SE0300770L - Förfarande för framställning av en statorkomponent - Google Patents

Förfarande för framställning av en statorkomponent

Info

Publication number
SE0300770L
SE0300770L SE0300770A SE0300770A SE0300770L SE 0300770 L SE0300770 L SE 0300770L SE 0300770 A SE0300770 A SE 0300770A SE 0300770 A SE0300770 A SE 0300770A SE 0300770 L SE0300770 L SE 0300770L
Authority
SE
Sweden
Prior art keywords
manufacturing
stator component
sectors
component
cast
Prior art date
Application number
SE0300770A
Other languages
English (en)
Other versions
SE0300770D0 (sv
SE525879C2 (sv
Inventor
Jan Lundgren
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 SE0300770A priority Critical patent/SE525879C2/sv
Publication of SE0300770D0 publication Critical patent/SE0300770D0/sv
Priority to ES04721052T priority patent/ES2286624T3/es
Priority to AT04721052T priority patent/ATE363586T1/de
Priority to PCT/SE2004/000387 priority patent/WO2004083605A1/en
Priority to EP04721052A priority patent/EP1608846B1/en
Priority to RU2005132387/06A priority patent/RU2338888C2/ru
Priority to JP2006507964A priority patent/JP4489762B2/ja
Priority to CNB200480007746XA priority patent/CN100338338C/zh
Priority to DE602004006732T priority patent/DE602004006732T2/de
Publication of SE0300770L publication Critical patent/SE0300770L/sv
Publication of SE525879C2 publication Critical patent/SE525879C2/sv
Priority to US11/162,139 priority patent/US7389583B2/en

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
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246—Fastening of diaphragms or stator-rings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K15/00—Electron-beam welding or cutting
    • B23K15/0046—Welding
    • B23K15/0093—Welding characterised by the properties of the materials to be welded
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/04—Making 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
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2101/00—Articles made by soldering, welding or cutting
    • B23K2101/001—Turbines
    • 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
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
    • F05D2230/232—Manufacture essentially without removing material by permanently joining parts together by welding
    • 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
    • F05D2240/00—Components
    • F05D2240/40—Use of a multiplicity of similar components
    • 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
    • Y10T29/49002—Electrical device making
    • Y10T29/49009—Dynamoelectric machine
    • 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
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making
    • Y10T29/49323—Assembling fluid flow directing devices, e.g., stators, diaphragms, nozzles
    • 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
    • Y10T29/4998—Combined manufacture including applying or shaping of fluent material
    • Y10T29/49988—Metal 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)
  • Iron Core Of Rotating Electric Machines (AREA)
  • Laser Beam Processing (AREA)
  • Supercharger (AREA)
SE0300770A 2003-03-21 2003-03-21 Förfarande för framställning av en statorkomponent SE525879C2 (sv)

Priority Applications (10)

Application Number Priority Date Filing Date Title
SE0300770A SE525879C2 (sv) 2003-03-21 2003-03-21 Förfarande för framställning av en statorkomponent
DE602004006732T DE602004006732T2 (de) 2003-03-21 2004-03-16 Verfahren zur herstellung einer statorkomponente
EP04721052A EP1608846B1 (en) 2003-03-21 2004-03-16 A method of manufacturing a stator component
AT04721052T ATE363586T1 (de) 2003-03-21 2004-03-16 Verfahren zur herstellung einer statorkomponente
PCT/SE2004/000387 WO2004083605A1 (en) 2003-03-21 2004-03-16 A method of manufacturing a stator component
ES04721052T ES2286624T3 (es) 2003-03-21 2004-03-16 Metodo de fabricacion de un componente de estator.
RU2005132387/06A RU2338888C2 (ru) 2003-03-21 2004-03-16 Способ изготовления компонента статора
JP2006507964A JP4489762B2 (ja) 2003-03-21 2004-03-16 静翼構成要素の製造方法
CNB200480007746XA CN100338338C (zh) 2003-03-21 2004-03-16 定子元件的制造方法
US11/162,139 US7389583B2 (en) 2003-03-21 2005-08-30 Method of manufacturing a stator component

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE0300770A SE525879C2 (sv) 2003-03-21 2003-03-21 Förfarande för framställning av en statorkomponent

Publications (3)

Publication Number Publication Date
SE0300770D0 SE0300770D0 (sv) 2003-03-21
SE0300770L true SE0300770L (sv) 2004-09-22
SE525879C2 SE525879C2 (sv) 2005-05-17

Family

ID=20290733

Family Applications (1)

Application Number Title Priority Date Filing Date
SE0300770A SE525879C2 (sv) 2003-03-21 2003-03-21 Förfarande för framställning av en statorkomponent

Country Status (10)

