FR2840879B1 - Dispositif et procede de protection contre la glace - Google Patents

Dispositif et procede de protection contre la glace

Info

Publication number
FR2840879B1
FR2840879B1 FR0306051A FR0306051A FR2840879B1 FR 2840879 B1 FR2840879 B1 FR 2840879B1 FR 0306051 A FR0306051 A FR 0306051A FR 0306051 A FR0306051 A FR 0306051A FR 2840879 B1 FR2840879 B1 FR 2840879B1
Authority
FR
France
Prior art keywords
protection device
ice protection
ice
protection
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
FR0306051A
Other languages
English (en)
Other versions
FR2840879A1 (fr
Inventor
Alan Linton
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
Short Brothers 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 Short Brothers PLC filed Critical Short Brothers PLC
Publication of FR2840879A1 publication Critical patent/FR2840879A1/fr
Application granted granted Critical
Publication of FR2840879B1 publication Critical patent/FR2840879B1/fr
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
    • B64D2033/0206—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising noise reduction means, e.g. acoustic liners
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR0306051A 2002-05-22 2003-05-20 Dispositif et procede de protection contre la glace Expired - Lifetime FR2840879B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB0211800.8A GB0211800D0 (en) 2002-05-22 2002-05-22 An ice protection system for aircraft structures

Publications (2)

Publication Number Publication Date
FR2840879A1 FR2840879A1 (fr) 2003-12-19
FR2840879B1 true FR2840879B1 (fr) 2005-08-05

Family

ID=9937209

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0306051A Expired - Lifetime FR2840879B1 (fr) 2002-05-22 2003-05-20 Dispositif et procede de protection contre la glace

Country Status (3)

Country Link
US (1) US6848656B2 (fr)
FR (1) FR2840879B1 (fr)
GB (2) GB0211800D0 (fr)

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FR2869360B1 (fr) * 2004-04-27 2006-07-14 Airbus France Sas Ensemble reducteur de bruit pour turboreacteur d'aeronef
US7137240B2 (en) * 2004-08-18 2006-11-21 Hamilton Sundstrand Corporation Inlet muff anti-icing system for an auxiliary power unit
EP1893484B1 (fr) * 2005-06-22 2010-11-03 Airbus Operations (S.A.S) Systeme d'anti-givrage et de degivrage de nacelle de moteur d'aeronef a tapis resistif
DE102006031330B4 (de) * 2005-07-14 2014-03-20 Goodrich Corp. Für Eis empfänglicher Abschnitt eines Flugzeugs, insbesondere Flugtriebwerk- Zelleneinlasslippe, umfassend ein Eisschutzsystem, Flugtriebwerk mit einer solchen Einlasslippe sowie ein Verfahren zum Schutz einer solchen Einlasslippe vor Vereisung
US7429166B2 (en) 2005-12-20 2008-09-30 General Electric Company Methods and apparatus for gas turbine engines
US7923668B2 (en) * 2006-02-24 2011-04-12 Rohr, Inc. Acoustic nacelle inlet lip having composite construction and an integral electric ice protection heater disposed therein
US7291815B2 (en) * 2006-02-24 2007-11-06 Goodrich Corporation Composite ice protection heater and method of producing same
US8962130B2 (en) * 2006-03-10 2015-02-24 Rohr, Inc. Low density lightning strike protection for use in airplanes
EP2013408B2 (fr) * 2006-05-02 2016-09-28 Rohr, Inc. Nacelles et ses composants utilisant des nanorenforcements
US20080166563A1 (en) 2007-01-04 2008-07-10 Goodrich Corporation Electrothermal heater made from thermally conducting electrically insulating polymer material
US8657567B2 (en) * 2007-05-29 2014-02-25 United Technologies Corporation Nacelle compartment plenum for bleed air flow delivery system
FR2924409B1 (fr) * 2007-12-03 2010-05-14 Airbus France Nacelle d'aeronef comprenant des moyens d'evacuations d'air chaud
US7900872B2 (en) * 2007-12-12 2011-03-08 Spirit Aerosystems, Inc. Nacelle inlet thermal anti-icing spray duct support system
US7837150B2 (en) * 2007-12-21 2010-11-23 Rohr, Inc. Ice protection system for a multi-segment aircraft component
ITMI20080886A1 (it) * 2008-05-15 2009-11-16 Alenia Aermacchi Spa Giunto per indurre elevate cadute di temperatura tra parti collegate su un velivolo
US9004407B2 (en) 2008-12-24 2015-04-14 Middle River Aircraft Systems Anti-icing system and method for preventing ice accumulation
FR2941675B1 (fr) * 2009-02-02 2012-08-17 Airbus France Nacelle d'aeronef comprenant un systeme de traitement acoustique optimise.
US9010084B2 (en) 2009-02-02 2015-04-21 Airbus Operations Sas Aircraft nacelle including an optimised acoustic processing system
FR2952032B1 (fr) * 2009-11-05 2012-04-06 Airbus Operations Sas Nacelle d'aeronef comprenant un systeme de traitement acoustique optimise
FR2943624B1 (fr) * 2009-03-27 2011-04-15 Airbus France Nacelle d'aeronef comportant une paroi exterieure renforcee
US8561934B2 (en) * 2009-08-28 2013-10-22 Teresa M. Kruckenberg Lightning strike protection
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
FR2954280B1 (fr) * 2009-12-18 2012-03-23 Airbus Operations Sas Entree d'air d'une nacelle d'aeronef comprenant un traitement du givre optimise
FR2954282B1 (fr) * 2009-12-22 2012-02-17 Airbus Operations Sas Nacelle incorporant un element de jonction entre une levre et un panneau d'attenuation acoustique
JP5582927B2 (ja) * 2010-08-30 2014-09-03 三菱重工業株式会社 航空機の防除氷システム及びこれを備える航空機
DE102012002132A1 (de) 2012-02-03 2013-08-08 Airbus Operations Gmbh Vereisungsschutzsystem für ein Flugzeug und Verfahren zum Betreiben eines Vereisungsschutzsystems
GB201406277D0 (en) 2014-04-08 2014-05-21 Rolls Royce Deutschland A gas turbine inlet
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
US10174633B2 (en) * 2015-10-30 2019-01-08 Rolls-Royce Corporation Containment hook for composite fan case
US10221765B2 (en) * 2016-08-26 2019-03-05 Honeywell International Inc. Anti-icing exhaust system
US10870491B2 (en) * 2017-07-20 2020-12-22 The Boeing Company Eductor driven anti-ice system
FR3087489B1 (fr) * 2018-10-18 2022-12-09 Airbus Operations Sas Partie anterieure de nacelle de groupe propulsif d'aeronef comportant une voie principale de propagation d'efforts entre une levre d'entree d'air et une peau arriere d'un panneau acoustique
US11220344B2 (en) * 2018-12-17 2022-01-11 Rohr, Inc. Anti-ice double walled duct system
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
FR3092620B1 (fr) 2019-02-08 2021-03-05 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
FR3092618B1 (fr) * 2019-02-08 2021-02-19 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
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
CN112977835B (zh) * 2021-05-11 2021-08-03 中国空气动力研究与发展中心低速空气动力研究所 一种防溢流装置
US11630016B2 (en) * 2021-08-20 2023-04-18 Pratt & Whitney Canada Corp. Pressure measurement system and method for operating same

