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GB9526236D0 - Aerofoil - Google Patents

Aerofoil

Info

Publication number
GB9526236D0
GB9526236D0 GBGB9526236.6A GB9526236A GB9526236D0 GB 9526236 D0 GB9526236 D0 GB 9526236D0 GB 9526236 A GB9526236 A GB 9526236A GB 9526236 D0 GB9526236 D0 GB 9526236D0
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.)
Granted
Application number
GBGB9526236.6A
Other versions
GB2296696A (en
GB2296696B (en
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Deutsches Zentrum fuer Luft und Raumfahrt eV
Original Assignee
Deutsches Zentrum fuer Luft und Raumfahrt eV
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=6536753&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=GB9526236(D0) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Deutsches Zentrum fuer Luft und Raumfahrt eV filed Critical Deutsches Zentrum fuer Luft und Raumfahrt eV
Publication of GB9526236D0 publication Critical patent/GB9526236D0/en
Publication of GB2296696A publication Critical patent/GB2296696A/en
Application granted granted Critical
Publication of GB2296696B publication Critical patent/GB2296696B/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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)
GB9526236A 1994-12-23 1995-12-21 Aerofoil Expired - Lifetime GB2296696B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE4446031A DE4446031C2 (en) 1994-12-23 1994-12-23 Wing with means for changing the profile

Publications (3)

Publication Number Publication Date
GB9526236D0 true GB9526236D0 (en) 1996-02-21
GB2296696A GB2296696A (en) 1996-07-10
GB2296696B 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 (en)
FR (1) FR2728534B1 (en)
GB (1) GB2296696B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114084342A (en) * 2021-12-09 2022-02-25 重庆邮电大学 Flexible deformable wing control system based on piezoelectric fiber composite material

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB9814122D0 (en) * 1998-07-01 1998-08-26 Secr Defence Aerofoil having improved buffet performance
DE19858872C2 (en) * 1998-12-19 2001-02-08 Daimler Chrysler Ag Adaptive aircraft wing
DK174261B1 (en) 2000-09-29 2002-10-21 Bonus Energy As Device for use in regulating air flow around a wind turbine blade
DE10155119B4 (en) * 2001-11-09 2006-12-28 Deutsches Zentrum für Luft- und Raumfahrt e.V. actuator
DE102004011030B4 (en) * 2004-03-04 2006-04-13 Siemens Ag Cover with integrated polymer actuator for deformation of the same
GB0803727D0 (en) * 2008-02-29 2008-04-09 Airbus Uk Ltd Aerodynamic structure with series of shock bumps
GB0803724D0 (en) * 2008-02-29 2008-04-09 Airbus Uk Aerodynamic structure with non-uniformly spaced shock bumps
GB0803730D0 (en) * 2008-02-29 2008-04-09 Airbus Uk Ltd Shock bump array
GB0803722D0 (en) * 2008-02-29 2008-04-09 Airbus Uk Ltd Shock bump
GB0803719D0 (en) * 2008-02-29 2008-04-09 Airbus Uk Ltd Aerodynamic structure with asymmetrical shock bump
GB0910955D0 (en) 2009-06-25 2009-08-05 Rolls Royce Plc Adjustable camber aerofoil
EP4054933B1 (en) 2019-11-06 2024-06-26 Airbus Operations GmbH Flow body for an aircraft with a selectively activatable shock bump
EP3842336B1 (en) * 2019-12-27 2023-06-28 Bombardier Inc. Variable wing leading edge camber
JP2021130375A (en) 2020-02-19 2021-09-09 三菱重工業株式会社 Shock wave suppression device and aircraft
RU2738149C1 (en) * 2020-03-12 2020-12-08 Федеральное государственное бюджетное образовательное учреждение высшего образования "Петербургский государственный университет путей сообщения Императора Александра I" Car body of pipeline transport
WO2022170733A1 (en) * 2021-02-10 2022-08-18 上海交通大学 Drag reduction device
CN113148110B (en) * 2021-05-28 2024-06-18 西北工业大学 Wing deformation device and wide-speed-domain hypersonic aircraft
CN115946842B (en) * 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 Drag reduction device of aircraft and aircraft

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2277723A2 (en) * 1974-07-12 1976-02-06 Morin Bernard AIRPLANE AT NORMAL SPEED / LANDING SPEED
DE2856400C2 (en) * 1978-01-03 1987-04-30 The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland, London Wings, especially for rotary-wing aircraft
US4296900A (en) * 1979-04-23 1981-10-27 Vought Corporation Airfoil construction
DE3320481A1 (en) * 1983-06-07 1984-12-13 Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt e.V., 5000 Köln Method and device for influencing the flow on aerodynamic profiles
US4582278A (en) * 1985-02-15 1986-04-15 Northrop Corporation Air foil having adjustable shape
DE4007694A1 (en) * 1990-03-10 1991-09-12 Deutsche Forsch Luft Raumfahrt Variable-profile aircraft wing - has front profiled component hinging where flow is deflected for high lift
GB9116787D0 (en) * 1991-08-01 1991-09-18 Secr Defence Article having an aerofoil section with a distensible expansion surface
US5374011A (en) * 1991-11-13 1994-12-20 Massachusetts Institute Of Technology Multivariable adaptive surface control
KR960702399A (en) * 1993-05-06 1996-04-27 제임스, 씨. 존슨 APPARATUS AND METHOD FOR CONTROLLING THE SHAPE OF STRUCTURES

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114084342A (en) * 2021-12-09 2022-02-25 重庆邮电大学 Flexible deformable wing control system based on piezoelectric fiber composite material
CN114084342B (en) * 2021-12-09 2023-12-12 重庆邮电大学 Flexible deformation wing control system based on piezoelectric fiber composite material

Also Published As

Publication number Publication date
FR2728534B1 (en) 2000-01-14
DE4446031C2 (en) 1998-11-26
GB2296696A (en) 1996-07-10
DE4446031A1 (en) 1996-06-27
FR2728534A1 (en) 1996-06-28
GB2296696B (en) 1998-12-16

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