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

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 (en) 2007-03-06 2008-10-01 Siemens Aktiengesellschaft Guide vane duct element for a guide vane assembly of a gas turbine engine
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
JP5946543B2 (ja) * 2011-12-23 2016-07-06 ゲーコーエヌ エアロスペース スウェーデン アーベー ガスタービンエンジンの支持構造物
US9631517B2 (en) 2012-12-29 2017-04-25 United Technologies Corporation Multi-piece fairing for monolithic turbine exhaust case
US9982561B2 (en) 2012-12-29 2018-05-29 United Technologies Corporation Heat shield for cooling a strut
WO2014105602A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Heat shield for a casing
WO2014105496A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Flow diverter element and assembly
US10378370B2 (en) 2012-12-29 2019-08-13 United Technologies Corporation Mechanical linkage for segmented heat shield
US10087843B2 (en) 2012-12-29 2018-10-02 United Technologies Corporation Mount with deflectable tabs
WO2014143329A2 (en) 2012-12-29 2014-09-18 United Technologies Corporation Frame junction cooling holes
WO2014105780A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Multi-purpose gas turbine seal support and assembly
US9845695B2 (en) 2012-12-29 2017-12-19 United Technologies Corporation Gas turbine seal assembly and seal support
WO2014105616A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Turbine exhaust case architecture
WO2014105425A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Turbine frame assembly and method of designing turbine frame assembly
EP2938837B1 (en) 2012-12-29 2018-06-27 United Technologies Corporation Gas turbine seal assembly and seal support
WO2014105603A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Multi-piece heat shield
WO2014105826A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Seal support disk and assembly
US10240481B2 (en) 2012-12-29 2019-03-26 United Technologies Corporation Angled cut to direct radiative heat load
WO2014105577A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Scupper channelling in gas turbine modules
WO2014137444A2 (en) 2012-12-29 2014-09-12 United Technologies Corporation Multi-ply finger seal
WO2014105100A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Bumper for seals in a turbine exhaust case
WO2014105619A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Multi-function boss for a turbine exhaust case
EP2938860B1 (en) 2012-12-31 2018-08-29 United Technologies Corporation Turbine exhaust case multi-piece frame
WO2014105682A1 (en) 2012-12-31 2014-07-03 United Technologies Corporation Turbine exhaust case multi-piece frame
JP6232446B2 (ja) 2012-12-31 2017-11-15 ユナイテッド テクノロジーズ コーポレイションＵｎｉｔｅｄ Ｔｅｃｈｎｏｌｏｇｉｅｓ Ｃｏｒｐｏｒａｔｉｏｎ タービン排気ケースのマルチピース型フレーム
EP2971579B1 (en) 2013-03-11 2020-04-29 United Technologies Corporation Aft fairing sub-assembly for turbine exhaust case fairing
EP2878433B1 (en) * 2013-11-29 2016-04-20 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Shrouded rotary assembly from segmented composite for aircraft and method for its manufacture
FR3051831B1 (fr) 2016-05-26 2018-05-18 Safran Aircraft Engines Carter d'echappement de turbomachine et son procede de fabrication
WO2018063221A1 (en) * 2016-09-29 2018-04-05 Gkn Aerospace Newington Llc Manufacturing method for cylindrical parts
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
ES2286624T3 (es) 2007-12-01
SE0300770D0 (sv) 2003-03-21
US20060000077A1 (en) 2006-01-05
DE602004006732D1 (de) 2007-07-12
RU2338888C2 (ru) 2008-11-20
CN1761802A (zh) 2006-04-19
WO2004083605A1 (en) 2004-09-30
EP1608846B1 (en) 2007-05-30
SE525879C2 (sv) 2005-05-17
CN100338338C (zh) 2007-09-19
ATE363586T1 (de) 2007-06-15
JP4489762B2 (ja) 2010-06-23
DE602004006732T2 (de) 2008-01-31
RU2005132387A (ru) 2007-04-27
JP2006520874A (ja) 2006-09-14
US7389583B2 (en) 2008-06-24
EP1608846A1 (en) 2005-12-28

Similar Documents

Publication Publication Date Title
SE0300770L (sv) Förfarande för framställning av en statorkomponent
DE602004010346D1 (de) Abgasabdichtung für einen Turbocharger
DE60128865D1 (de) Kühlung für einen Turbinenmantelring
ATE509217T1 (de) Zweiteilige statorschaufel
FR2889863B1 (fr) Compresseur comportant une pluralite de caissons reconstituant un volume annulaire de separation de flux dans une turbomachine.
UA87971C2 (ru) Неподвижный кольцевой компонент газовой турбины и сегмент неподвижного кольцевого компонента
NO20051741D0 (no) Stator med hoy virkningsgrad for den forste fase i en gassturbin
TW200632218A (en) Compressor discharge muffler
ATE551533T1 (de) Statorscheibe für turbomolekularpumpe
RU2016107008A (ru) Корпус газотурбинного двигателя и способ изготовления
RU2013152393A (ru) Статор осевой турбомашины с сегментным внутренним корпусом
JP2012513614A5 (sv)
ATE519087T1 (de) Mehrrohrwärmetauschervorrichtung und herstellungsverfahren dafür
FR2887919B1 (fr) Rotor de turbomachine comprenant au moins un disque renforce par un anneau composite
FR2712037B1 (fr) Turbomachine à compresseur dont le rotor a un étage amont amovible.
DE602004000789D1 (de) Ringförmige Brennkammer für eine Turbomaschine
ITMI20040712A1 (it) Rotore ed alevata efficenza per secondo stadio ri una turbina a gas
AU2003242165A1 (en) Method for manufacturing a stator component
BRPI0614795A8 (pt) Disposição de aleta diretriz de uma turbomáquina
EE200300588A (et) Vahend kulumise vähendamiseks gaasturbiini põlemiskambris
ITTO20010346A0 (it) Combustore per una turbina a gas, particolarmente per un motore aeronautico.
DE60113069D1 (de) Dichtungsanordnung für Turbomaschinenlager
FR2923526B1 (fr) Etage de turbine ou de compresseur de turbomachine
DE502004002190D1 (de) Strömungsmaschine, insbesondere gasturbine
DE502005006205D1 (de) Rotor-schluss

Legal Events

Date Code Title Description
NUG Patent has lapsed