DE60202540D1 - Enteisungverfahren mit Zwangsumlauf für die Lufteinlasshaube eines Strahltriebwerkes und Vorrichtung zur Durchführung des Verfahrens - Google Patents

Enteisungverfahren mit Zwangsumlauf für die Lufteinlasshaube eines Strahltriebwerkes und Vorrichtung zur Durchführung des Verfahrens

Info

Publication number
DE60202540D1
DE60202540D1 DE60202540T DE60202540T DE60202540D1 DE 60202540 D1 DE60202540 D1 DE 60202540D1 DE 60202540 T DE60202540 T DE 60202540T DE 60202540 T DE60202540 T DE 60202540T DE 60202540 D1 DE60202540 D1 DE 60202540D1
Authority
DE
Germany
Prior art keywords
islets
lip
icing
jet engine
air intake
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
DE60202540T
Other languages
English (en)
Other versions
DE60202540T2 (de
Inventor
Alain Porte
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 SAS
Original Assignee
Airbus Operations SAS
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 Airbus Operations SAS filed Critical Airbus Operations SAS
Publication of DE60202540D1 publication Critical patent/DE60202540D1/de
Application granted granted Critical
Publication of DE60202540T2 publication Critical patent/DE60202540T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0233—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising de-icing means
DE60202540T 2001-02-15 2002-02-12 Enteisungverfahren mit Zwangsumlauf für die Lufteinlasshaube eines Strahltriebwerkes und Vorrichtung zur Durchführung des Verfahrens Expired - Lifetime DE60202540T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0102090A FR2820716B1 (fr) 2001-02-15 2001-02-15 Procede de degivrage par circulation forcee d'un fluide, d'un capot d'entree d'air de moteur a reaction et dispositif pour sa mise en oeuvre
FR0102090 2001-02-15

Publications (2)

Publication Number Publication Date
DE60202540D1 true DE60202540D1 (de) 2005-02-17
DE60202540T2 DE60202540T2 (de) 2005-12-22

Family

ID=8860074

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60202540T Expired - Lifetime DE60202540T2 (de) 2001-02-15 2002-02-12 Enteisungverfahren mit Zwangsumlauf für die Lufteinlasshaube eines Strahltriebwerkes und Vorrichtung zur Durchführung des Verfahrens

Country Status (7)

Country Link
US (1) US6698691B2 (de)
EP (1) EP1232944B1 (de)
AT (1) ATE286828T1 (de)
CA (1) CA2371326C (de)
DE (1) DE60202540T2 (de)
ES (1) ES2236472T3 (de)
FR (1) FR2820716B1 (de)

Families Citing this family (70)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2820715B1 (fr) * 2001-02-15 2003-05-30 Eads Airbus Sa Procede de degivrage d'un capot d'entree d'air de moteur a reaction et dispositif pour sa mise en oeuvre
US20060032983A1 (en) * 2004-07-19 2006-02-16 Brand Joseph H Foreign object damage tolerant nacelle anti-icing system
US20060169532A1 (en) * 2005-02-03 2006-08-03 Patrick William P Acoustic liner with nonuniform impedance
FR2895554B1 (fr) * 2005-12-23 2008-03-21 Onera (Off Nat Aerospatiale) Corps poreux metallique propre a attenuer le bruit des turbines aeronautiques
US7823374B2 (en) * 2006-08-31 2010-11-02 General Electric Company Heat transfer system and method for turbine engine using heat pipes
US8387362B2 (en) * 2006-10-19 2013-03-05 Michael Ralph Storage Method and apparatus for operating gas turbine engine heat exchangers
US7797944B2 (en) * 2006-10-20 2010-09-21 United Technologies Corporation Gas turbine engine having slim-line nacelle
GB2442967B (en) * 2006-10-21 2011-02-16 Rolls Royce Plc An engine arrangement
US7870721B2 (en) * 2006-11-10 2011-01-18 United Technologies Corporation Gas turbine engine providing simulated boundary layer thickness increase
FR2908738B1 (fr) * 2006-11-16 2009-12-04 Airbus France Bord d'attaque d'aeronef.
WO2008104716A2 (fr) * 2007-02-20 2008-09-04 Airbus France Procede de realisation d ' un revetement pour le traitement acoustique et revetement ainsi obtenu
FR2912780B1 (fr) * 2007-02-20 2012-03-02 Airbus France Revetement pour le traitement acoustique incorporant une structure alveolaire avec une forme complexe
FR2912781B1 (fr) * 2007-02-20 2009-04-10 Airbus France Sas Revetement pour le traitement acoustique integrant la fonction de traitement du givre avec de l'air chaud
GB2447228B8 (en) * 2007-03-06 2009-03-04 Gkn Aerospace Services Ltd Thermal anti-icing system
US8408491B2 (en) * 2007-04-24 2013-04-02 United Technologies Corporation Nacelle assembly having inlet airfoil for a gas turbine engine
FR2917067B1 (fr) * 2007-06-08 2009-08-21 Airbus France Sas Revetement pour le traitement acoustique integrant la fonction de traitement du givre avec de l'air chaud
US7874137B2 (en) * 2007-06-18 2011-01-25 Honeywell International Inc. Gas turbine engine anti-ice formation device and system
US8402739B2 (en) 2007-06-28 2013-03-26 United Technologies Corporation Variable shape inlet section for a nacelle assembly of a gas turbine engine
US9004399B2 (en) 2007-11-13 2015-04-14 United Technologies Corporation Nacelle flow assembly
FR2924409B1 (fr) * 2007-12-03 2010-05-14 Airbus France Nacelle d'aeronef comprenant des moyens d'evacuations d'air chaud
US8192147B2 (en) * 2007-12-14 2012-06-05 United Technologies Corporation Nacelle assembly having inlet bleed
US8186942B2 (en) * 2007-12-14 2012-05-29 United Technologies Corporation Nacelle assembly with turbulators
FR2925463B1 (fr) 2007-12-21 2010-04-23 Airbus France Structure pour le traitement acoustique plus particulierement adaptee a une entree d'air d'une nacelle d'aeronef
FR2925878B1 (fr) * 2007-12-28 2010-04-23 Airbus France Ensemble propulsif d'aeronef comprenant des systemes de prelevement d'air chaud
DE102008019146A1 (de) * 2008-04-16 2009-11-05 Airbus Deutschland Gmbh Enteisungssystem für ein Flugzeug
US8052089B2 (en) * 2008-11-03 2011-11-08 The Boeing Company Anti-icing apparatus for honeycomb structures
EP2393648B1 (de) 2009-02-03 2012-11-07 Airbus Opérations SAS Verfahren zur herstlelung eines abflussrohrnetzwerkes für eine akustische verarbeitungsplatte
FR2950325B1 (fr) * 2009-09-23 2011-09-09 Airbus Operations Sas Panneau pour le traitement acoustique plus particulierement adapte a une entree d'air d'une nacelle d'aeronef
WO2010089496A1 (fr) 2009-02-03 2010-08-12 Airbus Operations Sas Panneau pour le traitement acoustique plus particulierement adapte a une entree d'air d'une nacelle d'aeronef
FR2950289B1 (fr) * 2009-09-23 2012-06-01 Airbus Operations Sas Procede de fabrication d'un reseau de conduits de drainage
FR2941676B1 (fr) * 2009-02-03 2011-02-18 Airbus France Panneau pour le traitement acoustique plus particulierement adapte a une entree d'air d'une nacelle d'aeronef.
FR2951436B1 (fr) * 2009-10-15 2011-12-09 Airbus Operations Sas Mat d'accrochage de turbomoteur d'aeronef a canalisations d'air chaud concentriques
FR2954279B1 (fr) * 2009-12-18 2014-08-22 Airbus Operations Sas Entree d'air d'une nacelle d'aeronef integrant des moyens d'injection en air chaud pour le traitement du givre optimises
US8382039B2 (en) * 2009-12-30 2013-02-26 MRA Systems Inc. Turbomachine nacelle and anti-icing system and method therefor
