KR100527685B1 - 가스 터빈의 세라믹 매트릭스 복합체에 대한 고온절연물의 사용 - Google Patents

가스 터빈의 세라믹 매트릭스 복합체에 대한 고온절연물의 사용 Download PDF

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Publication number
KR100527685B1
KR100527685B1 KR10-2000-7010756A KR20007010756A KR100527685B1 KR 100527685 B1 KR100527685 B1 KR 100527685B1 KR 20007010756 A KR20007010756 A KR 20007010756A KR 100527685 B1 KR100527685 B1 KR 100527685B1
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KR
South Korea
Prior art keywords
composition
gas turbine
bonded
filler powder
ceramic
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
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KR10-2000-7010756A
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English (en)
Korean (ko)
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KR20010042230A (ko
Inventor
모리슨제이알란
메릴게리브리앙
루드만에반맥닐
래인제이에드가
Original Assignee
지멘스 웨스팅하우스 파워 코포레이션
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Publication of KR20010042230A publication Critical patent/KR20010042230A/ko
Application granted granted Critical
Publication of KR100527685B1 publication Critical patent/KR100527685B1/ko
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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
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/12Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B28/00Compositions of mortars, concrete or artificial stone, containing inorganic binders or the reaction product of an inorganic and an organic binder, e.g. polycarboxylate cements
    • C04B28/34Compositions of mortars, concrete or artificial stone, containing inorganic binders or the reaction product of an inorganic and an organic binder, e.g. polycarboxylate cements containing cold phosphate binders
    • C04B28/344Compositions of mortars, concrete or artificial stone, containing inorganic binders or the reaction product of an inorganic and an organic binder, e.g. polycarboxylate cements containing cold phosphate binders the phosphate binder being present in the starting composition solely as one or more phosphates
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B38/00Porous mortars, concrete, artificial stone or ceramic ware; Preparation thereof
    • C04B38/08Porous mortars, concrete, artificial stone or ceramic ware; Preparation thereof by adding porous substances
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2111/00Mortars, concrete or artificial stone or mixtures to prepare them, characterised by specific function, property or use
    • C04B2111/00474Uses not provided for elsewhere in C04B2111/00
    • C04B2111/00482Coating or impregnation materials
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2111/00Mortars, concrete or artificial stone or mixtures to prepare them, characterised by specific function, property or use
    • C04B2111/20Resistance against chemical, physical or biological attack
    • C04B2111/28Fire resistance, i.e. materials resistant to accidental fires or high temperatures
    • 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
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/29Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
    • Y10T428/2982Particulate matter [e.g., sphere, flake, etc.]

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Materials Engineering (AREA)
  • Structural Engineering (AREA)
  • Organic Chemistry (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Inorganic Chemistry (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
KR10-2000-7010756A 1998-03-27 1999-02-11 가스 터빈의 세라믹 매트릭스 복합체에 대한 고온절연물의 사용 Expired - Fee Related KR100527685B1 (ko)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US9/049,369 1998-03-27
US09/049,369 US6197424B1 (en) 1998-03-27 1998-03-27 Use of high temperature insulation for ceramic matrix composites in gas turbines
US09/049,369 1998-03-27

Publications (2)

Publication Number Publication Date
KR20010042230A KR20010042230A (ko) 2001-05-25
KR100527685B1 true KR100527685B1 (ko) 2005-11-25

Family

ID=21959450

Family Applications (1)

Application Number Title Priority Date Filing Date
KR10-2000-7010756A Expired - Fee Related KR100527685B1 (ko) 1998-03-27 1999-02-11 가스 터빈의 세라믹 매트릭스 복합체에 대한 고온절연물의 사용

Country Status (6)

Country Link
US (1) US6197424B1 (enExample)
EP (1) EP1068161B1 (enExample)
JP (1) JP4318858B2 (enExample)
KR (1) KR100527685B1 (enExample)
DE (1) DE69901440T2 (enExample)
WO (1) WO1999048837A1 (enExample)

Families Citing this family (148)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6733907B2 (en) 1998-03-27 2004-05-11 Siemens Westinghouse Power Corporation Hybrid ceramic material composed of insulating and structural ceramic layers
US7067181B2 (en) * 2003-08-05 2006-06-27 Siemens Power Generation, Inc. Insulating ceramic based on partially filled shapes
US6641907B1 (en) * 1999-12-20 2003-11-04 Siemens Westinghouse Power Corporation High temperature erosion resistant coating and material containing compacted hollow geometric shapes
US6977060B1 (en) * 2000-03-28 2005-12-20 Siemens Westinghouse Power Corporation Method for making a high temperature erosion resistant coating and material containing compacted hollow geometric shapes
US7563504B2 (en) * 1998-03-27 2009-07-21 Siemens Energy, Inc. Utilization of discontinuous fibers for improving properties of high temperature insulation of ceramic matrix composites
US6676783B1 (en) * 1998-03-27 2004-01-13 Siemens Westinghouse Power Corporation High temperature insulation for ceramic matrix composites
US6485848B1 (en) * 1998-04-27 2002-11-26 General Electric Company Coated article and method of making
US6697130B2 (en) * 2001-01-16 2004-02-24 Visteon Global Technologies, Inc. Flexible led backlighting circuit
US6746755B2 (en) * 2001-09-24 2004-06-08 Siemens Westinghouse Power Corporation Ceramic matrix composite structure having integral cooling passages and method of manufacture
US6884384B2 (en) 2001-09-27 2005-04-26 Siemens Westinghouse Power Corporation Method for making a high temperature erosion resistant material containing compacted hollow geometric shapes
US20030112931A1 (en) * 2001-12-19 2003-06-19 Wendell Brown Facilitating navigation of an interactive voice response (IVR) menu to establish a telephone connection
US6495207B1 (en) 2001-12-21 2002-12-17 Pratt & Whitney Canada Corp. Method of manufacturing a composite wall
US6759151B1 (en) * 2002-05-22 2004-07-06 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Multilayer article characterized by low coefficient of thermal expansion outer layer
US6709230B2 (en) * 2002-05-31 2004-03-23 Siemens Westinghouse Power Corporation Ceramic matrix composite gas turbine vane
US6648597B1 (en) 2002-05-31 2003-11-18 Siemens Westinghouse Power Corporation Ceramic matrix composite turbine vane
GB0226997D0 (en) * 2002-11-19 2002-12-24 Welding Inst Heat resistant product
JP2004036443A (ja) * 2002-07-02 2004-02-05 Ishikawajima Harima Heavy Ind Co Ltd ガスタービンシュラウド構造
US6929852B2 (en) * 2002-08-08 2005-08-16 Siemens Westinghouse Power Corporation Protective overlayer for ceramics
DE10239631A1 (de) * 2002-08-23 2004-03-04 Carcoustics Tech Center Gmbh Isolierbauteil zur Wärme- und/oder Schallisolierung mit feuerhemmender Beschichtung
US6758653B2 (en) 2002-09-09 2004-07-06 Siemens Westinghouse Power Corporation Ceramic matrix composite component for a gas turbine engine
US7093359B2 (en) 2002-09-17 2006-08-22 Siemens Westinghouse Power Corporation Composite structure formed by CMC-on-insulation process
US9068464B2 (en) * 2002-09-17 2015-06-30 Siemens Energy, Inc. Method of joining ceramic parts and articles so formed
US7270890B2 (en) 2002-09-23 2007-09-18 Siemens Power Generation, Inc. Wear monitoring system with embedded conductors
US6838157B2 (en) 2002-09-23 2005-01-04 Siemens Westinghouse Power Corporation Method and apparatus for instrumenting a gas turbine component having a barrier coating
US7618712B2 (en) * 2002-09-23 2009-11-17 Siemens Energy, Inc. Apparatus and method of detecting wear in an abradable coating system
US20050198967A1 (en) * 2002-09-23 2005-09-15 Siemens Westinghouse Power Corp. Smart component for use in an operating environment
