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AU2001290458A1 - A method for manufacturing a vane to a gas turbine component and a method for manufacturing a gas turbine component - Google Patents

A method for manufacturing a vane to a gas turbine component and a method for manufacturing a gas turbine component

Info

Publication number
AU2001290458A1
AU2001290458A1 AU2001290458A AU9045801A AU2001290458A1 AU 2001290458 A1 AU2001290458 A1 AU 2001290458A1 AU 2001290458 A AU2001290458 A AU 2001290458A AU 9045801 A AU9045801 A AU 9045801A AU 2001290458 A1 AU2001290458 A1 AU 2001290458A1
Authority
AU
Australia
Prior art keywords
gas turbine
turbine component
manufacturing
vane
vanes
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.)
Abandoned
Application number
AU2001290458A
Inventor
Bertil Jonsson
Lars Sundin
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=20281792&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=AU2001290458(A1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Volvo Aero AB filed Critical Volvo Aero AB
Publication of AU2001290458A1 publication Critical patent/AU2001290458A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • 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
    • B23P15/02—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from one piece
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23H—WORKING OF METAL BY THE ACTION OF A HIGH CONCENTRATION OF ELECTRIC CURRENT ON A WORKPIECE USING AN ELECTRODE WHICH TAKES THE PLACE OF A TOOL; SUCH WORKING COMBINED WITH OTHER FORMS OF WORKING OF METAL
    • B23H7/00—Processes or apparatus applicable to both electrical discharge machining and electrochemical machining
    • B23H7/02—Wire-cutting
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23H—WORKING OF METAL BY THE ACTION OF A HIGH CONCENTRATION OF ELECTRIC CURRENT ON A WORKPIECE USING AN ELECTRODE WHICH TAKES THE PLACE OF A TOOL; SUCH WORKING COMBINED WITH OTHER FORMS OF WORKING OF METAL
    • B23H9/00—Machining specially adapted for treating particular metal objects or for obtaining special effects or results on metal objects
    • B23H9/10—Working turbine blades or nozzles
    • 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
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on 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
    • 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
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187—Convection cooling
    • 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
    • Y10T29/49316—Impeller making
    • Y10T29/49336—Blade making
    • 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
    • Y10T29/49336—Blade making
    • Y10T29/49339—Hollow blade
    • Y10T29/49341—Hollow blade with cooling passage
    • 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
    • Y10T29/49995—Shaping one-piece blank by removing material

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Thermal Sciences (AREA)
  • Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Electrochemistry (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)
  • Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
  • Separation By Low-Temperature Treatments (AREA)
  • Control Of Turbines (AREA)

Abstract

Method for manufacturing a vane ( 1 ) to a gas turbine component intended for guiding a gas flow. The vane ( 1 ) is produced by casting, and an internal hole ( 3 ) for coolant is then cut out of the cast vane ( 1 ). The vane ( 1 ) is provided with a starter hole ( 5 ), either during casting or once casting is completed, following which the internal hole ( 3 ) for coolant is cut out of the vane, proceeding from the starter hole. A method is also disclosed for manufacturing a gas turbine component including a plurality of vanes ( 1 ) for guiding a gas flow. The gas turbine component is cast in such a way that it includes the vanes and an internal hole ( 3 ) for coolant is then cut out of each of the vanes.
AU2001290458A 2000-11-09 2001-09-25 A method for manufacturing a vane to a gas turbine component and a method for manufacturing a gas turbine component Abandoned AU2001290458A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
SE0004138 2000-11-09
SE0004138A SE521759C2 (en) 2000-11-09 2000-11-09 Process for producing a blade for a gas turbine component and producing a gas turbine component
PCT/SE2001/002061 WO2002038330A1 (en) 2000-11-09 2001-09-25 A method for manufacturing a vane to a gas turbine component and a method for manufacturing a gas turbine component

Publications (1)

Publication Number Publication Date
AU2001290458A1 true AU2001290458A1 (en) 2002-05-21

Family

ID=20281792

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2001290458A Abandoned AU2001290458A1 (en) 2000-11-09 2001-09-25 A method for manufacturing a vane to a gas turbine component and a method for manufacturing a gas turbine component

Country Status (9)

Country Link
US (1) US6901661B2 (en)
EP (1) EP1337378B1 (en)
AT (1) ATE385211T1 (en)
AU (1) AU2001290458A1 (en)
CA (1) CA2423731A1 (en)
DE (1) DE60132672D1 (en)
RU (1) RU2266803C2 (en)
SE (1) SE521759C2 (en)
WO (1) WO2002038330A1 (en)

