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DE602005002144D1 - Flugzeugbauteil, insbesondere flügel - Google Patents

Flugzeugbauteil, insbesondere flügel

Info

Publication number
DE602005002144D1
DE602005002144D1 DE602005002144T DE602005002144T DE602005002144D1 DE 602005002144 D1 DE602005002144 D1 DE 602005002144D1 DE 602005002144 T DE602005002144 T DE 602005002144T DE 602005002144 T DE602005002144 T DE 602005002144T DE 602005002144 D1 DE602005002144 D1 DE 602005002144D1
Authority
DE
Germany
Prior art keywords
plane parts
wings
especially wings
plane
parts
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
Application number
DE602005002144T
Other languages
English (en)
Inventor
Juergen Meister
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.)
Airbus Operations GmbH
Original Assignee
Airbus Operations GmbH
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
Priority claimed from DE102004024007A external-priority patent/DE102004024007B4/de
Application filed by Airbus Operations GmbH filed Critical Airbus Operations GmbH
Publication of DE602005002144D1 publication Critical patent/DE602005002144D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • B64C21/08—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
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/02—De-icing or preventing icing on exterior surfaces of aircraft by ducted hot gas or liquid
    • B64D15/04—Hot gas application
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/06—Boundary layer controls by explicitly adjusting fluid flow, e.g. by using valves, variable aperture or slot areas, variable pump action or variable fluid pressure
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Hooks, Suction Cups, And Attachment By Adhesive Means (AREA)
DE602005002144T 2004-05-13 2005-05-11 Flugzeugbauteil, insbesondere flügel Expired - Lifetime DE602005002144D1 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102004024007A DE102004024007B4 (de) 2004-05-13 2004-05-13 Flugzeugkomponente, insbesondere Flügel
US60660104P 2004-09-02 2004-09-02
PCT/EP2005/005099 WO2005113336A1 (en) 2004-05-13 2005-05-11 Aircraft component, in particular a wing

Publications (1)

Publication Number Publication Date
DE602005002144D1 true DE602005002144D1 (de) 2007-10-04

Family

ID=34966909

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005002144T Expired - Lifetime DE602005002144D1 (de) 2004-05-13 2005-05-11 Flugzeugbauteil, insbesondere flügel

Country Status (2)

Country Link
US (1) US7922126B2 (de)
DE (1) DE602005002144D1 (de)

Families Citing this family (31)

* Cited by examiner, † Cited by third party
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FR2943624B1 (fr) * 2009-03-27 2011-04-15 Airbus France Nacelle d'aeronef comportant une paroi exterieure renforcee
GB2470043B (en) * 2009-05-06 2011-06-08 Gkn Aerospace Services Ltd Heating system
CN101602404B (zh) * 2009-07-03 2013-12-25 朱晓义 一种新型结构的飞行器
US8382039B2 (en) * 2009-12-30 2013-02-26 MRA Systems Inc. Turbomachine nacelle and anti-icing system and method therefor
US8783624B2 (en) * 2010-08-15 2014-07-22 The Boeing Company Laminar flow panel
US10556670B2 (en) 2010-08-15 2020-02-11 The Boeing Company Laminar flow panel
CN102167162A (zh) * 2011-03-10 2011-08-31 洪瑞庆 一种用于飞行器的超高压流体喷射动力变轨系统及方法
GB201114433D0 (en) * 2011-08-22 2011-10-05 Airbus Operations Ltd Wing leading edge venting
DE102011112555B4 (de) * 2011-09-08 2019-10-31 Airbus Operations Gmbh Verfahren zum Einsaugen und Ausblasen von Fluid durch eine Mehrzahl von Öffnungen in einen Strömungsoberflächen-Abschnitt eines Strömungskörpers
FR2998262B1 (fr) * 2012-11-21 2016-01-15 Airbus Operations Sas Dispositif passif pour generer un film d'air froid en contact avec une surface exterieure d'un aeronef
US9487288B2 (en) * 2013-06-04 2016-11-08 The Boeing Company Apparatus and methods for extending hybrid laminar flow control
US9488067B2 (en) * 2014-01-14 2016-11-08 The Boeing Company Aircraft anti-icing systems having deflector vanes
US10000277B2 (en) * 2014-10-16 2018-06-19 Rohr, Inc. Perforated surface for suction-type laminar flow control
CN104386236A (zh) 2014-11-17 2015-03-04 朱晓义 具有更大升力的飞行器
US9908620B2 (en) * 2015-05-15 2018-03-06 Rohr, Inc. Multi-zone active laminar flow control system for an aircraft propulsion system
ES2725617T3 (es) * 2015-10-20 2019-09-25 Airbus Operations Sl Borde de ataque con control de flujo laminar y procedimiento de fabricación del mismo
ES2688537T3 (es) * 2016-01-12 2018-11-05 Airbus Operations, S.L. Borde de ataque con control del flujo laminar y procedimiento de fabricación del mismo
CN106081122A (zh) * 2016-06-01 2016-11-09 中国航空工业集团公司西安飞机设计研究所 一种飞机除冰装置
WO2018196810A1 (zh) * 2017-04-26 2018-11-01 朱晓义 从流体连续性中获得更大推动力和升力的飞行器
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
EP3505441B1 (de) 2017-12-28 2023-02-08 Airbus Operations GmbH Vorderkantenstruktur für ein strömungsleitsystem eines flugzeugs
US11433990B2 (en) 2018-07-09 2022-09-06 Rohr, Inc. Active laminar flow control system with composite panel
US11136131B2 (en) 2018-07-11 2021-10-05 Goodrich Corporation Ice protection system for a component of an aerodynamic system
US11149766B2 (en) 2018-08-24 2021-10-19 Quest Engines, LLC Controlled turbulence system
US11673651B2 (en) * 2018-09-18 2023-06-13 Airbus Operations Gmbh Leading edge structure for a flow control system of an aircraft
FR3089492B1 (fr) * 2018-12-10 2024-06-21 Airbus Aeronef presentant une aile avec un bord d’attaque perfore et un systeme de soufflage et aspiration
FR3091263A1 (fr) * 2018-12-28 2020-07-03 Daher Aerospace Bec de bord d’attaque à structure optimisée
GB2581974A (en) 2019-03-05 2020-09-09 Airbus Operations Ltd Aerofoil leading edge structures
BE1027276B1 (fr) * 2019-09-24 2020-12-08 Sonaca Sa Systeme d'aspiration de couche limite et de protection contre le givre d'une surface portante d'aeronef
US20230009263A1 (en) * 2021-07-11 2023-01-12 Papa Abdoulaye MBODJ Boundary layer suction design by using a core of a wingtip vortex for a lift-generating body

