FR3010700B1 - Dispositif de suspension d'un carter, turbomachine et ensemble propulsif - Google Patents

Dispositif de suspension d'un carter, turbomachine et ensemble propulsif

Info

Publication number
FR3010700B1
FR3010700B1 FR1358981A FR1358981A FR3010700B1 FR 3010700 B1 FR3010700 B1 FR 3010700B1 FR 1358981 A FR1358981 A FR 1358981A FR 1358981 A FR1358981 A FR 1358981A FR 3010700 B1 FR3010700 B1 FR 3010700B1
Authority
FR
France
Prior art keywords
turbomachine
carter
suspending
propulsive assembly
propulsive
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
FR1358981A
Other languages
English (en)
Other versions
FR3010700A1 (fr
Inventor
Maria Natal
Arnaud Ple
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 FR1358981A priority Critical patent/FR3010700B1/fr
Priority to US14/489,649 priority patent/US10071812B2/en
Priority to GB1416537.7A priority patent/GB2520395B/en
Publication of FR3010700A1 publication Critical patent/FR3010700A1/fr
Application granted granted Critical
Publication of FR3010700B1 publication Critical patent/FR3010700B1/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
    • 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
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • B64D27/12—Aircraft characterised by the type or position of power plants of gas-turbine 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
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • 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
    • B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • F01D25/285—Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures
    • 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
    • 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
    • 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
    • F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
    • F16M1/00—Frames or casings of engines, machines or apparatus; Frames serving as machinery beds
    • F16M1/04—Frames or casings of engines, machines or apparatus; Frames serving as machinery beds for rotary engines or similar machines
    • 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
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Load-Engaging Elements For Cranes (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR1358981A 2013-09-18 2013-09-18 Dispositif de suspension d'un carter, turbomachine et ensemble propulsif Active FR3010700B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1358981A FR3010700B1 (fr) 2013-09-18 2013-09-18 Dispositif de suspension d'un carter, turbomachine et ensemble propulsif
US14/489,649 US10071812B2 (en) 2013-09-18 2014-09-18 Device for suspending a casing, a turbine engine and a propulsion assembly
GB1416537.7A GB2520395B (en) 2013-09-18 2014-09-18 Device for suspending a casing, a turbine engine and a propulsion assembly

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1358981A FR3010700B1 (fr) 2013-09-18 2013-09-18 Dispositif de suspension d'un carter, turbomachine et ensemble propulsif

Publications (2)

Publication Number Publication Date
FR3010700A1 FR3010700A1 (fr) 2015-03-20
FR3010700B1 true FR3010700B1 (fr) 2017-11-03

Family

ID=49753357

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1358981A Active FR3010700B1 (fr) 2013-09-18 2013-09-18 Dispositif de suspension d'un carter, turbomachine et ensemble propulsif

Country Status (3)

Country Link
US (1) US10071812B2 (fr)
FR (1) FR3010700B1 (fr)
GB (1) GB2520395B (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3057543B1 (fr) * 2016-10-14 2020-06-19 Safran Aircraft Engines Turbomachine a axes decales horizontalement
FR3097903B1 (fr) * 2019-06-28 2021-07-30 Safran Aircraft Engines Carter pour une turbomachine d’aeronef
US11643218B2 (en) * 2021-08-05 2023-05-09 Pratt & Whitney Canada Corp. AFT engine mount ring with spigot

Family Cites Families (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3155352A (en) * 1961-03-31 1964-11-03 United Aircraft Corp Mounting system for accessory case
US3543588A (en) * 1968-11-12 1970-12-01 Gen Motors Corp Accessory installation
US3688505A (en) * 1969-10-13 1972-09-05 Gen Motors Corp Ducted fan engine
US4044973A (en) * 1975-12-29 1977-08-30 The Boeing Company Nacelle assembly and mounting structures for a turbofan jet propulsion engine
DE69012071T2 (de) * 1989-12-05 1995-04-13 Rolls Royce Plc Ausfallsichere Haltevorrichtung für Treibwerke.
FR2677954B1 (fr) * 1991-06-19 1993-09-10 Snecma Structure de suspension arriere du carter d'echappement d'un turboreacteur.
US6260351B1 (en) 1998-12-10 2001-07-17 United Technologies Corporation Controlled spring rate gearbox mount
US6401448B1 (en) * 2000-08-31 2002-06-11 General Electric Company System for mounting aircraft engines
US6843449B1 (en) * 2004-02-09 2005-01-18 General Electric Company Fail-safe aircraft engine mounting system
US20060032974A1 (en) * 2004-08-16 2006-02-16 Honeywell International Inc. Modular installation kit for auxiliary power unit
US7500365B2 (en) 2005-05-05 2009-03-10 United Technologies Corporation Accessory gearbox
US8523516B2 (en) 2006-10-11 2013-09-03 Aircelle Bypass turbojet engine nacelle
US8950702B2 (en) * 2008-01-18 2015-02-10 United Technologies Corporation Pylon and engine mount configuration
FR2926788B1 (fr) 2008-01-25 2010-04-02 Snecma Fixation d'un turboreacteur multiflux a un aeronef
US8695920B2 (en) * 2008-06-02 2014-04-15 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US20140174056A1 (en) * 2008-06-02 2014-06-26 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US8800914B2 (en) * 2008-06-02 2014-08-12 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
FR2933070B1 (fr) * 2008-06-25 2010-08-20 Snecma Systeme propulsif d'aeronef
US8313293B2 (en) * 2009-05-15 2012-11-20 Pratt & Whitney Canada Corp. Turbofan mounting system
FR2950323B1 (fr) * 2009-09-22 2011-11-04 Airbus Operations Sas Mat d'accrochage de moteur d'aeronef, ensemble comprenant ce mat et aeronef associe
FR2952672B1 (fr) 2009-11-17 2011-12-09 Snecma Montage d'un boitier d'accessoires sur un carter intermediaire pour compartiment de soufflante de turboreacteur
GB201009548D0 (en) * 2010-06-08 2010-07-21 Rolls Royce Plc A mounting assembly
US8561501B2 (en) * 2011-05-31 2013-10-22 United Technologies Corporation Gearbox mount bracket
FR2981047B1 (fr) * 2011-10-06 2013-10-25 Aircelle Sa Ensemble propulsif d'aeronef
FR2986582B1 (fr) * 2012-02-06 2014-03-14 Snecma Carter de soufflante pour moteur a turbine a gaz munie d'une bride pour la fixation d'equipements
FR2987401B1 (fr) * 2012-02-28 2017-05-12 Snecma Procede pour maintenir une piece d'adaptation sur un carter tubulaire d'un turbomoteur, piece d'adaptation et systeme de maintien correspondants.
US9227734B2 (en) * 2012-08-31 2016-01-05 United Technologies Corporation Secondary load path for gas turbine engine
US10220950B2 (en) * 2013-03-15 2019-03-05 United Technologies Corporation Engine mount waiting fail safe lug joint with reduced dynamic amplification factor
GB201315968D0 (en) * 2013-09-09 2013-10-23 Rolls Royce Plc Aircraft engine mount
US10030541B2 (en) * 2015-07-01 2018-07-24 Rolls-Royce North American Technologies Inc. Turbine shroud with clamped flange attachment

Also Published As

Publication number Publication date
US10071812B2 (en) 2018-09-11
US20150075177A1 (en) 2015-03-19
GB2520395A (en) 2015-05-20
GB201416537D0 (en) 2014-11-05
GB2520395B (en) 2020-09-02
FR3010700A1 (fr) 2015-03-20

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