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FR2996823B1 - Protection thermique demontable en ligne pour un palonnier de suspension d'une turbomachine - Google Patents

Protection thermique demontable en ligne pour un palonnier de suspension d'une turbomachine

Info

Publication number
FR2996823B1
FR2996823B1 FR1259833A FR1259833A FR2996823B1 FR 2996823 B1 FR2996823 B1 FR 2996823B1 FR 1259833 A FR1259833 A FR 1259833A FR 1259833 A FR1259833 A FR 1259833A FR 2996823 B1 FR2996823 B1 FR 2996823B1
Authority
FR
France
Prior art keywords
turbomachine
line
thermal protection
suspension roll
detachable thermal
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.)
Active
Application number
FR1259833A
Other languages
English (en)
Other versions
FR2996823A1 (fr
Inventor
Lambert Olivier Marie Demoulin
Julien Pavillet
Guilhem Seize
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA 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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR1259833A priority Critical patent/FR2996823B1/fr
Priority to US14/053,862 priority patent/US9359954B2/en
Priority to GB1318247.2A priority patent/GB2510013B/en
Publication of FR2996823A1 publication Critical patent/FR2996823A1/fr
Application granted granted Critical
Publication of FR2996823B1 publication Critical patent/FR2996823B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
    • 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
    • F02C7/24—Heat or noise insulation
    • 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
    • F02C7/24—Heat or noise insulation
    • F02C7/25—Fire protection or prevention
    • 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
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Exhaust Silencers (AREA)
FR1259833A 2012-10-15 2012-10-15 Protection thermique demontable en ligne pour un palonnier de suspension d'une turbomachine Active FR2996823B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1259833A FR2996823B1 (fr) 2012-10-15 2012-10-15 Protection thermique demontable en ligne pour un palonnier de suspension d'une turbomachine
US14/053,862 US9359954B2 (en) 2012-10-15 2013-10-15 In-line removable heat shield for a turbomachine suspension yoke
GB1318247.2A GB2510013B (en) 2012-10-15 2013-10-15 In-line removable heat shield for a turbomachine suspension yoke

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1259833A FR2996823B1 (fr) 2012-10-15 2012-10-15 Protection thermique demontable en ligne pour un palonnier de suspension d'une turbomachine

Publications (2)

Publication Number Publication Date
FR2996823A1 FR2996823A1 (fr) 2014-04-18
FR2996823B1 true FR2996823B1 (fr) 2014-11-21

Family

ID=47428712

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1259833A Active FR2996823B1 (fr) 2012-10-15 2012-10-15 Protection thermique demontable en ligne pour un palonnier de suspension d'une turbomachine

Country Status (3)

Country Link
US (1) US9359954B2 (fr)
FR (1) FR2996823B1 (fr)
GB (1) GB2510013B (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018162811A1 (fr) 2017-03-06 2018-09-13 Psa Automobiles Sa Manchon de protection thermique de biellette anti-couple et biellette anti-couple équipée

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3014841B1 (fr) 2013-12-17 2017-12-08 Airbus Operations Sas Ensemble pour aeronef comprenant un corps d'attache moteur en partie realise d'une seule piece avec une nervure interieure de rigidification d'un caisson de mat d'accrochage
FR3014840B1 (fr) 2013-12-17 2017-10-13 Airbus Operations Sas Ensemble pour aeronef comprenant un corps d'attache moteur equipe d'au moins une ferrure de support de manille penetrant dans le caisson du mat d'accrochage
FR3015431B1 (fr) * 2013-12-19 2017-12-15 Airbus Operations Sas Structure primaire de mat d'accrochage renforcee.
FR3015433B1 (fr) 2013-12-23 2016-02-12 Airbus Operations Sas Ensemble pour aeronef comprenant un mat d'accrochage integre a la nacelle et agence en partie arriere du fuselage
FR3026137B1 (fr) * 2014-09-22 2019-03-15 Safran Aircraft Engines Element pour une turbomachine, telle par exemple qu'un turboreacteur ou un turbopropulseur d'avion
FR3073825B1 (fr) * 2017-11-20 2019-12-20 Safran Aircraft Engines Piece de protection d'une chape de suspension d'un carter de moteur d'aeronef
CN108868992B (zh) * 2018-07-19 2024-03-19 浙江零跑科技股份有限公司 一种隔热罩
FR3090041B1 (fr) * 2018-12-14 2020-11-27 Safran Aircraft Engines Dispositif de resistance au feu ameliore destine a etre interpose entre une extremite de mat d’accrochage de turbomachine d’aeronef, et un capotage de la turbomachine delimitant un compartiment inter-veine
FR3106126B1 (fr) * 2020-01-10 2022-01-07 Safran Aircraft Engines Assemblage entre un pylône d’aéronef et une turbomachine

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2635751B1 (fr) * 1988-09-01 1991-01-04 Snecma Dispositif de fixation d'une biellette de suspension d'un turboreacteur
GB9125011D0 (en) * 1991-11-25 1992-01-22 Rolls Royce Plc A mounting arrangement for a gas turbine engine
US5910094A (en) * 1996-09-10 1999-06-08 The Boeing Company Aircraft labyrinth fire seal
EP1284390A1 (fr) * 2001-06-27 2003-02-19 Siemens Aktiengesellschaft Ensemble bouclier thermique pour un composant acheminant un gaz chaud, notamment pour des pièces de structure de turbines à gaz
GB2459483B (en) * 2008-04-24 2010-06-30 Rolls Royce Plc Engine mounting arrangement
EP2382130B1 (fr) * 2009-01-26 2017-09-27 LORD Corporation Systeme d'accrochage d'un moteur d'aéronef et procede d'accrochage de moteur d'aéronef
US9534783B2 (en) * 2011-07-21 2017-01-03 United Technologies Corporation Insert adjacent to a heat shield element for a gas turbine engine combustor
FR2983172B1 (fr) * 2011-11-25 2014-05-16 Airbus Operations Sas Carenage arriere pour mat d'accrochage d'un moteur

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018162811A1 (fr) 2017-03-06 2018-09-13 Psa Automobiles Sa Manchon de protection thermique de biellette anti-couple et biellette anti-couple équipée

Also Published As

Publication number Publication date
GB201318247D0 (en) 2013-11-27
GB2510013A (en) 2014-07-23
US9359954B2 (en) 2016-06-07
US20140102114A1 (en) 2014-04-17
FR2996823A1 (fr) 2014-04-18
GB2510013B (en) 2020-04-29

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