FR2987401B1 - Procede pour maintenir une piece d'adaptation sur un carter tubulaire d'un turbomoteur, piece d'adaptation et systeme de maintien correspondants. - Google Patents

Procede pour maintenir une piece d'adaptation sur un carter tubulaire d'un turbomoteur, piece d'adaptation et systeme de maintien correspondants.

Info

Publication number
FR2987401B1
FR2987401B1 FR1251811A FR1251811A FR2987401B1 FR 2987401 B1 FR2987401 B1 FR 2987401B1 FR 1251811 A FR1251811 A FR 1251811A FR 1251811 A FR1251811 A FR 1251811A FR 2987401 B1 FR2987401 B1 FR 2987401B1
Authority
FR
France
Prior art keywords
adaptation part
turbomoteur
maintaining
tubular housing
holding system
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
FR1251811A
Other languages
English (en)
Other versions
FR2987401A1 (fr
Inventor
Antoine Jean Philippe Beaujard
Maryline Besnard
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 FR1251811A priority Critical patent/FR2987401B1/fr
Priority to PCT/FR2013/050409 priority patent/WO2013128123A1/fr
Priority to GB1415184.9A priority patent/GB2514064B/en
Priority to US14/380,470 priority patent/US9834312B2/en
Publication of FR2987401A1 publication Critical patent/FR2987401A1/fr
Application granted granted Critical
Publication of FR2987401B1 publication Critical patent/FR2987401B1/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
    • B64D27/40—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
    • F02C7/20—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
    • B64D27/10—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
    • 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
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00—Joints and connections
    • Y10T403/32—Articulated members
    • Y10T403/32114—Articulated members including static joint
    • Y10T403/32229—Articulate joint is a slide

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR1251811A 2012-02-28 2012-02-28 Procede pour maintenir une piece d'adaptation sur un carter tubulaire d'un turbomoteur, piece d'adaptation et systeme de maintien correspondants. Active FR2987401B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR1251811A FR2987401B1 (fr) 2012-02-28 2012-02-28 Procede pour maintenir une piece d'adaptation sur un carter tubulaire d'un turbomoteur, piece d'adaptation et systeme de maintien correspondants.
PCT/FR2013/050409 WO2013128123A1 (fr) 2012-02-28 2013-02-27 Procede pour maintenir une piece d'adaptation sur un carter tubulaire d'un turbomoteur, piece d'adaptation et systeme de maintien correspondants
GB1415184.9A GB2514064B (en) 2012-02-28 2013-02-27 Method for holding an adapting part on a tubular casing of a turbo-engine, and corresponding adapting part and holding system
US14/380,470 US9834312B2 (en) 2012-02-28 2013-02-27 Method for holding an adapter piece on a tubular housing of a turbo engine, and corresponding adapter piece and holding system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1251811A FR2987401B1 (fr) 2012-02-28 2012-02-28 Procede pour maintenir une piece d'adaptation sur un carter tubulaire d'un turbomoteur, piece d'adaptation et systeme de maintien correspondants.

Publications (2)

Publication Number Publication Date
FR2987401A1 FR2987401A1 (fr) 2013-08-30
FR2987401B1 true FR2987401B1 (fr) 2017-05-12

Family

ID=48014077

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1251811A Active FR2987401B1 (fr) 2012-02-28 2012-02-28 Procede pour maintenir une piece d'adaptation sur un carter tubulaire d'un turbomoteur, piece d'adaptation et systeme de maintien correspondants.

Country Status (4)

