FR3026137B1 - Element pour une turbomachine, telle par exemple qu'un turboreacteur ou un turbopropulseur d'avion - Google Patents

Element pour une turbomachine, telle par exemple qu'un turboreacteur ou un turbopropulseur d'avion Download PDF

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Publication number
FR3026137B1
FR3026137B1 FR1458900A FR1458900A FR3026137B1 FR 3026137 B1 FR3026137 B1 FR 3026137B1 FR 1458900 A FR1458900 A FR 1458900A FR 1458900 A FR1458900 A FR 1458900A FR 3026137 B1 FR3026137 B1 FR 3026137B1
Authority
FR
France
Prior art keywords
wall
turbomachine
turbopropulser
airborne
turbo
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
FR1458900A
Other languages
English (en)
Other versions
FR3026137A1 (fr
Inventor
Pierre Antoine Perse Erwan
Donatien Behaghel Laurent
Stephane Geyl
Yoann Guezel Yvan
Cecile Thieriet
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
Safran Aircraft Engines SAS
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 Safran Aircraft Engines SAS, SNECMA SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1458900A priority Critical patent/FR3026137B1/fr
Priority to GB1704532.9A priority patent/GB2544706B/en
Priority to PCT/FR2015/052524 priority patent/WO2016046482A1/fr
Priority to US15/513,065 priority patent/US10604267B2/en
Priority to CN201580050827.6A priority patent/CN107074371B/zh
Publication of FR3026137A1 publication Critical patent/FR3026137A1/fr
Application granted granted Critical
Publication of FR3026137B1 publication Critical patent/FR3026137B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • 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
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
    • 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
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
    • F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
    • 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
    • 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
    • B64D27/406—Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Connection Of Plates (AREA)

Abstract

L'invention concerne un élément (3) pour une turbomachine (1), comportant une paroi (11) et au moins un organe (17) en charge s'étendant sensiblement perpendiculairement à la paroi (11), ledit organe (17) étant destiné à être fixé sur un support (18) servant à la fixation sur une partie structurelle d'un aéronef, caractérisé en ce qu'un organe de protection thermique (23) entoure ledit organe (17), ledit organe de protection thermique (23) comprenant une base (24) en appui souple sur la paroi (11) de l'élément (3), ladite base épousant la forme de ladite paroi et au moins une partie de couverture (26) qui entoure ledit organe en charge.
FR1458900A 2014-09-22 2014-09-22 Element pour une turbomachine, telle par exemple qu'un turboreacteur ou un turbopropulseur d'avion Active FR3026137B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR1458900A FR3026137B1 (fr) 2014-09-22 2014-09-22 Element pour une turbomachine, telle par exemple qu'un turboreacteur ou un turbopropulseur d'avion
GB1704532.9A GB2544706B (en) 2014-09-22 2015-09-21 Turbine engine, such as for example an aircraft turbojet engine or a turboprop engine.
PCT/FR2015/052524 WO2016046482A1 (fr) 2014-09-22 2015-09-21 Turbomachine, telle par exemple qu'un turboréacteur ou un turbopropulseur d'avion
US15/513,065 US10604267B2 (en) 2014-09-22 2015-09-21 Turbine engine including a thermal protection member
CN201580050827.6A CN107074371B (zh) 2014-09-22 2015-09-21 涡轮发动机，诸如航空器涡轮喷气发动机或涡轮螺旋桨发动机

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1458900 2014-09-22
FR1458900A FR3026137B1 (fr) 2014-09-22 2014-09-22 Element pour une turbomachine, telle par exemple qu'un turboreacteur ou un turbopropulseur d'avion

Publications (2)

Publication Number Publication Date
FR3026137A1 FR3026137A1 (fr) 2016-03-25
FR3026137B1 true FR3026137B1 (fr) 2019-03-15

Family

ID=52007105

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1458900A Active FR3026137B1 (fr) 2014-09-22 2014-09-22 Element pour une turbomachine, telle par exemple qu'un turboreacteur ou un turbopropulseur d'avion

Country Status (5)

Country Link
US (1) US10604267B2 (fr)
CN (1) CN107074371B (fr)
FR (1) FR3026137B1 (fr)
GB (1) GB2544706B (fr)
WO (1) WO2016046482A1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3075174B1 (fr) * 2017-12-18 2020-12-11 Safran Aircraft Engines Structure porteuse destinee au montage sur un generateur de gaz
FR3075175B1 (fr) * 2017-12-20 2019-12-13 Safran Aircraft Engines Dispositif de suspension

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB759629A (en) * 1953-11-05 1956-10-24 Bristol Aeroplane Co Ltd Improvements in or relating to installation arrangements for gas turbine engines
US20030111238A1 (en) * 2001-12-14 2003-06-19 Anderson Stephen Arthur Flame arresting blankets on gas turbine
FR2868041B1 (fr) * 2004-03-25 2006-05-26 Snecma Moteurs Sa Suspension d'un moteur d'avion
FR2869874B1 (fr) * 2004-05-04 2006-06-23 Snecma Moteurs Sa Moteur d'avion avec des moyens de suspension a la structure d'un avion
FR2894934B1 (fr) * 2005-12-15 2009-11-13 Airbus France Attache arriere d'un moteur d'aeronef avec manille en attente et ressort pour un tel axe en attente
US7918081B2 (en) * 2006-12-19 2011-04-05 United Technologies Corporation Flame prevention device
US20080169038A1 (en) * 2007-01-11 2008-07-17 Timothy David Sellis Thermal shield and methods of construction and installation
FR2941673B1 (fr) * 2009-02-04 2011-01-14 Aircelle Sa Ensemble de suspension pour turboreacteur d'aeronef
FR2952614B1 (fr) * 2009-11-17 2012-02-03 Snecma Poutre de suspension d'un turbomoteur a la structure d'un aeronef, utilisation de la poutre et aeronef
FR2964737B1 (fr) * 2010-09-14 2013-05-31 Airbus Operations Sas Procede de mesure d'efforts dans des jonctions en environnement haute temperature et axe instrumente de mise en oeuvre, en particulier pour attache arriere de turboreacteur d'aeronef
FR2973339B1 (fr) * 2011-03-29 2014-08-22 Snecma Dispositif de suspension d'une turbomachine a un avion
FR2996823B1 (fr) * 2012-10-15 2014-11-21 Snecma Protection thermique demontable en ligne pour un palonnier de suspension d'une turbomachine

Also Published As

Publication number Publication date
WO2016046482A1 (fr) 2016-03-31
GB2544706B (en) 2020-09-30
GB2544706A (en) 2017-05-24
CN107074371B (zh) 2020-03-20
US10604267B2 (en) 2020-03-31
GB201704532D0 (en) 2017-05-03
CN107074371A (zh) 2017-08-18
US20170291713A1 (en) 2017-10-12
FR3026137A1 (fr) 2016-03-25

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