CN100402800C - 合成高温部件及其制造方法 - Google Patents

合成高温部件及其制造方法 Download PDF

Info

Publication number
CN100402800C
CN100402800C CNB031206530A CN03120653A CN100402800C CN 100402800 C CN100402800 C CN 100402800C CN B031206530 A CNB031206530 A CN B031206530A CN 03120653 A CN03120653 A CN 03120653A CN 100402800 C CN100402800 C CN 100402800C
Authority
CN
China
Prior art keywords
housing
component
post
column
spacer
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 - Fee Related
Application number
CNB031206530A
Other languages
English (en)
Chinese (zh)
Other versions
CN1445437A (zh
Inventor
J·-C·赵
L·姜
M·R·杰克逊
R·达罗利尔
R·E·沙夫里克
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of CN1445437A publication Critical patent/CN1445437A/zh
Application granted granted Critical
Publication of CN100402800C publication Critical patent/CN100402800C/zh
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

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
    • 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
    • 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
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • 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
    • F05D2300/00Materials; Properties thereof
    • F05D2300/10Metals, alloys or intermetallic compounds
    • F05D2300/14Noble metals, i.e. Ag, Au, platinum group metals
    • F05D2300/143Platinum group metals, i.e. Os, Ir, Pt, Ru, Rh, Pd
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CNB031206530A 2002-03-18 2003-03-18 合成高温部件及其制造方法 Expired - Fee Related CN100402800C (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/063,091 US6726444B2 (en) 2002-03-18 2002-03-18 Hybrid high temperature articles and method of making
US10/063091 2002-03-18

Publications (2)

Publication Number Publication Date
CN1445437A CN1445437A (zh) 2003-10-01
CN100402800C true CN100402800C (zh) 2008-07-16

Family

ID=27787422

Family Applications (1)

Application Number Title Priority Date Filing Date
CNB031206530A Expired - Fee Related CN100402800C (zh) 2002-03-18 2003-03-18 合成高温部件及其制造方法

Country Status (4)

Country Link
US (1) US6726444B2 (https=)
EP (1) EP1347151B1 (https=)
JP (1) JP4360484B2 (https=)
CN (1) CN100402800C (https=)