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US1932681A (en) 1929-04-05 1933-10-31 Smith John Hays Aeroplane structure
US2071744A (en) 1934-06-05 1937-02-23 Anathor-Henrikson Henrik Aeroplane
US2041795A (en) 1935-07-02 1936-05-26 Edward A Stalker Aircraft
US2422746A (en) 1941-09-13 1947-06-24 Patterson Ind Inc Airplane wing deicer
US2590457A (en) * 1946-04-20 1952-03-25 Sigma Jet propulsion device for airscrews or rotary wings
US2645435A (en) * 1947-04-09 1953-07-14 Gen Mecanique Appliquee Soc In Structure for conveying a fluid at high temperature
US2742247A (en) 1950-10-31 1956-04-17 Handley Page Ltd Outer surfaces for craft moving in one fluid
DE936618C (de) 1952-10-04 1955-12-15 Handley Page Ltd Aussenhaut fuer Fahrzeuge oder Koerper mit einer Saugvorrichtung fuer die Grenzschicht
US3213527A (en) 1956-04-30 1965-10-26 Fort Wayne Metals Inc Method of making permeable airfoil skin material
US3062483A (en) 1958-09-17 1962-11-06 Power Jets Res & Dev Ltd Aerofoil boundary layer control systems
US3085740A (en) 1960-08-30 1963-04-16 Ryan Aeronautical Co End inlet jet pump for boundary layer control system
US3194518A (en) 1963-12-12 1965-07-13 Robert L Walsh Aircraft panel construction for boundary air control
DE1266136B (de) 1964-07-07 1968-04-11 Handley Page Ltd Verfahren zur Herstellung einer mit Schlitzen versehenen Flugzeugbeplankung
US5114100A (en) 1989-12-29 1992-05-19 The Boeing Company Anti-icing system for aircraft
US5348256A (en) 1992-05-13 1994-09-20 The Boeing Company Supersonic aircraft and method
JPH06191491A (ja) 1992-07-06 1994-07-12 Rockwell Internatl Corp 層流制御に使われるタイプの穴を開けられたパネルの表面に圧力の離散領域を確立するシステム
GB9400555D0 (en) 1994-01-13 1994-03-09 Short Brothers Plc Boundery layer control in aerodynamic low drag structures
GB9408451D0 (en) 1994-04-28 1994-06-22 British Aerospace Laminar flow skin
US5772156A (en) 1995-11-30 1998-06-30 The Boeing Company Aircraft boundary layer control system with discharge transpiration panel
GB2314887B (en) 1996-07-02 2000-02-09 Rolls Royce Plc Ice protection for porous structure
US5813625A (en) 1996-10-09 1998-09-29 Mcdonnell Douglas Helicopter Company Active blowing system for rotorcraft vortex interaction noise reduction
DE19643069C2 (de) 1996-10-18 1999-03-25 Daimler Benz Aerospace Airbus Seitenleitwerksstrukur für ein Flugzeug
US6302360B1 (en) 2000-01-10 2001-10-16 The University Of Toledo Vortex generation for control of the air flow along the surface of an airfoil
US20020134891A1 (en) 2001-02-09 2002-09-26 Guillot Stephen A. Ejector pump flow control

Also Published As

Publication number Publication date
US7922126B2 (en) 2011-04-12
US20100116943A1 (en) 2010-05-13

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Legal Events

Date Code Title Description
8332 No legal effect for de