SE0403193D0 - Static gas turbine component and method for repairing such a component - Google Patents

Static gas turbine component and method for repairing such a component

Info

Publication number
SE0403193D0
SE0403193D0 SE0403193A SE0403193A SE0403193D0 SE 0403193 D0 SE0403193 D0 SE 0403193D0 SE 0403193 A SE0403193 A SE 0403193A SE 0403193 A SE0403193 A SE 0403193A SE 0403193 D0 SE0403193 D0 SE 0403193D0
Authority
SE
Sweden
Prior art keywords
component
gas turbine
core
static gas
repairing
Prior art date
Application number
SE0403193A
Other languages
English (en)
Other versions
SE0403193L (sv
SE528006C2 (sv
Inventor
Anders Sjunnesson
Original Assignee
Volvo Aero Corp
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 Volvo Aero Corp filed Critical Volvo Aero Corp
Priority to SE0403193A priority Critical patent/SE528006C2/sv
Publication of SE0403193D0 publication Critical patent/SE0403193D0/sv
Priority to CA002588470A priority patent/CA2588470A1/en
Priority to RU2007128096/06A priority patent/RU2394161C2/ru
Priority to US11/722,716 priority patent/US8070432B2/en
Priority to PCT/SE2005/001975 priority patent/WO2006068599A1/en
Priority to CN2005800447762A priority patent/CN101087928B/zh
Priority to EP05819799A priority patent/EP1831505B1/en
Priority to JP2007548148A priority patent/JP4820373B2/ja
Publication of SE0403193L publication Critical patent/SE0403193L/sv
Publication of SE528006C2 publication Critical patent/SE528006C2/sv

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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow 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
    • F01D9/02—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
    • 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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/50—Intrinsic material properties or characteristics
    • F05D2300/501—Elasticity
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/50—Intrinsic material properties or characteristics
    • F05D2300/506—Hardness
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/612—Foam
    • 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
    • Y10T29/49229—Prime mover or fluid pump making
    • Y10T29/49236—Fluid pump or compressor making
    • Y10T29/49238—Repairing, converting, servicing or salvaging

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Architecture (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Vibration Dampers (AREA)
SE0403193A 2004-12-23 2004-12-23 Statisk gasturbinkomponent och förfarande för reparation av en sådan komponent SE528006C2 (sv)

Priority Applications (8)

Application Number Priority Date Filing Date Title
SE0403193A SE528006C2 (sv) 2004-12-23 2004-12-23 Statisk gasturbinkomponent och förfarande för reparation av en sådan komponent
CA002588470A CA2588470A1 (en) 2004-12-23 2005-12-19 Static gas turbine component and method for repairing such a component
RU2007128096/06A RU2394161C2 (ru) 2004-12-23 2005-12-19 Узел статора газотурбинного двигателя и способ ремонта такого узла, а также двигатель, содержащий такой узел статора
US11/722,716 US8070432B2 (en) 2004-12-23 2005-12-19 Static gas turbine component and method for repairing such a component
PCT/SE2005/001975 WO2006068599A1 (en) 2004-12-23 2005-12-19 Static gas turbine component and method for repairing such a component
CN2005800447762A CN101087928B (zh) 2004-12-23 2005-12-19 静态燃气涡轮机部件及维修这种部件的方法
EP05819799A EP1831505B1 (en) 2004-12-23 2005-12-19 Static gas turbine component and method for repairing such a component
JP2007548148A JP4820373B2 (ja) 2004-12-23 2005-12-19 スタティックガスタービン部分品及びそうした部分品の補修法

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE0403193A SE528006C2 (sv) 2004-12-23 2004-12-23 Statisk gasturbinkomponent och förfarande för reparation av en sådan komponent

Publications (3)

Publication Number Publication Date
SE0403193D0 true SE0403193D0 (sv) 2004-12-23
SE0403193L SE0403193L (sv) 2006-06-24
SE528006C2 SE528006C2 (sv) 2006-08-01

Family

ID=34102135

Family Applications (1)

Application Number Title Priority Date Filing Date
SE0403193A SE528006C2 (sv) 2004-12-23 2004-12-23 Statisk gasturbinkomponent och förfarande för reparation av en sådan komponent

Country Status (8)

