DE69803741T2 - Enteisungsvorrichtung für die Verkleidung des Lufteinlaufs eines Strahltriebwerkes - Google Patents

Enteisungsvorrichtung für die Verkleidung des Lufteinlaufs eines Strahltriebwerkes

Info

Publication number
DE69803741T2
DE69803741T2 DE69803741T DE69803741T DE69803741T2 DE 69803741 T2 DE69803741 T2 DE 69803741T2 DE 69803741 T DE69803741 T DE 69803741T DE 69803741 T DE69803741 T DE 69803741T DE 69803741 T2 DE69803741 T2 DE 69803741T2
Authority
DE
Germany
Prior art keywords
cladding
air intake
jet engine
deicing device
deicing
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
DE69803741T
Other languages
English (en)
Other versions
DE69803741D1 (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.)
Aerospatiale Matra
Original Assignee
Aerospatiale Matra
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 Aerospatiale Matra filed Critical Aerospatiale Matra
Application granted granted Critical
Publication of DE69803741D1 publication Critical patent/DE69803741D1/de
Publication of DE69803741T2 publication Critical patent/DE69803741T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L27/00—Adjustable joints, Joints allowing movement
    • F16L27/12—Adjustable joints, Joints allowing movement allowing substantial longitudinal adjustment or movement
    • F16L27/125—Adjustable joints, Joints allowing movement allowing substantial longitudinal adjustment or movement having longitudinal and rotary movement
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/047—Heating to prevent icing
    • 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
    • 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
    • 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
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
  • Motor Or Generator Cooling System (AREA)
DE69803741T 1997-11-21 1998-11-19 Enteisungsvorrichtung für die Verkleidung des Lufteinlaufs eines Strahltriebwerkes Expired - Lifetime DE69803741T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9714611A FR2771452B1 (fr) 1997-11-21 1997-11-21 Dispositif de degivrage pour capot d'entree d'air de moteur a reaction

Publications (2)

Publication Number Publication Date
DE69803741D1 DE69803741D1 (de) 2002-03-21
DE69803741T2 true DE69803741T2 (de) 2002-09-26

Family

ID=9513628

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69803741T Expired - Lifetime DE69803741T2 (de) 1997-11-21 1998-11-19 Enteisungsvorrichtung für die Verkleidung des Lufteinlaufs eines Strahltriebwerkes

Country Status (5)

Country Link
US (1) US6193192B1 (de)
EP (1) EP0918150B1 (de)
DE (1) DE69803741T2 (de)
ES (1) ES2172103T3 (de)
FR (1) FR2771452B1 (de)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6709024B1 (en) 2000-09-27 2004-03-23 General Electric Company Method and apparatus for assembling couplings for transferring fluids
FR2886674B1 (fr) * 2005-06-07 2007-08-03 Airbus France Sas Systeme pour le degivrage du bord d'attaque d'un capot d'entree d'air pour turbomoteur
FR2887294B1 (fr) * 2005-06-21 2007-08-10 Airbus France Sas Systeme pour le degivrage du bord d'attaque d'un capot d'entree d'air pour turbomoteur
FR2898867B1 (fr) * 2006-03-27 2008-12-19 Airbus France Sas Systeme pour le degivrage d'un capot d'entree d'air pour turbomoteur.
GB2440133A (en) * 2006-07-18 2008-01-23 Gkn Aerospace Transparency Sys A de-icing heated leading edge component of an aircraft
FR2921901B1 (fr) * 2007-10-08 2011-03-18 Aircelle Sa Structure d'entree d'air apte a etre montee en amont d'une structure mediane de nacelle pour moteur d'aeronef, et nacelle equipee d'une telle structure d'entree d'air
US20090108134A1 (en) * 2007-10-25 2009-04-30 General Electric Company Icing protection system and method for enhancing heat transfer
US7975966B2 (en) * 2008-02-04 2011-07-12 Embraer - Empresa Brasileira De Aeronautica S.A. Icing protection for aircraft air inlet scoops
FR2927882B1 (fr) * 2008-02-27 2010-02-12 Aircelle Sa Structure d'entree d'air pour une nacelle d'un aeronef
FR2928695B1 (fr) * 2008-03-13 2012-06-29 Aircelle Sa Dispositif d'acheminement d'air sous pression entre un moteur d'aeronef et un compartiment de degivrage d'une structure d'entree d'air de nacelle
GB0812562D0 (en) * 2008-07-10 2008-08-13 Airbus Uk Ltd A Connector for an aircraft fuel pipe
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
FR2957586B1 (fr) * 2010-03-18 2012-04-27 Airbus Operations Sas Dispositif de degivrage comprenant des moyens pour detecter une fuite au niveau d'une alimentation en air chaud
FR2975435B1 (fr) * 2011-05-16 2016-09-02 Snecma Dispositif de degivrage d'un bec de separation de turbomachine
ES2424064B1 (es) * 2012-03-23 2014-07-16 Juan Francisco LÓPEZ GIL Apertura de sobres con facilidad
US9528442B2 (en) * 2013-08-21 2016-12-27 The Boeing Company Aircraft engine anti-icing (EAI) barrier assembly, system and method
US10138811B2 (en) * 2014-03-13 2018-11-27 The Boeing Company Enhanced temperature control anti-ice nozzle
BE1023289B1 (fr) 2015-07-17 2017-01-24 Safran Aero Boosters S.A. Bec de separation de compresseur basse pression de turbomachine axiale avec conduit annulaire de degivrage
US10625871B1 (en) * 2015-08-24 2020-04-21 Roller Bearing Company Of America, Inc. Dynamic movement tube connection system
US10267334B2 (en) * 2016-08-01 2019-04-23 United Technologies Corporation Annular heatshield
US10708979B2 (en) 2016-10-07 2020-07-07 De-Ice Technologies Heating a bulk medium
RU177304U1 (ru) * 2017-08-29 2018-02-15 Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") Труба подвода горячего воздуха к противообледенительной системе
FR3072421B1 (fr) * 2017-10-18 2019-09-27 Airbus Operations Levre d'entree d'air d'un moteur d'aeronef comportant un systeme de degivrage
FR3087477A1 (fr) * 2018-10-22 2020-04-24 Safran Aircraft Engines Dispositif de degivrage d'un bec de turbomachine
US11220344B2 (en) * 2018-12-17 2022-01-11 Rohr, Inc. Anti-ice double walled duct system
US11325716B2 (en) * 2019-05-24 2022-05-10 Rohr, Inc. Inlet bulkhead with ventilation groove

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2657076A (en) * 1950-05-19 1953-10-27 Ryan Aeronautical Co Flexible joint for tubes
US2836436A (en) * 1955-01-24 1958-05-27 R L A P I Soc Coupling joined by fluid-pressure-deformed packing
US2931672A (en) * 1956-06-05 1960-04-05 George W Merritt Flexible duct mounting
CH417245A (de) * 1964-05-22 1966-07-15 Jansen & Co Ag Muffenverbindung für Rohre, insbesondere für Kunststoffrohre
US3339832A (en) * 1965-08-19 1967-09-05 Gen Electric Pipe connections for aircraft gas turbine engines
US3502356A (en) * 1967-11-02 1970-03-24 Hancock Brick & Tile Co Plain end sewer pipes and coupling for same
US3596934A (en) * 1969-05-06 1971-08-03 Herbert A De Cenzo Flexible fluidtight coupling for tubes
US4522433A (en) * 1982-05-14 1985-06-11 Stanley Aviation Corporation Spherical seat flexible O-ring coupling
US4733890A (en) * 1984-07-09 1988-03-29 Stratoflex, Inc. Formed fluid coupling apparatus
AU581684B2 (en) * 1984-10-08 1989-03-02 Short Brothers Plc Duct for hot air
FR2621554B1 (fr) * 1987-10-07 1990-01-05 Snecma Capot d'entree non tournant de turboreacteur a fixation centrale et turboreacteur ainsi equipe
US5106129A (en) * 1990-10-09 1992-04-21 Delaware Capital Formation, Inc. Flexible coupling for transferring a fluid between two fluid conduits
GB9120113D0 (en) * 1991-09-20 1992-09-23 Short Brothers Plc Thermal antiicing of aircraft structures
US5127681A (en) * 1991-12-09 1992-07-07 Aeroquip Corporation Flexible connector
US5772254A (en) * 1995-12-20 1998-06-30 Eg&G Pressure Science, Inc. Modular joint, with a replaceable sealing sleeve

Also Published As

Publication number Publication date
EP0918150A1 (de) 1999-05-26
ES2172103T3 (es) 2002-09-16
EP0918150B1 (de) 2002-02-06
US6193192B1 (en) 2001-02-27
FR2771452A1 (fr) 1999-05-28
DE69803741D1 (de) 2002-03-21
FR2771452B1 (fr) 2000-04-14

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