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DE102006050440A1 (en) * 2006-10-26 2008-04-30 Mtu Aero Engines Gmbh Lightweight structure-turbine blade manufacturing method, involves casting blade unit with blade wall and hollow space surrounding blade wall, where blade unit extends radially from floor area to head area
RU2340437C2 (en) * 2006-12-07 2008-12-10 Федеральное государственное унитарное предприятие "Московское машиностроительное производственное предприятие "САЛЮТ" (ФГУП "ММПП "САЛЮТ") Method for turbine hollow blade blank manufacturing for gas turbine engine
US8083511B2 (en) * 2007-12-05 2011-12-27 United Technologies Corp. Systems and methods involving pattern molds
US8042268B2 (en) * 2008-03-21 2011-10-25 Siemens Energy, Inc. Method of producing a turbine component with multiple interconnected layers of cooling channels
US20090324841A1 (en) * 2008-05-09 2009-12-31 Siemens Power Generation, Inc. Method of restoring near-wall cooled turbine components
RU2383421C1 (en) * 2008-07-10 2010-03-10 Общество с ограниченной ответственностью "Щекинский завод РТО" Method to produce gas turbine axial compressor diffuser vanes
US9890647B2 (en) * 2009-12-29 2018-02-13 Rolls-Royce North American Technologies Inc. Composite gas turbine engine component
EP2716787A1 (en) 2012-10-05 2014-04-09 Siemens Aktiengesellschaft Method for manufacturing a turbine assembly
WO2014160695A1 (en) * 2013-03-28 2014-10-02 United Technologies Corporation Gas turbine component manufacturing
WO2016064463A1 (en) * 2014-10-24 2016-04-28 Siemens Aktiengesellschaft Electrochemical machining inner contours of gas turbine engine components
US10641113B2 (en) 2015-04-08 2020-05-05 United Technologies Corporation Airfoils
CN107269580B (en) * 2017-07-26 2023-05-16 广东顺威精密塑料股份有限公司 Low-cost efficient cross flow wind wheel
US11021966B2 (en) * 2019-04-24 2021-06-01 Raytheon Technologies Corporation Vane core assemblies and methods

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3934322A (en) * 1972-09-21 1976-01-27 General Electric Company Method for forming cooling slot in airfoil blades
US3963894A (en) * 1974-01-24 1976-06-15 Chromalloy American Corporation Turbine-nozzle manufacturing apparatus
US3957104A (en) * 1974-02-27 1976-05-18 The United States Of America As Represented By The Administrator Of The United States National Aeronautics And Space Administration Method of making an apertured casting
US4188522A (en) * 1975-11-06 1980-02-12 Amchem Company Limited Method of machining a workpiece to a predetermined depth using a machining process in which machine tool wear occurs
US5152059A (en) * 1980-09-19 1992-10-06 Rolls-Royce Plc Manufacture of cooled aerofoil blades
GB2142387A (en) * 1983-07-02 1985-01-16 Rolls Royce An aerofoil for a gas turbine engine
US4672727A (en) * 1985-12-23 1987-06-16 United Technologies Corporation Method of fabricating film cooling slot in a hollow airfoil
SU1533138A1 (en) * 1986-12-19 1995-02-27 И.Л. Ровенский Gas turbine rotors production method
US4827587A (en) * 1988-01-25 1989-05-09 United Technologies Corporation Method of fabricating an air cooled turbine blade
RU2013179C1 (en) * 1990-06-05 1994-05-30 Рыбинский Авиационный Технологический Институт Method of manufacture of blades of gas-turbine engines
US5405242A (en) * 1990-07-09 1995-04-11 United Technologies Corporation Cooled vane
EP0503697B1 (en) * 1991-03-11 1995-06-21 General Motors Corporation Method for joining individual turbine blades within a multiple-property turbine rotor
US5240376A (en) * 1991-07-31 1993-08-31 Mcdonnell Douglas Corporation SPF/DB hollow core fan blade
DE69404168T2 (en) * 1993-11-24 1998-02-19 United Technologies Corp COOLED TURBINE BLADE
RU2094179C1 (en) * 1996-02-20 1997-10-27 Товарищество с ограниченной ответственностью Научно-производственное предприятие "ПУМОРИ-инструмент" Chuck for clamping axial cutting tool
JPH1052736A (en) * 1996-08-09 1998-02-24 Honda Motor Co Ltd Method for producing hollow casting by lost wax method
US6850874B1 (en) * 1998-04-17 2005-02-01 United Technologies Corporation Method and apparatus for predicting a characteristic of a product attribute formed by a machining process using a model of the process
US6162347A (en) * 1998-09-28 2000-12-19 General Electric Company Co-machined bonded airfoil
US5914060A (en) * 1998-09-29 1999-06-22 United Technologies Corporation Method of laser drilling an airfoil
US6214248B1 (en) * 1998-11-12 2001-04-10 General Electric Company Method of forming hollow channels within a component
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US6517312B1 (en) * 2000-03-23 2003-02-11 General Electric Company Turbine stator vane segment having internal cooling circuits

Also Published As

Publication number Publication date
SE0004138D0 (en) 2000-11-09
DE60132672D1 (en) 2008-03-20
WO2002038330A1 (en) 2002-05-16
SE521759C2 (en) 2003-12-02
EP1337378B1 (en) 2008-01-30
ATE385211T1 (en) 2008-02-15
US20030172530A1 (en) 2003-09-18
SE0004138L (en) 2002-05-10
US6901661B2 (en) 2005-06-07
EP1337378A1 (en) 2003-08-27
RU2003112976A (en) 2005-02-27
CA2423731A1 (en) 2002-05-16
RU2266803C2 (en) 2005-12-27

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