Country Link
US (1) US9834312B2 (fr)
FR (1) FR2987401B1 (fr)
GB (1) GB2514064B (fr)
WO (1) WO2013128123A1 (fr)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3010700B1 (fr) * 2013-09-18 2017-11-03 Snecma Dispositif de suspension d'un carter, turbomachine et ensemble propulsif
FR3013077B1 (fr) * 2013-11-08 2015-11-20 Snecma Turbomachine comportant des moyens de support d'au moins un equipement
FR3014414B1 (fr) 2013-12-11 2017-08-11 Airbus Operations Sas Partie de voilure d'aeronef comportant un support de fixation d'un dispositif de raccordement monte en translation
FR3032180B1 (fr) * 2015-01-30 2018-05-18 Airbus Operations Ensemble propulsif comportant un turboreacteur et un mat d'accrochage permettant une nouvelle distribution des efforts entre le turboreacteur et la voilure
FR3036442B1 (fr) * 2015-05-21 2021-07-16 Snecma Turbomachine comportant un systeme de ventilation
FR3041935B1 (fr) * 2015-10-05 2017-12-15 Airbus Operations Sas Ensemble moteur pour aeronef comprenant au moins deux attaches moteur arriere decalees axialement l'une de l'autre
FR3095233B1 (fr) * 2019-04-16 2021-03-12 Safran Aircraft Engines Carter d'échappement d'une turbomachine à l'aérodynamisme amélioré
FR3114129B1 (fr) 2020-09-14 2022-08-05 Safran Aircraft Engines Ensemble comportant une turbomachine d’aeronef et son pylone d’accrochage
FR3118992B1 (fr) 2021-01-21 2022-12-09 Safran Aircraft Engines Ensemble comportant une turbomachine d’aeronef et son pylone d’accrochage
FR3123323B1 (fr) 2021-05-27 2024-05-03 Safran Aircraft Engines Structure de liaison et de support d’une turbomachine a un pylone d’aeronef
FR3133375A1 (fr) * 2022-03-11 2023-09-15 Airbus Operations (S.A.S.) Ensemble de propulsion électrique compact comportant une attache moteur isostatique, aéronef comportant au moins un tel ensemble de propulsion électrique
US11859506B2 (en) 2022-05-17 2024-01-02 Pratt & Whitney Canada Corp. Mounting structure for a gas turbine engine case
FR3136010A1 (fr) * 2022-05-25 2023-12-01 Safran Aircraft Engines Procede de fabrication d’un carter annulaire de turbomachine

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2560854B1 (fr) * 1984-03-07 1986-09-12 Snecma Capotages structuraux participant a la rigidite d'ensemble d'un turboreacteur
GB2239678B (en) * 1989-12-08 1993-03-03 Rolls Royce Plc Gas turbine engine blade shroud assembly
US5127797A (en) * 1990-09-12 1992-07-07 United Technologies Corporation Compressor case attachment means
GB2271390B (en) * 1992-10-12 1995-07-05 Rolls Royce Plc Mounting for a gas turbine engine
US5303880A (en) * 1992-10-28 1994-04-19 General Electric Company Aircraft engine pin mount
US5452575A (en) * 1993-09-07 1995-09-26 General Electric Company Aircraft gas turbine engine thrust mount
US5927644A (en) * 1997-10-08 1999-07-27 General Electric Company Double failsafe engine mount
JP3600911B2 (ja) * 2001-01-25 2004-12-15 川崎重工業株式会社 環状燃焼器のライナ支持構造
FR2867155B1 (fr) * 2004-03-08 2007-06-29 Snecma Moteurs Suspension d'un moteur a la structure d'un avion
GB0507721D0 (en) * 2005-04-16 2005-05-25 Rolls Royce Plc Gas turbine engine mounting arrangement
GB0607991D0 (en) * 2006-04-22 2006-05-31 Rolls Royce Plc Aeroengine mounting
FR2915177B1 (fr) * 2007-04-20 2009-07-10 Airbus France Sa Dispositif d'accrochage de moteur d'aeronef et aeronef comportant au moins un tel dispositif
US8167237B2 (en) * 2008-03-21 2012-05-01 United Technologies Corporation Mounting system for a gas turbine engine
FR2933070B1 (fr) * 2008-06-25 2010-08-20 Snecma Systeme propulsif d'aeronef
US20130232768A1 (en) * 2012-03-12 2013-09-12 United Technologies Corporation Turbine engine case mount and dismount

Also Published As

Publication number Publication date
GB201415184D0 (en) 2014-10-08
GB2514064B (en) 2019-10-30
FR2987401A1 (fr) 2013-08-30
GB2514064A (en) 2014-11-12
US20150047370A1 (en) 2015-02-19
WO2013128123A1 (fr) 2013-09-06
US9834312B2 (en) 2017-12-05

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