DE602004006732D1 - Verfahren zur herstellung einer statorkomponente - Google Patents

Verfahren zur herstellung einer statorkomponente

Info

Publication number
DE602004006732D1
DE602004006732D1 DE602004006732T DE602004006732T DE602004006732D1 DE 602004006732 D1 DE602004006732 D1 DE 602004006732D1 DE 602004006732 T DE602004006732 T DE 602004006732T DE 602004006732 T DE602004006732 T DE 602004006732T DE 602004006732 D1 DE602004006732 D1 DE 602004006732D1
Authority
DE
Germany
Prior art keywords
stator component
producing
sectors
component
cast
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.)
Expired - Lifetime
Application number
DE602004006732T
Other languages
English (en)
Other versions
DE602004006732T2 (de
Inventor
Jan Lundgren
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.)
GKN Aerospace Sweden AB
Original Assignee
Volvo Aero AB
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 AB filed Critical Volvo Aero AB
Publication of DE602004006732D1 publication Critical patent/DE602004006732D1/de
Application granted granted Critical
Publication of DE602004006732T2 publication Critical patent/DE602004006732T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246Fastening of diaphragms or stator-rings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K15/00Electron-beam welding or cutting
    • B23K15/0046Welding
    • B23K15/0093Welding characterised by the properties of the materials to be welded
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/04Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from several pieces
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2101/00Articles made by soldering, welding or cutting
    • B23K2101/001Turbines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/20Manufacture essentially without removing material
    • F05D2230/23Manufacture essentially without removing material by permanently joining parts together
    • F05D2230/232Manufacture essentially without removing material by permanently joining parts together by welding
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/40Use of a multiplicity of similar components
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49002Electrical device making
    • Y10T29/49009Dynamoelectric machine
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49316Impeller making
    • Y10T29/4932Turbomachine making
    • Y10T29/49323Assembling fluid flow directing devices, e.g., stators, diaphragms, nozzles
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/4998Combined manufacture including applying or shaping of fluent material
    • Y10T29/49988Metal casting

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Manufacture Of Motors, Generators (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Laser Beam Processing (AREA)
  • Iron Core Of Rotating Electric Machines (AREA)
  • Supercharger (AREA)
DE602004006732T 2003-03-21 2004-03-16 Verfahren zur herstellung einer statorkomponente Expired - Lifetime DE602004006732T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
SE0300770A SE525879C2 (sv) 2003-03-21 2003-03-21 Förfarande för framställning av en statorkomponent
SE0300770 2003-03-21
PCT/SE2004/000387 WO2004083605A1 (en) 2003-03-21 2004-03-16 A method of manufacturing a stator component

Publications (2)

Publication Number Publication Date
DE602004006732D1 true DE602004006732D1 (de) 2007-07-12
DE602004006732T2 DE602004006732T2 (de) 2008-01-31

Family

ID=20290733

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602004006732T Expired - Lifetime DE602004006732T2 (de) 2003-03-21 2004-03-16 Verfahren zur herstellung einer statorkomponente

Country Status (10)

Country Link
US (1) US7389583B2 (de)
EP (1) EP1608846B1 (de)
JP (1) JP4489762B2 (de)
CN (1) CN100338338C (de)
AT (1) ATE363586T1 (de)
DE (1) DE602004006732T2 (de)
ES (1) ES2286624T3 (de)
RU (1) RU2338888C2 (de)
SE (1) SE525879C2 (de)
WO (1) WO2004083605A1 (de)