FR2968636B1 (fr) * 2010-12-09 2013-01-18 Airbus Operations Sas Entree d'air pour ensemble propulsif d'aeronef a structure resistante aux surpressions et procede de reparation d'une entree d'air d'ensemble propulsif d'aeronef
CN102182559A (zh) * 2011-05-04 2011-09-14 中国航空工业集团公司西安飞机设计研究所 一种带预冷和回热功能的进气道防冰系统
FR2976556B1 (fr) * 2011-06-17 2013-12-27 Airbus Operations Sas Entree d'air d'une nacelle d'aeronef incorporant une levre renforcee avec un systeme de degivrage par effet joule
FR2980776B1 (fr) * 2011-10-03 2014-08-22 Airbus Operations Sas Nacelle d'aeronef comportant un panneau pour le traitement acoustique integrant des canaux d'air chaud et au moins un canal annulaire
FR2981049B1 (fr) * 2011-10-07 2014-04-11 Aircelle Sa Procede de fabrication d'un panneau d'absorption acoustique
DE102012003902A1 (de) * 2011-12-14 2013-06-20 Istvan Bolgar Einlauf für eine Gasturbine
GB201121887D0 (en) * 2011-12-20 2012-02-01 Rolls Royce Plc Intake liner for a gas turbine engine
US8985513B2 (en) * 2013-06-17 2015-03-24 The Boeing Company Honeycomb cores with splice joints and methods of assembling honeycomb cores
WO2015130384A2 (en) * 2013-12-16 2015-09-03 United Technologies Corporation Fan nacelle inlet flow control
US9488067B2 (en) * 2014-01-14 2016-11-08 The Boeing Company Aircraft anti-icing systems having deflector vanes
EP3094845B1 (de) * 2014-01-15 2020-04-29 United Technologies Corporation Kühlsysteme für gasturbinenmotoren
FR3023538B1 (fr) * 2014-07-11 2016-07-15 Aircelle Sa Levre avant de nacelle de turboreacteur comportant des percages d’air chaud en amont de panneaux acoustiques
FR3024494B1 (fr) * 2014-07-31 2016-07-22 Airbus Operations Sas Turbomachine d'aeronef comprenant un deflecteur
US10486821B2 (en) * 2015-07-07 2019-11-26 The Boeing Company Jet engine anti-icing and noise-attenuating air inlets
US10723464B2 (en) * 2015-08-26 2020-07-28 Rohr, Inc. Injector nozzle configuration for swirl anti-icing system
FR3041937B1 (fr) * 2015-10-05 2017-10-20 Airbus Operations Sas Structure compartimentee pour le traitement acoustique et le degivrage d'une nacelle d'aeronef et nacelle d'aeronef incorporant ladite structure
US9845728B2 (en) 2015-10-15 2017-12-19 Rohr, Inc. Forming a nacelle inlet for a turbine engine propulsion system
US10189572B2 (en) * 2016-05-02 2019-01-29 The Boeing Company Systems and methods for preventing ice formation on portions of an aircraft
US10708979B2 (en) 2016-10-07 2020-07-07 De-Ice Technologies Heating a bulk medium
EP3351702A4 (de) * 2016-10-31 2019-04-10 Yue Zhang Metallplatte mit sandwichartig darin angeordneten hohlrohren und deren verwendung
US10569495B2 (en) * 2017-05-08 2020-02-25 The Boeing Company Composite structure assembly having a conformable core
FR3070674B1 (fr) * 2017-09-06 2019-09-13 Safran Nacelles Integration a la levre acoustique degivree
FR3077800B1 (fr) * 2018-02-12 2020-09-25 Safran Nacelles Dispositif de degivrage et de traitement acoustique pour une levre d’entree d’air d’une nacelle de turboreacteur
US11433990B2 (en) 2018-07-09 2022-09-06 Rohr, Inc. Active laminar flow control system with composite panel
US11524770B2 (en) 2018-09-28 2022-12-13 Rohr, Inc. Active laminar flow control plenum panel arrangements and installation methods
US11414203B2 (en) * 2018-09-28 2022-08-16 Rohr, Inc. Active laminar flow control plenum panel arrangement
US11396366B2 (en) 2018-09-28 2022-07-26 Rohr, Inc. Active laminar flow control structural plenums fastened
FR3086786B1 (fr) * 2018-10-01 2020-12-18 Airbus Operations Sas Procede de fabrication d'une peau acoustique degivrante pour panneau acoustique d'aeronef, utilisant un dispositif d'ecartement de fibres
US11084600B2 (en) 2018-10-03 2021-08-10 Rohr, Inc. Nacelle inlet with reinforcement structure
EP3632791B1 (de) * 2018-10-03 2022-04-20 Rohr, Inc. Gondeleinlass mit verstärkungsstruktur
US11440665B2 (en) * 2018-10-23 2022-09-13 Airbus Operations Gmbh Vented leading-edge assembly and method for manufacturing a vented leading-edge assembly
FR3092619B1 (fr) * 2019-02-08 2021-03-19 Safran Nacelles Entrée d'air d'une nacelle de turboréacteur d'aéronef comportant des ouvertures de ventilation d’un flux d’air chaud de dégivrage
US11325716B2 (en) 2019-05-24 2022-05-10 Rohr, Inc. Inlet bulkhead with ventilation groove
FR3096662B1 (fr) 2019-05-27 2022-08-12 Safran Nacelles Lèvre d’entrée d’air de nacelle de turbomachine comprenant un dispositif acoustique et procédé de fabrication d’une telle lèvre
US20210163141A1 (en) * 2019-11-28 2021-06-03 Pratt & Whitney Canada Corp. Gas turbine engine, nacelle thereof, and associated method of operating a gas turbine engine
US20240077018A1 (en) * 2022-09-02 2024-03-07 Rohr, Inc. Thermal anti-icing system for an aircraft propulsion system