US7582359B2 (en) * 2002-09-23 2009-09-01 Siemens Energy, Inc. Apparatus and method of monitoring operating parameters of a gas turbine
US8151623B2 (en) 2002-09-23 2012-04-10 Siemens Energy, Inc. Sensor for quantifying widening reduction wear on a surface
US7572524B2 (en) * 2002-09-23 2009-08-11 Siemens Energy, Inc. Method of instrumenting a component
US7094027B2 (en) * 2002-11-27 2006-08-22 General Electric Company Row of long and short chord length and high and low temperature capability turbine airfoils
US6893750B2 (en) 2002-12-12 2005-05-17 General Electric Company Thermal barrier coating protected by alumina and method for preparing same
US6767659B1 (en) 2003-02-27 2004-07-27 Siemens Westinghouse Power Corporation Backside radiative cooled ceramic matrix composite component
US7871716B2 (en) * 2003-04-25 2011-01-18 Siemens Energy, Inc. Damage tolerant gas turbine component
US7198860B2 (en) * 2003-04-25 2007-04-03 Siemens Power Generation, Inc. Ceramic tile insulation for gas turbine component
US7311790B2 (en) * 2003-04-25 2007-12-25 Siemens Power Generation, Inc. Hybrid structure using ceramic tiles and method of manufacture
US7108925B2 (en) * 2003-09-22 2006-09-19 Siemens Power Generation, Inc. High temperature insulation utilizing zirconia-hafnia
US7985493B2 (en) * 2003-09-22 2011-07-26 Siemens Energy, Inc. High temperature insulation and insulated article
US7064825B2 (en) * 2003-11-25 2006-06-20 General Electric Company Methods and apparatus for evaluating rotary machinery
US6997673B2 (en) * 2003-12-11 2006-02-14 Honeywell International, Inc. Gas turbine high temperature turbine blade outer air seal assembly
US8315834B2 (en) * 2003-12-17 2012-11-20 Siemens Energy, Inc. System and method for measuring coating thickness
US7351364B2 (en) * 2004-01-29 2008-04-01 Siemens Power Generation, Inc. Method of manufacturing a hybrid structure
US7066717B2 (en) * 2004-04-22 2006-06-27 Siemens Power Generation, Inc. Ceramic matrix composite airfoil trailing edge arrangement
US7334330B2 (en) * 2004-04-28 2008-02-26 Siemens Power Generation, Inc. Thermally insulating layer incorporating a distinguishing agent and method for inspecting the same
DE102004023623A1 (de) * 2004-05-10 2005-12-01 Alstom Technology Ltd Strömungsmaschinenschaufel
US8004423B2 (en) * 2004-06-21 2011-08-23 Siemens Energy, Inc. Instrumented component for use in an operating environment
US8742944B2 (en) * 2004-06-21 2014-06-03 Siemens Energy, Inc. Apparatus and method of monitoring operating parameters of a gas turbine
US7247002B2 (en) * 2004-12-02 2007-07-24 Siemens Power Generation, Inc. Lamellate CMC structure with interlock to metallic support structure
US7402347B2 (en) * 2004-12-02 2008-07-22 Siemens Power Generation, Inc. In-situ formed thermal barrier coating for a ceramic component
US7314674B2 (en) * 2004-12-15 2008-01-01 General Electric Company Corrosion resistant coating composition, coated turbine component and method for coating same
US7310938B2 (en) * 2004-12-16 2007-12-25 Siemens Power Generation, Inc. Cooled gas turbine transition duct
US7435058B2 (en) * 2005-01-18 2008-10-14 Siemens Power Generation, Inc. Ceramic matrix composite vane with chordwise stiffener
US20060166019A1 (en) * 2005-01-21 2006-07-27 Irene Spitsberg Thermal/environmental barrier coating for silicon-comprising materials
US7258530B2 (en) * 2005-01-21 2007-08-21 Siemens Power Generation, Inc. CMC component and method of fabrication
US7449254B2 (en) * 2005-01-21 2008-11-11 General Electric Company Environmental barrier coating with physical barrier layer for silicon-comprising materials