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0412775D0 (en) * 2004-06-09 2004-07-07 Rolls Royce Plc Method of replacing damaged aerofoil
SE528948C2 (sv) * 2004-12-23 2007-03-20 Volvo Aero Corp Ringformad vridstyv statisk komponent för en flygplansmotor
EP1975373A1 (de) * 2007-03-06 2008-10-01 Siemens Aktiengesellschaft Leitschaufelkanalelement für eine Leitschaufelanordnung eines Gasturbinentriebwerks
CN101468437B (zh) * 2007-12-26 2010-09-08 深圳市大族激光科技股份有限公司 一种定子的加工方法
US8430627B2 (en) * 2009-10-29 2013-04-30 Alstom Technology Ltd Gas turbine exhaust strut refurbishment
EP2333252A1 (de) * 2009-12-08 2011-06-15 Siemens Aktiengesellschaft Mehrteiliges Innengehäuse für eine Dampfturbine
EP2794182B1 (de) * 2011-12-23 2016-09-14 Volvo Aero Corporation Stützstruktur für ein Gasturbinentriebwerk, zugehöriges Gasturbinentriebwerk, Flugzeug und Herstellungsverfahren
US9845695B2 (en) 2012-12-29 2017-12-19 United Technologies Corporation Gas turbine seal assembly and seal support
US10240532B2 (en) 2012-12-29 2019-03-26 United Technologies Corporation Frame junction cooling holes
WO2014105602A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Heat shield for a casing
EP2938837B1 (de) 2012-12-29 2018-06-27 United Technologies Corporation Gasturbinendichtungsanordnung und dichtungshalterung
JP6385955B2 (ja) 2012-12-29 2018-09-05 ユナイテッド テクノロジーズ コーポレイションUnited Technologies Corporation タービンフレームアセンブリおよびタービンフレームアセンブリを設計する方法
WO2014105603A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Multi-piece heat shield
WO2014105512A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Mechanical linkage for segmented heat shield
US10053998B2 (en) 2012-12-29 2018-08-21 United Technologies Corporation Multi-purpose gas turbine seal support and assembly
US9903224B2 (en) 2012-12-29 2018-02-27 United Technologies Corporation Scupper channelling in gas turbine modules
EP2938857B2 (de) 2012-12-29 2020-11-25 United Technologies Corporation Hitzeschild zur kühlung einer strebe
WO2014105496A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Flow diverter element and assembly
WO2014105604A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Angled cut to direct radiative heat load
US10138742B2 (en) 2012-12-29 2018-11-27 United Technologies Corporation Multi-ply finger seal
WO2014105826A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Seal support disk and assembly
US10006306B2 (en) 2012-12-29 2018-06-26 United Technologies Corporation Turbine exhaust case architecture
US9631517B2 (en) 2012-12-29 2017-04-25 United Technologies Corporation Multi-piece fairing for monolithic turbine exhaust case
EP2938834A1 (de) 2012-12-29 2015-11-04 United Technologies Corporation Stossfänger für abdichtungen in einem turbinenabgasgehäuse
WO2014105619A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Multi-function boss for a turbine exhaust case
WO2014105657A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Mount with deflectable tabs
US9890663B2 (en) 2012-12-31 2018-02-13 United Technologies Corporation Turbine exhaust case multi-piece frame
US10054009B2 (en) 2012-12-31 2018-08-21 United Technologies Corporation Turbine exhaust case multi-piece frame
DE112013006315T5 (de) 2012-12-31 2015-09-17 United Technologies Corporation Mehrteiliger Rahmen eines Turbinenabgasgehäuses
US10330011B2 (en) 2013-03-11 2019-06-25 United Technologies Corporation Bench aft sub-assembly for turbine exhaust case fairing
EP2878433B1 (de) * 2013-11-29 2016-04-20 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Ummantelte Drehanordnung aus segmentiertem Verbundwerkstoff für Flugzeuge sowie verfahren zu deren Herstellung
FR3051831B1 (fr) * 2016-05-26 2018-05-18 Safran Aircraft Engines Carter d'echappement de turbomachine et son procede de fabrication
EP3519681A4 (de) * 2016-09-29 2020-12-02 GKN Aerospace Newington LLC Herstellungsverfahren für zylindrische teile
BE1025975B1 (fr) 2018-02-02 2019-09-03 Safran Aero Boosters S.A. Carter structural pour turbomachine axiale
CN113523721B (zh) * 2021-07-13 2023-07-07 江苏振江新能源装备股份有限公司 三瓣式定子构件的制造方法及三瓣式定子构件

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4511306A (en) * 1982-02-02 1985-04-16 Westinghouse Electric Corp. Combustion turbine single airfoil stator vane structure
US5177954A (en) * 1984-10-10 1993-01-12 Paul Marius A Gas turbine engine with cooled turbine blades
US5176496A (en) * 1991-09-27 1993-01-05 General Electric Company Mounting arrangements for turbine nozzles
US5248240A (en) * 1993-02-08 1993-09-28 General Electric Company Turbine stator vane assembly
JP3218800B2 (ja) * 1993-05-31 2001-10-15 石川島播磨重工業株式会社 タービン静翼の組み付け方法
DE19544817A1 (de) * 1995-12-01 1997-06-05 Asea Brown Boveri Verfahren zur Herstellung eines Leitschaufelsegmentes für eine Gasturbine
US5813832A (en) * 1996-12-05 1998-09-29 General Electric Company Turbine engine vane segment
US6464457B1 (en) * 2001-06-21 2002-10-15 General Electric Company Turbine leaf seal mounting with headless pins
SE519781C2 (sv) * 2001-08-29 2003-04-08 Volvo Aero Corp Förfarande för framställning av en stator-eller rotorkomponent
JP2004056932A (ja) * 2002-07-22 2004-02-19 Hitachi Ltd 外転型モータ

Also Published As

Publication number Publication date
SE525879C2 (sv) 2005-05-17
CN100338338C (zh) 2007-09-19
SE0300770L (sv) 2004-09-22
US20060000077A1 (en) 2006-01-05
ES2286624T3 (es) 2007-12-01
SE0300770D0 (sv) 2003-03-21
US7389583B2 (en) 2008-06-24
EP1608846B1 (de) 2007-05-30
RU2005132387A (ru) 2007-04-27
WO2004083605A1 (en) 2004-09-30
JP2006520874A (ja) 2006-09-14
JP4489762B2 (ja) 2010-06-23
EP1608846A1 (de) 2005-12-28
CN1761802A (zh) 2006-04-19
RU2338888C2 (ru) 2008-11-20
ATE363586T1 (de) 2007-06-15
DE602004006732T2 (de) 2008-01-31

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition