HK1196331A1 - 尤其用於渦輪機翼的鑲鑄冷卻特徵 - Google Patents

尤其用於渦輪機翼的鑲鑄冷卻特徵

Info

Publication number
HK1196331A1
HK1196331A1 HK14109833.6A HK14109833A HK1196331A1 HK 1196331 A1 HK1196331 A1 HK 1196331A1 HK 14109833 A HK14109833 A HK 14109833A HK 1196331 A1 HK1196331 A1 HK 1196331A1
Authority
HK
Hong Kong
Prior art keywords
cast
cooling features
turbine airfoils
features especially
airfoils
Prior art date
Application number
HK14109833.6A
Other languages
English (en)
Inventor
Boyd A Mueller
Michael A Pepper
Darren K Rogers
Gail R Cole
Original Assignee
Howmet 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 Howmet Corp filed Critical Howmet Corp
Publication of HK1196331A1 publication Critical patent/HK1196331A1/zh

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
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187Convection cooling
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C7/00Patterns; Manufacture thereof so far as not provided for in other classes
    • B22C7/02Lost patterns
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C21/00Flasks; Accessories therefor
    • B22C21/12Accessories
    • B22C21/14Accessories for reinforcing or securing moulding materials or cores, e.g. gaggers, chaplets, pins, bars
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • B22C9/02Sand moulds or like moulds for shaped castings
    • B22C9/04Use of lost patterns
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • B22C9/10Cores; Manufacture or installation of cores
    • 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
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/186Film cooling

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
HK14109833.6A 2013-03-12 2014-09-30 尤其用於渦輪機翼的鑲鑄冷卻特徵 HK1196331A1 (zh)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US13/815,595 US9835035B2 (en) 2013-03-12 2013-03-12 Cast-in cooling features especially for turbine airfoils

Publications (1)

Publication Number Publication Date
HK1196331A1 true HK1196331A1 (zh) 2014-12-12

Family

ID=50241177

Family Applications (1)

Application Number Title Priority Date Filing Date
HK14109833.6A HK1196331A1 (zh) 2013-03-12 2014-09-30 尤其用於渦輪機翼的鑲鑄冷卻特徵

Country Status (5)

Country Link
US (1) US9835035B2 (zh)
EP (1) EP2777842B1 (zh)
JP (1) JP6315553B2 (zh)
ES (1) ES2564407T3 (zh)
HK (1) HK1196331A1 (zh)

Families Citing this family (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2735387A1 (de) * 2012-11-22 2014-05-28 Siemens Aktiengesellschaft Gussform mit angeschrägten Stirnseiten bei inneren Wänden
EP3086893B1 (en) 2013-12-23 2019-07-24 United Technologies Corporation Lost core structural frame
US20150202702A1 (en) * 2014-01-17 2015-07-23 United Technologies Corporation Gas turbine engine cast structure method for finishing
RU2016137904A (ru) * 2014-02-25 2018-03-29 Сименс Акциенгезелльшафт Термобарьерное покрытие компонента турбины с изолирующими трещины техническими элементами в виде канавок
US9970319B2 (en) * 2014-05-05 2018-05-15 United Technologies Corporation Reducing variation in cooling hole meter length
US10022790B2 (en) * 2014-06-18 2018-07-17 Siemens Aktiengesellschaft Turbine airfoil cooling system with leading edge impingement cooling system turbine blade investment casting using film hole protrusions for integral wall thickness control
EP2990605A1 (de) 2014-08-26 2016-03-02 Siemens Aktiengesellschaft Turbinenschaufel
US9963975B2 (en) 2015-02-09 2018-05-08 United Technologies Corporation Trip strip restagger
WO2016133982A1 (en) 2015-02-18 2016-08-25 Siemens Aktiengesellschaft Forming cooling passages in thermal barrier coated, combustion turbine superalloy components
US10502066B2 (en) 2015-05-08 2019-12-10 United Technologies Corporation Turbine engine component including an axially aligned skin core passage interrupted by a pedestal
US10323524B2 (en) 2015-05-08 2019-06-18 United Technologies Corporation Axial skin core cooling passage for a turbine engine component
US10830052B2 (en) 2016-09-15 2020-11-10 Honeywell International Inc. Gas turbine component with cooling aperture having shaped inlet and method of forming the same
US10807154B2 (en) 2016-12-13 2020-10-20 General Electric Company Integrated casting core-shell structure for making cast component with cooling holes in inaccessible locations
US11813669B2 (en) 2016-12-13 2023-11-14 General Electric Company Method for making an integrated core-shell structure
US20180161856A1 (en) * 2016-12-13 2018-06-14 General Electric Company Integrated casting core-shell structure and filter for making cast component
US20180161852A1 (en) * 2016-12-13 2018-06-14 General Electric Company Integrated casting core-shell structure with printed tubes for making cast component
US20180161855A1 (en) * 2016-12-13 2018-06-14 General Electric Company Multi-piece integrated core-shell structure with standoff and/or bumper for making cast component
US20180161859A1 (en) * 2016-12-13 2018-06-14 General Electric Company Integrated casting core-shell structure for making cast component with non-linear holes
US20180161866A1 (en) * 2016-12-13 2018-06-14 General Electric Company Multi-piece integrated core-shell structure for making cast component
US20180161854A1 (en) 2016-12-13 2018-06-14 General Electric Company Integrated casting core-shell structure
US10934854B2 (en) 2018-09-11 2021-03-02 General Electric Company CMC component cooling cavities
US11040915B2 (en) 2018-09-11 2021-06-22 General Electric Company Method of forming CMC component cooling cavities
US10913106B2 (en) 2018-09-14 2021-02-09 Raytheon Technologies Corporation Cast-in film cooling hole structures
US20230135989A1 (en) * 2021-07-12 2023-05-04 Imagine Aero Inc. Manufacturing methods and related structures, for example useful in airframes and other structures
US11898465B2 (en) 2021-08-13 2024-02-13 Rtx Corporation Forming lined cooling aperture(s) in a turbine engine component
US11813706B2 (en) 2021-08-13 2023-11-14 Rtx Corporation Methods for forming cooling apertures in a turbine engine component
US11673200B2 (en) 2021-08-13 2023-06-13 Raytheon Technologies Corporation Forming cooling aperture(s) using electrical discharge machining
US11542831B1 (en) 2021-08-13 2023-01-03 Raytheon Technologies Corporation Energy beam positioning during formation of a cooling aperture
US11732590B2 (en) 2021-08-13 2023-08-22 Raytheon Technologies Corporation Transition section for accommodating mismatch between other sections of a cooling aperture in a turbine engine component
US11913119B2 (en) 2021-08-13 2024-02-27 Rtx Corporation Forming cooling aperture(s) in a turbine engine component
US11603769B2 (en) 2021-08-13 2023-03-14 Raytheon Technologies Corporation Forming lined cooling aperture(s) in a turbine engine component
US11998974B2 (en) * 2022-08-30 2024-06-04 General Electric Company Casting core for a cast engine component

