DE69508640D1 - Laminarströmungsschicht - Google Patents

Laminarströmungsschicht

Info

Publication number
DE69508640D1
DE69508640D1 DE69508640T DE69508640T DE69508640D1 DE 69508640 D1 DE69508640 D1 DE 69508640D1 DE 69508640 T DE69508640 T DE 69508640T DE 69508640 T DE69508640 T DE 69508640T DE 69508640 D1 DE69508640 D1 DE 69508640D1
Authority
DE
Germany
Prior art keywords
laminar flow
flow layer
layer
laminar
flow
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
Application number
DE69508640T
Other languages
English (en)
Other versions
DE69508640T2 (de
Inventor
George R Seyfang
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.)
BAE Systems PLC
Original Assignee
British Aerospace PLC
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 British Aerospace PLC filed Critical British Aerospace PLC
Publication of DE69508640D1 publication Critical patent/DE69508640D1/de
Application granted granted Critical
Publication of DE69508640T2 publication Critical patent/DE69508640T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
    • B64C21/025—Influencing 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
    • B64C21/06—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for sucking
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
    • B64C21/08—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like adjustable
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/20—Boundary layer controls by passively inducing fluid flow, e.g. by means of a pressure difference between both ends of a slot or duct
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/22—Boundary layer controls by using a surface having multiple apertures of relatively small openings other than slots
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction
DE69508640T 1994-04-28 1995-04-26 Laminarströmungsschicht Expired - Fee Related DE69508640T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9408451A GB9408451D0 (en) 1994-04-28 1994-04-28 Laminar flow skin

Publications (2)

Publication Number Publication Date
DE69508640D1 true DE69508640D1 (de) 1999-05-06
DE69508640T2 DE69508640T2 (de) 1999-07-22

Family

ID=10754282

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69508640T Expired - Fee Related DE69508640T2 (de) 1994-04-28 1995-04-26 Laminarströmungsschicht

Country Status (4)

Country Link
US (1) US5848768A (de)
EP (1) EP0679572B1 (de)
DE (1) DE69508640T2 (de)
GB (1) GB9408451D0 (de)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19649132C2 (de) * 1996-11-27 1999-09-02 Daimler Chrysler Aerospace Nase für eine aerodynamische Fläche und Verfahren zu ihrer Herstellung
DE102004024007B4 (de) * 2004-05-13 2007-10-11 Airbus Deutschland Gmbh Flugzeugkomponente, insbesondere Flügel
DE602005002144D1 (de) 2004-05-13 2007-10-04 Airbus Gmbh Flugzeugbauteil, insbesondere flügel
US7866609B2 (en) * 2007-06-15 2011-01-11 The Boeing Company Passive removal of suction air for laminar flow control, and associated systems and methods
WO2008152158A1 (es) * 2007-06-15 2008-12-18 Eads Construcciones Aeronáuticas, S.A. Dispositivo para la reducción de la fuerza lateral generada por la sección de mástiles de reabastecimiento en vuelo
US8128399B1 (en) * 2008-02-22 2012-03-06 Great Southern Flameless, Llc Method and apparatus for controlling gas flow patterns inside a heater chamber and equalizing radiant heat flux to a double fired coil
CN101602404B (zh) * 2009-07-03 2013-12-25 朱晓义 一种新型结构的飞行器
CN101941518B (zh) * 2010-08-11 2012-09-12 朱晓义 航水机动装置
CN102514683A (zh) * 2012-01-09 2012-06-27 朱晓义 一种船
US9701399B1 (en) 2013-03-18 2017-07-11 Techdyne Llc Parasitic drag induced boundary layer reduction system and method
US9487288B2 (en) 2013-06-04 2016-11-08 The Boeing Company Apparatus and methods for extending hybrid laminar flow control
CN104386236A (zh) 2014-11-17 2015-03-04 朱晓义 具有更大升力的飞行器
EP3363733B1 (de) 2017-02-18 2021-11-10 Jean-Eloi William Lombard Passivströmungsteuerungsmechanismus zur abschwächung und/oder unterdrückung von tollmien-schlichting-wellen, zur verzögerung des übergangs zu turbulenzen und zur verringerung des widerstands
CN107150788A (zh) * 2017-04-26 2017-09-12 朱晓义 一种产生更大升力的固定翼飞行器
EP3428062A1 (de) * 2017-07-11 2019-01-16 Airbus Operations GmbH Vorderkantenstruktur für ein strömungsleitsystem eines flugzeugs
ES2943266T3 (es) 2017-12-28 2023-06-12 Airbus Operations Gmbh Estructura de borde de ataque para un sistema de control de flujo de una aeronave
EP3907401A1 (de) * 2020-05-05 2021-11-10 Siemens Gamesa Renewable Energy A/S Vorrichtung zur änderung des auftriebs eines rotorblatts, rotorblatt einer windturbine und verfahren zur änderung des auftriebs eines rotorblatts
CN116680817B (zh) * 2023-08-04 2023-11-28 中国空气动力研究与发展中心计算空气动力研究所 一种表面微槽道抑制第二模态波的优化方法及优化结构

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2841344A (en) * 1955-11-28 1958-07-01 Stroukoff Michael Boundary layer control
US2821351A (en) * 1957-01-03 1958-01-28 Vadym V Utgoff Airplane wing structure embodying jet engine
US3097817A (en) * 1962-04-05 1963-07-16 Jr Hugh E Towzey Airfoil design for jet engined aircraft
DE1273338B (de) * 1962-12-01 1968-07-18 Mcmullen Ass John J Staudruck-Fluegelfahrzeug
GB1125121A (en) * 1964-10-20 1968-08-28 Joseph Brian Edwards Improvements in or relating to aircraft aerodynamic structures
US3952823A (en) * 1972-07-10 1976-04-27 Hinderks M V Vehicle gas extractor
US4462429A (en) * 1982-05-06 1984-07-31 E. I. Du Pont De Nemours And Company Apparatus and method for transferring a Bingham solid through a long conduit
DE3342421A1 (de) * 1983-11-24 1985-06-05 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Verfahren zur stabilisierenden beeinflussung abgeloester laminarer grenzschichten
US4671474A (en) * 1984-06-21 1987-06-09 The Boeing Company Fluid control apparatus and method utilizing cellular array containing mini-vortex flow patterns
WO1993008076A1 (fr) * 1991-10-14 1993-04-29 Nauchno-Proizvodstvennoe Predpriyatie 'triumf' Procede de controle de la couche limite sur la surface aerodynamique d'un aeronef, et aeronef
DE4207103C1 (de) * 1992-03-06 1993-09-16 Deutsche Aerospace Airbus Gmbh, 21129 Hamburg, De

Also Published As

Publication number Publication date
GB9408451D0 (en) 1994-06-22
US5848768A (en) 1998-12-15
DE69508640T2 (de) 1999-07-22
EP0679572A3 (de) 1996-04-17
EP0679572A2 (de) 1995-11-02
EP0679572B1 (de) 1999-03-31

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: BAE SYSTEMS PLC, FARNBOROUGH, HAMPSHIRE, GB

8339 Ceased/non-payment of the annual fee