PL2182177T3 - Konstrukcja nośna łożyska dla turbiny - Google Patents

Konstrukcja nośna łożyska dla turbiny

Info

Publication number
PL2182177T3
PL2182177T3 PL09380162T PL09380162T PL2182177T3 PL 2182177 T3 PL2182177 T3 PL 2182177T3 PL 09380162 T PL09380162 T PL 09380162T PL 09380162 T PL09380162 T PL 09380162T PL 2182177 T3 PL2182177 T3 PL 2182177T3
Authority
PL
Poland
Prior art keywords
turbine
support structure
bearing support
bearing
support
Prior art date
Application number
PL09380162T
Other languages
English (en)
Inventor
Jon Heriz Agiriano
Raúl Vázquez Díaz
David Cadrecha Robles
Sergio Moñux Rodrigo
Erlantz Cristobal Camio
Original Assignee
Industria De Turbo Propulsores S.A.
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 Industria De Turbo Propulsores S.A. filed Critical Industria De Turbo Propulsores S.A.
Publication of PL2182177T3 publication Critical patent/PL2182177T3/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
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • 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
    • F01D9/00—Stators
    • F01D9/06—Fluid supply conduits to nozzles or the like
    • F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • F05D2230/642—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins using maintaining alignment while permitting differential dilatation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/94—Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF]
    • F05D2260/941—Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF] particularly aimed at mechanical or thermal stress reduction
    • 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
PL09380162T 2008-11-04 2009-10-09 Konstrukcja nośna łożyska dla turbiny PL2182177T3 (pl)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ES200803145A ES2370307B1 (es) 2008-11-04 2008-11-04 Estructura soporte de rodamiento para turbina.
EP09380162.9A EP2182177B1 (en) 2008-11-04 2009-10-09 Bearing support structure for turbine

Publications (1)

Publication Number Publication Date
PL2182177T3 true PL2182177T3 (pl) 2019-02-28

Family

ID=41353934

Family Applications (1)

Application Number Title Priority Date Filing Date
PL09380162T PL2182177T3 (pl) 2008-11-04 2009-10-09 Konstrukcja nośna łożyska dla turbiny

Country Status (5)

Country Link
US (1) US8454304B2 (pl)
EP (1) EP2182177B1 (pl)
CA (1) CA2683382C (pl)
ES (2) ES2370307B1 (pl)
PL (1) PL2182177T3 (pl)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8162603B2 (en) * 2009-01-30 2012-04-24 General Electric Company Vane frame for a turbomachine and method of minimizing weight thereof
DE102010014900A1 (de) 2010-04-14 2011-10-20 Rolls-Royce Deutschland Ltd & Co Kg Nebenstromkanal eines Turbofantriebwerkes
US8915703B2 (en) * 2011-07-28 2014-12-23 United Technologies Corporation Internally actuated inlet guide vane for fan section
US10221707B2 (en) 2013-03-07 2019-03-05 Pratt & Whitney Canada Corp. Integrated strut-vane
US10344603B2 (en) 2013-07-30 2019-07-09 United Technologies Corporation Gas turbine engine turbine vane ring arrangement
US9835038B2 (en) 2013-08-07 2017-12-05 Pratt & Whitney Canada Corp. Integrated strut and vane arrangements
US9556746B2 (en) 2013-10-08 2017-01-31 Pratt & Whitney Canada Corp. Integrated strut and turbine vane nozzle arrangement
US9909434B2 (en) 2015-07-24 2018-03-06 Pratt & Whitney Canada Corp. Integrated strut-vane nozzle (ISV) with uneven vane axial chords
US10443451B2 (en) 2016-07-18 2019-10-15 Pratt & Whitney Canada Corp. Shroud housing supported by vane segments
US10612420B2 (en) 2016-11-17 2020-04-07 General Electric Company Support structures for rotors
FR3077329B1 (fr) 2018-01-29 2022-06-24 Safran Aircraft Engines Carter inter-turbines comprenant des aubes separatrices rapportees
US10883376B2 (en) 2019-02-01 2021-01-05 Rolls-Royce Plc Turbine vane assembly with ceramic matrix composite vanes
US10767493B2 (en) 2019-02-01 2020-09-08 Rolls-Royce Plc Turbine vane assembly with ceramic matrix composite vanes
US11319822B2 (en) 2020-05-06 2022-05-03 Rolls-Royce North American Technologies Inc. Hybrid vane segment with ceramic matrix composite airfoils
DE102020215576A1 (de) * 2020-12-09 2022-06-09 Rolls-Royce Deutschland Ltd & Co Kg Strömungsleitvorrichtung und ein Gasturbinentriebwerk
US11773735B2 (en) 2021-12-22 2023-10-03 Rolls-Royce Plc Vane ring assembly with ceramic matrix composite airfoils

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2941781A (en) * 1955-10-13 1960-06-21 Westinghouse Electric Corp Guide vane array for turbines
US2930662A (en) * 1956-11-01 1960-03-29 Bristol Aero Engines Ltd Supporting structure for a gas turbine bearing
US3319930A (en) * 1961-12-19 1967-05-16 Gen Electric Stator assembly for turbomachines
US4989406A (en) * 1988-12-29 1991-02-05 General Electric Company Turbine engine assembly with aft mounted outlet guide vanes
DE4017861A1 (de) * 1990-06-02 1991-12-05 Mtu Muenchen Gmbh Leitkranz fuer eine gasturbine
US5411370A (en) * 1994-08-01 1995-05-02 United Technologies Corporation Vibration damping shroud for a turbomachine vane
FR2738283B1 (fr) * 1995-08-30 1997-09-26 Snecma Agencement de turbomachine comprenant une grille d'aubes et un carter intermediaire
US6358001B1 (en) * 2000-04-29 2002-03-19 General Electric Company Turbine frame assembly
US8757965B2 (en) * 2004-06-01 2014-06-24 Volvo Aero Corporation Gas turbine compression system and compressor structure
ATE395506T1 (de) * 2004-06-01 2008-05-15 Volvo Aero Corp Gasturbinen-kompressionssystem und verdichterstruktur
US7052234B2 (en) * 2004-06-23 2006-05-30 General Electric Company Turbine vane collar seal
US7100358B2 (en) * 2004-07-16 2006-09-05 Pratt & Whitney Canada Corp. Turbine exhaust case and method of making
SE528006C2 (sv) * 2004-12-23 2006-08-01 Volvo Aero Corp Statisk gasturbinkomponent och förfarande för reparation av en sådan komponent
US7600970B2 (en) * 2005-12-08 2009-10-13 General Electric Company Ceramic matrix composite vane seals
FR2901574B1 (fr) * 2006-05-29 2008-07-04 Snecma Sa Dispositif de guidage d'un flux d'air a l'entree d'une chambre de combustion dans une turbomachine

Also Published As

Publication number Publication date
CA2683382C (en) 2013-02-12
EP2182177B1 (en) 2018-08-29
ES2370307B1 (es) 2012-11-27
EP2182177A2 (en) 2010-05-05
EP2182177A3 (en) 2017-05-10
US20100111690A1 (en) 2010-05-06
CA2683382A1 (en) 2010-05-04
ES2699901T3 (es) 2019-02-13
ES2370307A1 (es) 2011-12-14
US8454304B2 (en) 2013-06-04

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