Family Cites Families (49)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3965963A (en) * 1973-11-16 1976-06-29 United Technologies Corporation Mold and process for casting high temperature alloys
IT1096996B (it) * 1977-07-22 1985-08-26 Rolls Royce Metodo per la fabbricazione di una pala o lama per motori a turbina a gas
JPS55114439A (en) 1979-02-28 1980-09-03 Hitachi Ltd Production of turbine blade
US4283835A (en) 1980-04-02 1981-08-18 United Technologies Corporation Cambered core positioning for injection molding
US4574451A (en) * 1982-12-22 1986-03-11 General Electric Company Method for producing an article with a fluid passage
JPH02258137A (ja) 1989-03-30 1990-10-18 Mitsubishi Metal Corp ろう型法
US5394932A (en) 1992-01-17 1995-03-07 Howmet Corporation Multiple part cores for investment casting
US5295530A (en) 1992-02-18 1994-03-22 General Motors Corporation Single-cast, high-temperature, thin wall structures and methods of making the same
US5296308A (en) * 1992-08-10 1994-03-22 Howmet Corporation Investment casting using core with integral wall thickness control means
DE69327714T2 (de) 1993-04-13 2001-02-22 Martinez De Lahidalga Insausti Feingiessverfahren zur Herstellung von Gussstücken
FR2714858B1 (fr) * 1994-01-12 1996-02-09 Snecma Procédé de fabrication d'un moule carapace en matériau céramique pour fonderie à modèle perdu.
US5524696A (en) 1994-08-05 1996-06-11 General Motors Corporation Method of making a casting having an embedded preform
US5820774A (en) * 1996-10-28 1998-10-13 United Technologies Corporation Ceramic core for casting a turbine blade
DE19821770C1 (de) * 1998-05-14 1999-04-15 Siemens Ag Verfahren und Vorrichtung zur Herstellung eines metallischen Hohlkörpers
US5989476A (en) 1998-06-12 1999-11-23 3D Systems, Inc. Process of making a molded refractory article
US6206638B1 (en) * 1999-02-12 2001-03-27 General Electric Company Low cost airfoil cooling circuit with sidewall impingement cooling chambers
JP4092674B2 (ja) 1999-03-02 2008-05-28 日立金属株式会社 セラミック中子を有するワックス模型の成型方法
JP2000297606A (ja) 1999-04-13 2000-10-24 Hmy Ltd 蒸気タービン用静翼の製造方法
ATE350182T1 (de) * 1999-10-26 2007-01-15 Howmet Res Corp Mehrwandiger kern und verfahren
US6505678B2 (en) 2001-04-17 2003-01-14 Howmet Research Corporation Ceramic core with locators and method
JP2002346696A (ja) * 2001-05-24 2002-12-03 Nakakin:Kk 成形用型枠
US20030015308A1 (en) 2001-07-23 2003-01-23 Fosaaen Ken E. Core and pattern manufacture for investment casting
US6637500B2 (en) * 2001-10-24 2003-10-28 United Technologies Corporation Cores for use in precision investment casting
DE10236339B3 (de) 2002-08-08 2004-02-19 Doncasters Precision Castings-Bochum Gmbh Verfahren zum Herstellen von Turbinenschaufeln mit darin angeordneten Kühlkanälen
DE10314373A1 (de) * 2003-03-28 2004-10-07 Rwth Aachen Urfomverfahren für ein Bauteil mit Mikrostruktur-Funktionselement
US7014424B2 (en) * 2003-04-08 2006-03-21 United Technologies Corporation Turbine element
US20050006047A1 (en) 2003-07-10 2005-01-13 General Electric Company Investment casting method and cores and dies used therein