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1161186A (en) * 1968-05-28 1969-08-13 Rolls Royce A Gas Turbine Ducted Fan Engine.
US3933327A (en) * 1974-08-30 1976-01-20 Rohr Industries, Inc. Aircraft anti-icing plenum
AU581684B2 (en) * 1984-10-08 1989-03-02 Short Brothers Plc Duct for hot air
US4738416A (en) * 1986-09-26 1988-04-19 Quiet Nacelle Corporation Nacelle anti-icing system
US5088277A (en) * 1988-10-03 1992-02-18 General Electric Company Aircraft engine inlet cowl anti-icing system
GB9120113D0 (en) 1991-09-20 1992-09-23 Short Brothers Plc Thermal antiicing of aircraft structures
US5257498A (en) * 1992-04-23 1993-11-02 United Technologies Corporation Efficient anti-ice exhaust vent
FR2771451B1 (fr) 1997-11-21 2000-04-14 Aerospatiale Dispositif de protection pour capot d'entree d'air de moteur a reaction, pourvu d'un systeme de degivrage
FR2771776B1 (fr) * 1997-12-02 2000-01-28 Aerospatiale Dispositif d'evacuation d'air chaud pour capot d'entree d'air de moteur a reaction, a circuit de degivrage
US6371411B1 (en) * 1999-11-23 2002-04-16 The Boeing Company Method and apparatus for aircraft inlet ice protection
FR2802573B1 (fr) * 1999-12-21 2002-02-15 Aerospatiale Matra Airbus Dispositif d'evacuation d'air chaud pour capot d'entree d'air de moteur a reaction, a circuit de degivrage
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
GB2391284A (en) 2004-02-04
US20040031878A1 (en) 2004-02-19
GB0311635D0 (en) 2003-06-25
US6848656B2 (en) 2005-02-01
GB0211800D0 (en) 2002-07-03
FR2840879A1 (fr) 2003-12-19
GB2391284B (en) 2005-11-16

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