Country Link
US (1) US8070432B2 (sv)
EP (1) EP1831505B1 (sv)
JP (1) JP4820373B2 (sv)
CN (1) CN101087928B (sv)
CA (1) CA2588470A1 (sv)
RU (1) RU2394161C2 (sv)
SE (1) SE528006C2 (sv)
WO (1) WO2006068599A1 (sv)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080072569A1 (en) * 2006-09-27 2008-03-27 Thomas Ory Moniz Guide vane and method of fabricating the same
DE102006057912A1 (de) * 2006-12-08 2008-06-12 Mtu Aero Engines Gmbh Leitschaufelkranz sowie Verfahren zum Herstellen desselben
US20080159851A1 (en) * 2006-12-29 2008-07-03 Thomas Ory Moniz Guide Vane and Method of Fabricating the Same
US8485783B2 (en) * 2007-12-20 2013-07-16 Volvo Aero Corporation Gas turbine engine
FR2926337B1 (fr) * 2008-01-14 2013-12-06 Snecma Aube directrice de sortie pour un turboreacteur d'avion et turboreacteur comportant cette aube
ES2370307B1 (es) * 2008-11-04 2012-11-27 Industria De Turbo Propulsores, S.A. Estructura soporte de rodamiento para turbina.
FR2938238B1 (fr) * 2008-11-13 2010-11-12 Aircelle Sa Structure d'entree d'air de nacelle
US8807931B2 (en) * 2010-01-04 2014-08-19 General Electric Company System for impact zone reinforcement
US9765648B2 (en) * 2011-12-08 2017-09-19 Gkn Aerospace Sweden Ab Gas turbine engine component
GB2497809B (en) * 2011-12-22 2014-03-12 Rolls Royce Plc Method of servicing a gas turbine engine
US9163525B2 (en) * 2012-06-27 2015-10-20 United Technologies Corporation Turbine wheel catcher
EP2971574B1 (en) * 2013-03-15 2019-08-21 United Technologies Corporation Structural guide vane leading edge
US10822970B2 (en) 2014-11-06 2020-11-03 Raytheon Technologies Corporation Gas turbine engine structural guide vanes
BE1023290B1 (fr) * 2015-07-22 2017-01-24 Safran Aero Boosters S.A. Aube composite de compresseur de turbomachine axiale
ES2870479T3 (es) * 2016-11-11 2021-10-27 Airbus Operations Gmbh Método para el reacondicionamiento de una parte dañada de un componente e inserto para ello

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3892612A (en) * 1971-07-02 1975-07-01 Gen Electric Method for fabricating foreign object damage protection for rotar blades
DE2333903B2 (de) * 1973-06-29 1976-08-12 Stroemungsprofil zur auftriebserzeugung
GB1533551A (en) * 1974-11-08 1978-11-29 Gen Electric Gas turbofan engines
US4108572A (en) * 1976-12-23 1978-08-22 United Technologies Corporation Composite rotor blade
US4111606A (en) * 1976-12-27 1978-09-05 United Technologies Corporation Composite rotor blade
US5056738A (en) * 1989-09-07 1991-10-15 General Electric Company Damper assembly for a strut in a jet propulsion engine
US5449273A (en) 1994-03-21 1995-09-12 United Technologies Corporation Composite airfoil leading edge protection
EP1049562B1 (en) * 1997-10-27 2005-02-16 Siemens Westinghouse Power Corporation Turbine blades made from multiple single crystal cast superalloy segments
US6547518B1 (en) * 2001-04-06 2003-04-15 General Electric Company Low hoop stress turbine frame support
US6796765B2 (en) * 2001-12-27 2004-09-28 General Electric Company Methods and apparatus for assembling gas turbine engine struts
US7063505B2 (en) * 2003-02-07 2006-06-20 General Electric Company Gas turbine engine frame having struts connected to rings with morse pins
GB2407142B (en) * 2003-10-15 2006-03-01 Rolls Royce Plc An arrangement for bleeding the boundary layer from an aircraft engine
DE102004017096A1 (de) * 2004-04-07 2005-10-27 Mtu Aero Engines Gmbh Strebe für ein Turbinentriebwerk

Also Published As

Publication number Publication date
JP4820373B2 (ja) 2011-11-24
CA2588470A1 (en) 2006-06-29
EP1831505B1 (en) 2012-12-05
CN101087928A (zh) 2007-12-12
RU2394161C2 (ru) 2010-07-10
US20090028699A1 (en) 2009-01-29
RU2007128096A (ru) 2009-01-27
JP2008525706A (ja) 2008-07-17
CN101087928B (zh) 2011-01-26
WO2006068599A1 (en) 2006-06-29
US8070432B2 (en) 2011-12-06
SE0403193L (sv) 2006-06-24
EP1831505A4 (en) 2012-02-22
SE528006C2 (sv) 2006-08-01
EP1831505A1 (en) 2007-09-12

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