PL2805029T3 - Obsada do co najmniej jednego łożyska części gorącej silnika turbinowego, i odpowiadający jej silnik turbinowy - Google Patents

Obsada do co najmniej jednego łożyska części gorącej silnika turbinowego, i odpowiadający jej silnik turbinowy

Info

Publication number
PL2805029T3
PL2805029T3 PL13704149T PL13704149T PL2805029T3 PL 2805029 T3 PL2805029 T3 PL 2805029T3 PL 13704149 T PL13704149 T PL 13704149T PL 13704149 T PL13704149 T PL 13704149T PL 2805029 T3 PL2805029 T3 PL 2805029T3
Authority
PL
Poland
Prior art keywords
turboengine
bearing
support
hot section
hot
Prior art date
Application number
PL13704149T
Other languages
English (en)
Inventor
Jean-François Perronnet
Jean-Luc Breining
Manuel Silva
Original Assignee
Turbomeca
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 Turbomeca filed Critical Turbomeca
Publication of PL2805029T3 publication Critical patent/PL2805029T3/pl

Links

Classifications

    • 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
    • F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
    • F01D25/162—Bearing supports
    • 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/10—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor
    • F02C3/103—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor the compressor being of the centrifugal type
    • 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
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C35/00—Rigid support of bearing units; Housings, e.g. caps, covers
    • F16C35/02—Rigid support of bearing units; Housings, e.g. caps, covers in the case of sliding-contact bearings
    • 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)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mounting Of Bearings Or Others (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Support Of The Bearing (AREA)
  • Rolling Contact Bearings (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
PL13704149T 2012-01-20 2013-01-11 Obsada do co najmniej jednego łożyska części gorącej silnika turbinowego, i odpowiadający jej silnik turbinowy PL2805029T3 (pl)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1250574A FR2986040B1 (fr) 2012-01-20 2012-01-20 Support de palier de turbomachine
EP13704149.7A EP2805029B1 (fr) 2012-01-20 2013-01-11 Support pour au moins un palier de section chaude de turbomoteur, et turbomoteur associé
PCT/FR2013/050068 WO2013107966A1 (fr) 2012-01-20 2013-01-11 Support de palier de turbomachine

Publications (1)

Publication Number Publication Date
PL2805029T3 true PL2805029T3 (pl) 2016-05-31

Family

ID=47714388

Family Applications (1)

Application Number Title Priority Date Filing Date
PL13704149T PL2805029T3 (pl) 2012-01-20 2013-01-11 Obsada do co najmniej jednego łożyska części gorącej silnika turbinowego, i odpowiadający jej silnik turbinowy

Country Status (11)

Country Link
US (1) US9915173B2 (pl)
EP (1) EP2805029B1 (pl)
JP (1) JP5908608B2 (pl)
KR (1) KR102051160B1 (pl)
CN (1) CN104053865B (pl)
CA (1) CA2861738C (pl)
ES (1) ES2562229T3 (pl)
FR (1) FR2986040B1 (pl)
PL (1) PL2805029T3 (pl)
RU (1) RU2615888C2 (pl)
WO (1) WO2013107966A1 (pl)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104948301A (zh) * 2015-05-20 2015-09-30 西安交通大学 一种燃气轮机的热端支承
US11174786B2 (en) * 2016-11-15 2021-11-16 General Electric Company Monolithic superstructure for load path optimization
US20200080435A1 (en) * 2018-09-10 2020-03-12 Pratt & Whitney Canada Corp. Turbine exhaust structure for a gas turbine engine
US11028778B2 (en) 2018-09-27 2021-06-08 Pratt & Whitney Canada Corp. Engine with start assist
FR3088672B1 (fr) * 2018-11-16 2020-12-18 Safran Aircraft Engines Dispositif pour le centrage et le guidage en rotation d'une piece rotative avec bras entrelaces
KR20200121095A (ko) 2019-04-15 2020-10-23 주식회사 엘케이 타일통공 마킹장치
FR3097259B1 (fr) 2019-06-12 2021-05-21 Safran Helicopter Engines Piece annulaire de support d’un palier pour une turbomachine
US11268405B2 (en) * 2020-03-04 2022-03-08 Pratt & Whitney Canada Corp. Bearing support structure with variable stiffness