Family Cites Families (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3612173A (en) * 1969-01-10 1971-10-12 Ilg Ind Inc Unit heater device
US3821999A (en) * 1972-09-05 1974-07-02 Mc Donnell Douglas Corp Acoustic liner
US3820628A (en) * 1972-10-02 1974-06-28 United Aircraft Corp Sound suppression means for rotating machinery
US3917193A (en) * 1974-01-21 1975-11-04 Boeing Co Boundary layer control and anti-icing apparatus for an aircraft wing
US3890060A (en) 1974-02-15 1975-06-17 Gen Electric Acoustic duct with asymmetric acoustical treatment
US3910374A (en) * 1974-03-18 1975-10-07 Rohr Industries Inc Low frequency structural acoustic attenuator
US3948346A (en) * 1974-04-02 1976-04-06 Mcdonnell Douglas Corporation Multi-layered acoustic liner
US3933327A (en) * 1974-08-30 1976-01-20 Rohr Industries, Inc. Aircraft anti-icing plenum
US4522859A (en) * 1979-10-29 1985-06-11 Rohr Industries, Inc. Method of manufacture of honeycomb noise attenuation structure for high temperature applications
US4482114A (en) * 1981-01-26 1984-11-13 The Boeing Company Integrated thermal anti-icing and environmental control system
US4475624A (en) * 1981-07-27 1984-10-09 Ltv Aerospace And Defense Company Honeycomb structure
FR2528384A1 (fr) * 1982-06-09 1983-12-16 Snecma Dispositif pour detecter et empecher la formation de glace sur des surfaces profilees
IL78786A0 (en) * 1985-06-03 1986-08-31 Short Brothers Plc Duct for hot air
US4743740A (en) * 1985-10-07 1988-05-10 Rohr Industries, Inc. Buried element deicer
US4749150A (en) * 1985-12-24 1988-06-07 Rohr Industries, Inc. Turbofan duct with noise suppression and boundary layer control
US4688745A (en) * 1986-01-24 1987-08-25 Rohr Industries, Inc. Swirl anti-ice system
US4738416A (en) * 1986-09-26 1988-04-19 Quiet Nacelle Corporation Nacelle anti-icing system
US4759513A (en) * 1986-09-26 1988-07-26 Quiet Nacelle Corporation Noise reduction nacelle
US4926963A (en) * 1987-10-06 1990-05-22 Uas Support, Inc. Sound attenuating laminate for jet aircraft engines
DE3813740A1 (de) * 1988-04-23 1989-11-02 Vorwerk Co Interholding Gewebe zur herstellung eines bauteils
US5088277A (en) * 1988-10-03 1992-02-18 General Electric Company Aircraft engine inlet cowl anti-icing system
US5011098A (en) * 1988-12-30 1991-04-30 The Boeing Company Thermal anti-icing system for aircraft
US5025888A (en) * 1989-06-26 1991-06-25 Grumman Aerospace Corporation Acoustic liner
US5041323A (en) * 1989-10-26 1991-08-20 Rohr Industries, Inc. Honeycomb noise attenuation structure
US5423658A (en) * 1993-11-01 1995-06-13 General Electric Company Active noise control using noise source having adaptive resonant frequency tuning through variable ring loading
US5415522A (en) * 1993-11-01 1995-05-16 General Electric Company Active noise control using noise source having adaptive resonant frequency tuning through stress variation
US5498127A (en) * 1994-11-14 1996-03-12 General Electric Company Active acoustic liner
US5590849A (en) * 1994-12-19 1997-01-07 General Electric Company Active noise control using an array of plate radiators and acoustic resonators
US5683062A (en) * 1995-02-27 1997-11-04 General Electric Company Aircraft anti-insect system
US5776579A (en) * 1996-03-28 1998-07-07 The Boeing Company Structural bonding with encapsulated foaming adhesive
GB2314887B (en) * 1996-07-02 2000-02-09 Rolls Royce Plc Ice protection for porous structure
US5702231A (en) 1996-08-09 1997-12-30 The Boeing Company Apparatus and method for reducing noise emissions from a gas turbine engine inlet
US5841079A (en) 1997-11-03 1998-11-24 Northrop Grumman Corporation Combined acoustic and anti-ice engine inlet liner
US6371411B1 (en) * 1999-11-23 2002-04-16 The Boeing Company Method and apparatus for aircraft inlet ice protection
FR2820715B1 (fr) * 2001-02-15 2003-05-30 Eads Airbus Sa Procede de degivrage d'un capot d'entree d'air de moteur a reaction et dispositif pour sa mise en oeuvre

