * | 2021-02-10 | 2022-08-18 | 上海交通大学 | 一种减阻装置 |
| CN113148110A (zh) * | 2021-05-28 | 2021-07-23 | 西北工业大学 | 一种基于激波控制鼓包的机翼变形装置和宽速域高超声速飞行器 |
| CN113148110B (zh) * | 2021-05-28 | 2024-06-18 | 西北工业大学 | 机翼变形装置和宽速域高超声速飞行器 |
Also Published As
| Publication number | Publication date |
|---|---|
| GB2296696A (en) | 1996-07-10 |
| GB9526236D0 (en) | 1996-02-21 |
| DE4446031A1 (de) | 1996-06-27 |
| DE4446031C2 (de) | 1998-11-26 |
| FR2728534A1 (fr) | 1996-06-28 |
| FR2728534B1 (fr) | 2000-01-14 |
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