Family Cites Families (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2744722A (en) * 1951-04-06 1956-05-08 Gen Motors Corp Turbine bearing support
US2941781A (en) * 1955-10-13 1960-06-21 Westinghouse Electric Corp Guide vane array for turbines
US3002793A (en) * 1958-05-07 1961-10-03 Ford Motor Co Bearing support structure
US3015524A (en) * 1958-11-19 1962-01-02 Owens Corning Fiberglass Corp Inverted turbine
GB938286A (en) * 1961-05-04 1963-10-02 Rolls Royce Improvements in or relating to gas turbine engines
DE1235072B (de) * 1963-03-07 1967-02-23 Daimler Benz Ag Nachgiebige Lagergehaeuseaufhaengung an der Aussenwand eines Gasturbinentriebwerks
US3536414A (en) * 1968-03-06 1970-10-27 Gen Electric Vanes for turning fluid flow in an annular duct
US3830056A (en) * 1972-12-04 1974-08-20 Gen Electric Conversion means for a gas turbine engine
US3830058A (en) 1973-02-26 1974-08-20 Avco Corp Fan engine mounting
JPS5524399Y2 (pl) * 1974-09-10 1980-06-11
US4053189A (en) * 1976-06-17 1977-10-11 United Technologies Corporation Turbine construction
FR2470861A1 (fr) * 1979-12-06 1981-06-12 Rolls Royce Dispositif de maintien d'un etat de tension constant dans les organes d'une turbine a gaz
GB2114669B (en) * 1982-02-12 1985-01-16 Rolls Royce Gas turbine engine bearing support structure
US4820117A (en) * 1987-07-09 1989-04-11 United Technologies Corporation Crossed I-beam structural strut
US4989406A (en) * 1988-12-29 1991-02-05 General Electric Company Turbine engine assembly with aft mounted outlet guide vanes
JPH0692723B2 (ja) * 1990-03-19 1994-11-16 株式会社日立製作所 軸流流体機械
US5450719A (en) * 1993-11-17 1995-09-19 Alliedsignal, Inc. Gas turbine engine rear magnetic or foil bearing cooling using exhaust eductor
US6353789B1 (en) * 1999-12-13 2002-03-05 United Technologies Corporation Predicting broadband noise from a stator vane of a gas turbine engine
JP2002349498A (ja) * 2001-05-24 2002-12-04 Ishikawajima Harima Heavy Ind Co Ltd 低騒音ファン静翼
GB0520850D0 (en) * 2005-10-14 2005-11-23 Rolls Royce Plc Fan static structure
US20100303608A1 (en) * 2006-09-28 2010-12-02 Mitsubishi Heavy Industries, Ltd. Two-shaft gas turbine
GB0622405D0 (en) * 2006-11-10 2006-12-20 Rolls Royce Plc A turbine engine mounting arrangement
FR2914697B1 (fr) * 2007-04-06 2012-11-30 Turbomeca Dispositif d'assistance aux phases transitoires d'acceleration et de deceleration
FR2923263B1 (fr) * 2007-11-07 2014-05-09 Turbomeca Turbomoteur comportant des moyens pour chauffer l'air entrant dans la turbine libre
FR2923530B1 (fr) * 2007-11-09 2014-04-04 Snecma Raccordement de bras radiaux a une virole circulaire par des axes et des entretoises
JP4969500B2 (ja) * 2008-03-28 2012-07-04 三菱重工業株式会社 ガスタービン
US8221071B2 (en) * 2008-09-30 2012-07-17 General Electric Company Integrated guide vane assembly

Also Published As

Publication number Publication date
CN104053865B (zh) 2016-04-06
RU2615888C2 (ru) 2017-04-11
KR20140116115A (ko) 2014-10-01
CA2861738A1 (fr) 2013-07-25
EP2805029A1 (fr) 2014-11-26
CA2861738C (fr) 2019-04-30
US9915173B2 (en) 2018-03-13
JP2015504140A (ja) 2015-02-05
WO2013107966A1 (fr) 2013-07-25
JP5908608B2 (ja) 2016-04-26
EP2805029B1 (fr) 2016-01-06
FR2986040B1 (fr) 2016-03-25
US20150000306A1 (en) 2015-01-01
RU2014134019A (ru) 2016-03-20
ES2562229T3 (es) 2016-03-03
CN104053865A (zh) 2014-09-17
FR2986040A1 (fr) 2013-07-26
KR102051160B1 (ko) 2019-12-02

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