US7326468B2 (en) * 2005-01-21 2008-02-05 General Electric Company Thermal/environmental barrier coating for silicon-comprising materials
US7115326B2 (en) * 2005-01-21 2006-10-03 General Electric Company Thermal/environmental barrier coating with transition layer for silicon-comprising materials
US7115327B2 (en) 2005-01-21 2006-10-03 General Electric Company Thermal/environmental barrier coating with transition layer for silicon-comprising materials
US7300621B2 (en) * 2005-03-16 2007-11-27 Siemens Power Generation, Inc. Method of making a ceramic matrix composite utilizing partially stabilized fibers
US8137611B2 (en) * 2005-03-17 2012-03-20 Siemens Energy, Inc. Processing method for solid core ceramic matrix composite airfoil
US20060280954A1 (en) * 2005-06-13 2006-12-14 Irene Spitsberg Corrosion resistant sealant for outer EBL of silicon-containing substrate and processes for preparing same
US20060280955A1 (en) * 2005-06-13 2006-12-14 Irene Spitsberg Corrosion resistant sealant for EBC of silicon-containing substrate and processes for preparing same
US7550107B2 (en) * 2005-07-25 2009-06-23 Siemens Energy, Inc. Method of forming CMC component
US7785076B2 (en) * 2005-08-30 2010-08-31 Siemens Energy, Inc. Refractory component with ceramic matrix composite skeleton
US7754342B2 (en) * 2005-12-19 2010-07-13 General Electric Company Strain tolerant corrosion protecting coating and spray method of application
US7604867B2 (en) * 2005-12-20 2009-10-20 General Electric Company Particulate corrosion resistant coating composition, coated turbine component and method for coating same
US20080026248A1 (en) * 2006-01-27 2008-01-31 Shekar Balagopal Environmental and Thermal Barrier Coating to Provide Protection in Various Environments
US7942639B2 (en) * 2006-03-31 2011-05-17 General Electric Company Hybrid bucket dovetail pocket design for mechanical retainment
US7604456B2 (en) * 2006-04-11 2009-10-20 Siemens Energy, Inc. Vane shroud through-flow platform cover
US7534086B2 (en) * 2006-05-05 2009-05-19 Siemens Energy, Inc. Multi-layer ring seal
US7726936B2 (en) * 2006-07-25 2010-06-01 Siemens Energy, Inc. Turbine engine ring seal
US7641440B2 (en) * 2006-08-31 2010-01-05 Siemens Energy, Inc. Cooling arrangement for CMC components with thermally conductive layer
US7368827B2 (en) * 2006-09-06 2008-05-06 Siemens Power Generation, Inc. Electrical assembly for monitoring conditions in a combustion turbine operating environment
US7969323B2 (en) * 2006-09-14 2011-06-28 Siemens Energy, Inc. Instrumented component for combustion turbine engine
US7753643B2 (en) * 2006-09-22 2010-07-13 Siemens Energy, Inc. Stacked laminate bolted ring segment
US20080072569A1 (en) * 2006-09-27 2008-03-27 Thomas Ory Moniz Guide vane and method of fabricating the same
US7950234B2 (en) * 2006-10-13 2011-05-31 Siemens Energy, Inc. Ceramic matrix composite turbine engine components with unitary stiffening frame
US20100119777A1 (en) * 2006-11-16 2010-05-13 Siemens Power Generation, Inc. Ceramic matrix composite surfaces with open features for improved bonding to coatings
US20080274336A1 (en) * 2006-12-01 2008-11-06 Siemens Power Generation, Inc. High temperature insulation with enhanced abradability
US20080199661A1 (en) * 2007-02-15 2008-08-21 Siemens Power Generation, Inc. Thermally insulated CMC structure with internal cooling
US7887300B2 (en) * 2007-02-27 2011-02-15 Siemens Energy, Inc. CMC airfoil with thin trailing edge
US8257809B2 (en) 2007-03-08 2012-09-04 Siemens Energy, Inc. CMC wall structure with integral cooling channels
US7819625B2 (en) * 2007-05-07 2010-10-26 Siemens Energy, Inc. Abradable CMC stacked laminate ring segment for a gas turbine