JP2005097039A (ja) * 2003-09-25 2005-04-14 Kyocera Corp セラミック焼結体の製造方法及びこれによって得られたセラミック焼結体
US7207375B2 (en) 2004-05-06 2007-04-24 United Technologies Corporation Investment casting
US20050258577A1 (en) * 2004-05-20 2005-11-24 Holowczak John E Method of producing unitary multi-element ceramic casting cores and integral core/shell system
GB0418906D0 (en) * 2004-08-25 2004-09-29 Rolls Royce Plc Internally cooled aerofoils
US7207373B2 (en) * 2004-10-26 2007-04-24 United Technologies Corporation Non-oxidizable coating
US7093645B2 (en) 2004-12-20 2006-08-22 Howmet Research Corporation Ceramic casting core and method
US7569172B2 (en) * 2005-06-23 2009-08-04 United Technologies Corporation Method for forming turbine blade with angled internal ribs
US7306026B2 (en) * 2005-09-01 2007-12-11 United Technologies Corporation Cooled turbine airfoils and methods of manufacture
US7185695B1 (en) 2005-09-01 2007-03-06 United Technologies Corporation Investment casting pattern manufacture
US20070074839A1 (en) 2005-10-03 2007-04-05 United Technologies Corporation Method for manufacturing a pattern for a hollow component
US8413709B2 (en) * 2006-12-06 2013-04-09 General Electric Company Composite core die, methods of manufacture thereof and articles manufactured therefrom
US7624787B2 (en) 2006-12-06 2009-12-01 General Electric Company Disposable insert, and use thereof in a method for manufacturing an airfoil
US7938168B2 (en) 2006-12-06 2011-05-10 General Electric Company Ceramic cores, methods of manufacture thereof and articles manufactured from the same
US7717676B2 (en) * 2006-12-11 2010-05-18 United Technologies Corporation High aspect ratio blade main core modifications for peripheral serpentine microcircuits
US7487819B2 (en) 2006-12-11 2009-02-10 General Electric Company Disposable thin wall core die, methods of manufacture thereof and articles manufactured therefrom
US8292581B2 (en) * 2008-01-09 2012-10-23 Honeywell International Inc. Air cooled turbine blades and methods of manufacturing
US7913743B2 (en) 2008-06-12 2011-03-29 Pcc Airfoils, Inc. Method of forming a pattern
JP5717627B2 (ja) * 2008-06-12 2015-05-13 アルストム テクノロジー リミテッドALSTOM Technology Ltd ガスタービンに用いられる翼ならびにこのような翼を鋳造技術により製造するための方法
US20110135446A1 (en) * 2009-12-04 2011-06-09 United Technologies Corporation Castings, Casting Cores, and Methods
US20110132562A1 (en) 2009-12-08 2011-06-09 Merrill Gary B Waxless precision casting process
US9017025B2 (en) * 2011-04-22 2015-04-28 Siemens Energy, Inc. Serpentine cooling circuit with T-shaped partitions in a turbine airfoil
US8899303B2 (en) * 2011-05-10 2014-12-02 Howmet Corporation Ceramic core with composite insert for casting airfoils

Also Published As

Publication number Publication date
JP2014208373A (ja) 2014-11-06
EP2777842B1 (en) 2016-01-20
EP2777842A1 (en) 2014-09-17
US9835035B2 (en) 2017-12-05
US20140271129A1 (en) 2014-09-18
JP6315553B2 (ja) 2018-04-25
ES2564407T3 (es) 2016-03-22

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