Also Published As

Publication number Publication date
ES2236472T3 (es) 2005-07-16
EP1232944B1 (de) 2005-01-12
US6698691B2 (en) 2004-03-02
ATE286828T1 (de) 2005-01-15
CA2371326A1 (fr) 2002-08-15
EP1232944A1 (de) 2002-08-21
FR2820716A1 (fr) 2002-08-16
FR2820716B1 (fr) 2003-05-30
DE60202540T2 (de) 2005-12-22
CA2371326C (fr) 2009-09-01
US20020139899A1 (en) 2002-10-03

Similar Documents

Publication Publication Date Title
DE60202540D1 (de) Enteisungverfahren mit Zwangsumlauf für die Lufteinlasshaube eines Strahltriebwerkes und Vorrichtung zur Durchführung des Verfahrens
ATE518751T1 (de) Enteisungverfahren für die lufteinlasshaube eines strahltriebwerkes und vorrichtung zur durchführung des verfahrens
SE0301123D0 (sv) Förfarande för ventilering av en arbetsmaskin, och en sådan arbetsmaskin
DE60017063D1 (de) Heissluftabfuhrvorrichtung für die Lufteinlasshaube eines Strahltriebwerkes mit Enteisungskreislauf
CA2344128A1 (en) Method and apparatus for the cooling of jet-engine turbine casings
DE69104511T2 (de) Luftströmungsmengenmesser für Brennkraftmaschine.
DE59610030D1 (de) Filter, insbesondere luftfilter für die ansaugluft einer brennkraftmaschine
GB2288752B (en) Air filter, particularly for the intake air of an internal-combustion engine
DE69817127D1 (de) Heissluftabfuhrvorrichtung für die Lufteinlasshaube eines Strahltriebwerkes mit Enteisungskreislauf
IT8021936A0 (it) Presa d'aria ad asse incurvato per turbomotore a gas.
DE69934397D1 (de) Luftzufuhrsystem für brennkraftmaschine
DE69911630D1 (de) Lufteinlasskanalsystem für flugzeugtriebwerke
DE69803741T2 (de) Enteisungsvorrichtung für die Verkleidung des Lufteinlaufs eines Strahltriebwerkes
DE69622248D1 (de) Abgasrückführungssystem mit senkrecht zum Lufteinlasskanal angeordnetem Steuerventil
DE60200835D1 (de) Sekundärluftzuführung in das abgassystem eines verbrennungsmotors
DE60025981D1 (de) Einlassluftsteuerungsventil für Brennkraftmaschine und Verfahren zu seiner Herstellung
EP0962720A3 (de) Belüftungssystem für einen Raum zur Planarisierung
DE3763757D1 (de) Lufteinlauf zum testen eines flugtriebwerks.
DE59709685D1 (de) Lufteinlauf für Triebwerke
SE9402476D0 (sv) Device for an internal combustion engine
DE59813081D1 (de) Luftansaugkanalsystem für eine Brennkraftmaschine
ATE316873T1 (de) Belüftungs- und klimaanlage für ein kraftfahrzeug
SE0302356D0 (sv) Förfarande och anordning för avluftning av en förbränningsmotor
DE59300789D1 (de) Luftansaugkanalsystem für Brennkraftmaschinen.
EP1111209A3 (de) Abgasanlage für Kraftfahrzeuge

Legal Events

Date Code Title Description
8364 No opposition during term of opposition
R082 Change of representative

Ref document number: 1232944

Country of ref document: EP

Representative=s name: SPARING - ROEHL - HENSELER, 40237 DUESSELDORF, DE