CA2106850A1 - Regulation de couche limite - Google Patents

Regulation de couche limite

Info

Publication number
CA2106850A1
CA2106850A1 CA002106850A CA2106850A CA2106850A1 CA 2106850 A1 CA2106850 A1 CA 2106850A1 CA 002106850 A CA002106850 A CA 002106850A CA 2106850 A CA2106850 A CA 2106850A CA 2106850 A1 CA2106850 A1 CA 2106850A1
Authority
CA
Canada
Prior art keywords
component
component part
face
facing
front face
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.)
Abandoned
Application number
CA002106850A
Other languages
English (en)
Inventor
Mark A. Braniff
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.)
Short Brothers PLC
Original Assignee
Individual
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
Application filed by Individual filed Critical Individual
Publication of CA2106850A1 publication Critical patent/CA2106850A1/fr
Abandoned legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C21/00Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/02Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
    • B64C21/025Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for simultaneous blowing and sucking
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C2230/00Boundary layer controls
    • B64C2230/04Boundary layer controls by actively generating fluid flow
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C2230/00Boundary layer controls
    • B64C2230/22Boundary layer controls by using a surface having multiple apertures of relatively small openings other than slots
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0226Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising boundary layer control means
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/10Drag reduction
CA002106850A 1991-05-30 1992-05-27 Regulation de couche limite Abandoned CA2106850A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB919111620A GB9111620D0 (en) 1991-05-30 1991-05-30 Boundary layer control
GB9111620.2 1991-05-30

Publications (1)

Publication Number Publication Date
CA2106850A1 true CA2106850A1 (fr) 1992-12-01

Family

ID=10695800

Family Applications (1)

Application Number Title Priority Date Filing Date
CA002106850A Abandoned CA2106850A1 (fr) 1991-05-30 1992-05-27 Regulation de couche limite

Country Status (6)

Country Link
EP (1) EP0585305A1 (fr)
AU (1) AU1767292A (fr)
CA (1) CA2106850A1 (fr)
GB (2) GB9111620D0 (fr)
IL (1) IL102048A0 (fr)
WO (1) WO1992021560A1 (fr)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4414205C2 (de) * 1994-04-23 1999-09-02 Daimler Chrysler Aerospace Anordnung zur Grenzschichtabsaugung
GB2294709B (en) * 1994-11-04 1998-03-04 Rolls Royce Plc A method of manufacturing a porous material
GB9914652D0 (en) 1999-06-24 1999-08-25 British Aerospace Laminar flow control system and suction panel for use therein
NZ511661A (en) 2001-05-11 2003-09-26 Graham Bond Grove An improved aerofoil
FR2850353B1 (fr) * 2003-01-29 2005-12-30 Const Aeronautiques Du Nord Es Dispositif de modulation de turbulences pour avions
EP1607624A3 (fr) * 2004-06-15 2008-11-26 NORDEX ENERGY GmbH Pale pour éolienne
CN103025607B (zh) 2010-04-12 2016-08-03 空中客车运作有限责任公司 用作流动体的外壁的轮廓板部分,制造轮廓板部分的方法和包括流体的吸入-抽出装置的流动体组件
DE102010036154B4 (de) 2010-09-02 2017-01-26 Airbus Operations Gmbh Luft absaugende Fahrzeugrumpfkomponente, Verfahren zum Herstellen einer Luft absaugenden Fahrzeugrumpfkomponente und Fahrzeug, insbesondere Flugzeug, mit einer Luft absaugenden Fahrzeugrumpfkomponente
US9745053B2 (en) 2014-11-11 2017-08-29 Airbus Operations Gmbh Aerodynamic component and method for producing an aerodynamic component
EP3428062A1 (fr) 2017-07-11 2019-01-16 Airbus Operations GmbH Structure de bord d'attaque pour système de commande d'écoulement d'un aéronef
ES2927476T3 (es) 2017-10-09 2022-11-07 Airbus Operations Gmbh Unidad de cola vertical para control de flujo
EP3466811B1 (fr) 2017-10-09 2023-06-21 Airbus Operations GmbH Empennage vertical pour la régulation de l'écoulement
GB2567683A (en) 2017-10-20 2019-04-24 Airbus Operations Ltd Apparatus for laminar flow control
US11396366B2 (en) 2018-09-28 2022-07-26 Rohr, Inc. Active laminar flow control structural plenums fastened
US11414203B2 (en) 2018-09-28 2022-08-16 Rohr, Inc. Active laminar flow control plenum panel arrangement
US11524770B2 (en) 2018-09-28 2022-12-13 Rohr, Inc. Active laminar flow control plenum panel arrangements and installation methods

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3128973A (en) * 1964-04-14 Porous material
GB619722A (en) * 1946-12-20 1949-03-14 English Electric Co Ltd Improvements in and relating to boundary layer control in fluid conduits
GB687723A (en) * 1950-04-06 1953-02-18 Malcolm Robert Head Improvements in suction aerofoils and the like
GB713426A (en) * 1950-10-31 1954-08-11 Handley Page Ltd Improvements in or relating to external surfaces for moving craft
GB718421A (en) * 1951-02-12 1954-11-17 Fairey Aviat Co Ltd Improvements relating to boundary layer control means for aerofoils and other boundary walls
GB743598A (en) * 1953-04-15 1956-01-18 Power Jets U Res And Developme Aircraft boundary layer suction systems and compressors therefor
US2843341A (en) * 1956-01-18 1958-07-15 Robert E Dannenberg Airfoils, variable permeability material and method of fabrication thereof
GB862032A (en) * 1958-10-03 1961-03-01 Power Jets Res & Dev Ltd Aircraft
US3467348A (en) * 1967-10-10 1969-09-16 Jerome H Lemelson Aircraft structures and systems
GB1240995A (en) * 1967-11-06 1971-07-28 Hawker Siddeley Aviation Ltd Improvements in or relating to aircraft lifting surfaces
US4296899A (en) * 1977-06-30 1981-10-27 The Boeing Company Apparatus and method for manufacturing laminar flow control aircraft structure
US4258889A (en) * 1979-03-29 1981-03-31 The Boeing Company Method and apparatus for laminar flow control
US4575030A (en) * 1982-09-13 1986-03-11 The Boeing Company Laminar flow control airfoil
US4749150A (en) * 1985-12-24 1988-06-07 Rohr Industries, Inc. Turbofan duct with noise suppression and boundary layer control

Also Published As

Publication number Publication date
GB2256253B (en) 1995-01-11
EP0585305A1 (fr) 1994-03-09
GB9211225D0 (en) 1992-07-15
IL102048A0 (en) 1992-12-30
GB9111620D0 (en) 1991-07-24
WO1992021560A1 (fr) 1992-12-10
AU1767292A (en) 1993-01-08
GB2256253A (en) 1992-12-02

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Legal Events

Date Code Title Description
FZDE Discontinued