Families Citing this family (42)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7189459B2 (en) * 2002-12-31 2007-03-13 General Electric Company Turbine blade for extreme temperature conditions
US20050158171A1 (en) * 2004-01-15 2005-07-21 General Electric Company Hybrid ceramic matrix composite turbine blades for improved processibility and performance
US20050282032A1 (en) * 2004-06-18 2005-12-22 General Electric Company Smooth outer coating for combustor components and coating method therefor
US20060040129A1 (en) * 2004-08-20 2006-02-23 General Electric Company Article protected by a strong local coating
DE102005002671B3 (de) * 2005-01-14 2006-06-22 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Turbinenschaufel für Strömungsmaschinen und Verfahren zu ihrer Herstellung
US20060188736A1 (en) * 2005-02-18 2006-08-24 General Electric Company Diffusion barrier for assemblies with metallic and silicon-containing components and method therefor
EP1847696A1 (de) * 2006-04-21 2007-10-24 Siemens Aktiengesellschaft Bauteil für eine gestufte Verbrennung in einer Gasturbine und entsprechende Gasturbine.
US20080085191A1 (en) * 2006-10-05 2008-04-10 Siemens Power Generation, Inc. Thermal barrier coating system for a turbine airfoil usable in a turbine engine
EP1942250A1 (de) * 2007-01-05 2008-07-09 Siemens Aktiengesellschaft Bauteil mit schräg verlaufenden Vertiefungen in der Oberfläche und Verfahren zum Betreiben einer Turbine
US7766617B1 (en) * 2007-03-06 2010-08-03 Florida Turbine Technologies, Inc. Transpiration cooled turbine airfoil
US8047789B1 (en) 2007-10-19 2011-11-01 Florida Turbine Technologies, Inc. Turbine airfoil
US20110059321A1 (en) * 2008-06-23 2011-03-10 General Electric Company Method of repairing a thermal barrier coating and repaired coating formed thereby
US8033790B2 (en) 2008-09-26 2011-10-11 Siemens Energy, Inc. Multiple piece turbine engine airfoil with a structural spar
US8007242B1 (en) * 2009-03-16 2011-08-30 Florida Turbine Technologies, Inc. High temperature turbine rotor blade
US8091419B2 (en) * 2009-03-20 2012-01-10 United Technologies Corporation Fluid pressure operated fixture
US8052391B1 (en) * 2009-03-25 2011-11-08 Florida Turbine Technologies, Inc. High temperature turbine rotor blade
US8206109B2 (en) * 2009-03-30 2012-06-26 General Electric Company Turbine blade assemblies with thermal insulation
US8070450B1 (en) * 2009-04-20 2011-12-06 Florida Turbine Technologies, Inc. High temperature turbine rotor blade
US8387245B2 (en) * 2010-11-10 2013-03-05 General Electric Company Components with re-entrant shaped cooling channels and methods of manufacture
FR2971178B1 (fr) * 2011-02-09 2014-01-10 Snecma Procede de production d'aube de guidage
US8870523B2 (en) * 2011-03-07 2014-10-28 General Electric Company Method for manufacturing a hot gas path component and hot gas path turbine component
US8528208B2 (en) * 2011-04-11 2013-09-10 General Electric Company Methods of fabricating a coated component using multiple types of fillers
US9925584B2 (en) * 2011-09-29 2018-03-27 United Technologies Corporation Method and system for die casting a hybrid component
DE102012209549A1 (de) * 2012-06-06 2013-12-12 Siemens Aktiengesellschaft Kühlmittelüberbrückungsleitung für eine Gasturbine
US9428650B2 (en) 2012-12-11 2016-08-30 General Electric Company Environmental barrier coatings and methods therefor
US10072503B2 (en) 2013-08-14 2018-09-11 Elwha Llc Dual element turbine blade
US10145245B2 (en) * 2013-09-24 2018-12-04 United Technologies Corporation Bonded multi-piece gas turbine engine component
US9561986B2 (en) 2013-10-31 2017-02-07 General Electric Company Silica-forming articles having engineered surfaces to enhance resistance to creep sliding under high-temperature loading
US9718735B2 (en) * 2015-02-03 2017-08-01 General Electric Company CMC turbine components and methods of forming CMC turbine components
US10233126B2 (en) * 2015-08-12 2019-03-19 Rolls-Royce Corporation Forming a ceramic matrix composite having a silicide layer
US20170145831A1 (en) * 2015-11-24 2017-05-25 General Electric Company Gas turbine engine with film holes
CN108699914A (zh) * 2016-02-19 2018-10-23 西门子股份公司 具有冷却通道的混合部件及对应方法
US10436048B2 (en) 2016-08-12 2019-10-08 General Electric Comapny Systems for removing heat from turbine components
US10443397B2 (en) 2016-08-12 2019-10-15 General Electric Company Impingement system for an airfoil
US10408062B2 (en) 2016-08-12 2019-09-10 General Electric Company Impingement system for an airfoil
US10364685B2 (en) 2016-08-12 2019-07-30 Gneral Electric Company Impingement system for an airfoil
US10648341B2 (en) 2016-11-15 2020-05-12 Rolls-Royce Corporation Airfoil leading edge impingement cooling
US10465526B2 (en) 2016-11-15 2019-11-05 Rolls-Royce Corporation Dual-wall airfoil with leading edge cooling slot
US11187105B2 (en) * 2017-02-09 2021-11-30 General Electric Company Apparatus with thermal break
US11047240B2 (en) * 2017-05-11 2021-06-29 General Electric Company CMC components having microchannels and methods for forming microchannels in CMC components
US10450873B2 (en) 2017-07-31 2019-10-22 Rolls-Royce Corporation Airfoil edge cooling channels
US11512601B2 (en) * 2020-05-18 2022-11-29 Raytheon Technologies Corporation Airfoil vane with coated jumper tube

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5328331A (en) * 1993-06-28 1994-07-12 General Electric Company Turbine airfoil with double shell outer wall
US5626462A (en) * 1995-01-03 1997-05-06 General Electric Company Double-wall airfoil
US6168871B1 (en) * 1998-03-06 2001-01-02 General Electric Company Method of forming high-temperature components and components formed thereby

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3423069A (en) 1967-09-29 1969-01-21 Trw Inc Airfoil
US3647316A (en) * 1970-04-28 1972-03-07 Curtiss Wright Corp Variable permeability and oxidation-resistant airfoil
US4376004A (en) * 1979-01-16 1983-03-08 Westinghouse Electric Corp. Method of manufacturing a transpiration cooled ceramic blade for a gas turbine
DE3327218A1 (de) * 1983-07-28 1985-02-07 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Thermisch hochbeanspruchtes, gekuehltes bauteil, insbesondere turbinenschaufel
US5125793A (en) * 1991-07-08 1992-06-30 The United States Of America As Represented By The Secretary Of The Air Force Turbine blade cooling with endothermic fuel
US5338577A (en) * 1993-05-14 1994-08-16 Kemira, Inc. Metal with ceramic coating and method
US6003754A (en) 1997-10-21 1999-12-21 Allison Advanced Development Co. Airfoil for a gas turbine engine and method of manufacture
US6565312B1 (en) * 2001-12-19 2003-05-20 The Boeing Company Fluid-cooled turbine blades

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5328331A (en) * 1993-06-28 1994-07-12 General Electric Company Turbine airfoil with double shell outer wall
US5626462A (en) * 1995-01-03 1997-05-06 General Electric Company Double-wall airfoil
US6168871B1 (en) * 1998-03-06 2001-01-02 General Electric Company Method of forming high-temperature components and components formed thereby

Also Published As

Publication number Publication date
CN1445437A (zh) 2003-10-01
US6726444B2 (en) 2004-04-27
JP4360484B2 (ja) 2009-11-11
US20030175122A1 (en) 2003-09-18
EP1347151B1 (en) 2012-12-12
JP2004036606A (ja) 2004-02-05
EP1347151A2 (en) 2003-09-24
EP1347151A3 (en) 2004-12-15

Similar Documents

Publication Publication Date Title
CN100402800C (zh) 合成高温部件及其制造方法
US6609894B2 (en) Airfoils with improved oxidation resistance and manufacture and repair thereof
US6908288B2 (en) Repair of advanced gas turbine blades
CN100534778C (zh) 用于散热的高温涂层系统及其制造方法
US6464456B2 (en) Turbine vane assembly including a low ductility vane
CN102562176B (zh) 用于在高温构件内提供流体冷却系统的方法及高温构件
US7900458B2 (en) Turbine airfoils with near surface cooling passages and method of making same
RU2423544C2 (ru) Многослойное термобарьерное покрытие для детали из сплава на основе кобальта или никеля и деталь
JP4981256B2 (ja) 燃焼器組立体を製作するための燃焼器部材及び方法
US8876481B2 (en) Turbine airfoil component assembly for use in a gas turbine engine and methods for fabricating same
CN102695818B (zh) 纳米和微米结构的陶瓷绝热涂层
CN1890456B (zh) 带有绝热层和抗侵蚀保护层的部件
US6720088B2 (en) Materials for protection of substrates at high temperature, articles made therefrom, and method for protecting substrates
CN102272354B (zh) 具有不同铬含量和铝含量的MCrAlX-层
JP2008544127A (ja) 部品に対する断熱層と金属浸食防護層とを備えた被覆系と、その被覆系の製造方法と、蒸気タービンの運転方法
CN106906471A (zh) 具有改进的隔热涂层系统的燃气涡轮构件
CN103797141A (zh) 合金、保护层和构件
CN100535166C (zh) 金属保护层
CN101133173A (zh) 合金,防止构件高温腐蚀和/或氧化的保护层及构件
CN103774134A (zh) 具有隔热涂层的燃气轮机用高温部件
JP2018184945A (ja) ハイブリッド被覆システムを有する構成要素および構成要素を形成するための方法
JP2005054271A (ja) 高温用途のための合金、これから作られた物品、及び物品を修理する方法
CN101356137A (zh) 陶瓷实心构件和具有高孔隙度的陶瓷层以及该层的应用和含该层的构件
US20100209733A1 (en) Hot Gas-Guided Component of a Turbomachine
EP1457579B1 (en) Materials for protection of superalloy substrates at high temperature, articles made therefrom, and method for protecting substrates

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20080716

Termination date: 20170318