US7648605B2 (en) * 2007-05-17 2010-01-19 Siemens Energy, Inc. Process for applying a thermal barrier coating to a ceramic matrix composite
US9447503B2 (en) 2007-05-30 2016-09-20 United Technologies Corporation Closed pore ceramic composite article
US20100021716A1 (en) * 2007-06-19 2010-01-28 Strock Christopher W Thermal barrier system and bonding method
US7908867B2 (en) * 2007-09-14 2011-03-22 Siemens Energy, Inc. Wavy CMC wall hybrid ceramic apparatus
US8128350B2 (en) * 2007-09-21 2012-03-06 Siemens Energy, Inc. Stacked lamellae ceramic gas turbine ring segment component
US9071888B2 (en) * 2007-11-08 2015-06-30 Siemens Aktiengesellschaft Instrumented component for wireless telemetry
US8519866B2 (en) 2007-11-08 2013-08-27 Siemens Energy, Inc. Wireless telemetry for instrumented component
US8797179B2 (en) * 2007-11-08 2014-08-05 Siemens Aktiengesellschaft Instrumented component for wireless telemetry
FR2929690B1 (fr) * 2008-04-03 2012-08-17 Snecma Propulsion Solide Chambre de combustion sectorisee en cmc pour turbine a gaz
US8202588B2 (en) * 2008-04-08 2012-06-19 Siemens Energy, Inc. Hybrid ceramic structure with internal cooling arrangements
US9127565B2 (en) * 2008-04-16 2015-09-08 Siemens Energy, Inc. Apparatus comprising a CMC-comprising body and compliant porous element preloaded within an outer metal shell
US8366983B2 (en) * 2008-07-22 2013-02-05 Siemens Energy, Inc. Method of manufacturing a thermal insulation article
US20100021643A1 (en) * 2008-07-22 2010-01-28 Siemens Power Generation, Inc. Method of Forming a Turbine Engine Component Having a Vapor Resistant Layer
US8333812B2 (en) * 2008-08-18 2012-12-18 Forestwood Industrial, Inc. Method and device for use of hollow spheres in a composite material
US20100047526A1 (en) * 2008-08-19 2010-02-25 Merrill Gary B Subsurface inclusions of spheroids and methodology for strengthening a surface bond in a hybrid ceramic matrix composite structure
US20100047512A1 (en) * 2008-08-19 2010-02-25 Morrison Jay A Methodology and tooling arrangements for strengthening a surface bond in a hybrid ceramic matrix composite structure
US8118546B2 (en) * 2008-08-20 2012-02-21 Siemens Energy, Inc. Grid ceramic matrix composite structure for gas turbine shroud ring segment
US20100061847A1 (en) * 2008-09-09 2010-03-11 General Electric Company Steam turbine part including ceramic matrix composite (cmc)
US20100069226A1 (en) * 2008-09-17 2010-03-18 General Electric Company Rare earth phosphate bonded ceramics
US7704596B2 (en) 2008-09-23 2010-04-27 Siemens Energy, Inc. Subsurface inclusion of fugitive objects and methodology for strengthening a surface bond in a hybrid ceramic matrix composite structure
US8382436B2 (en) * 2009-01-06 2013-02-26 General Electric Company Non-integral turbine blade platforms and systems
US8251651B2 (en) 2009-01-28 2012-08-28 United Technologies Corporation Segmented ceramic matrix composite turbine airfoil component
US8262345B2 (en) * 2009-02-06 2012-09-11 General Electric Company Ceramic matrix composite turbine engine
US8177513B2 (en) * 2009-02-18 2012-05-15 General Electric Company Method and apparatus for a structural outlet guide vane
GB0911500D0 (en) * 2009-07-03 2009-08-12 Rolls Royce Plc Rotor blade over-tip leakage control
US8256088B2 (en) * 2009-08-24 2012-09-04 Siemens Energy, Inc. Joining mechanism with stem tension and interlocked compression ring
US9085991B2 (en) * 2009-11-06 2015-07-21 Honeywell International Inc. Protective coatings for ceramic matrix composite substrates and methods for improving the wear resistance thereof and coated articles produced therefrom
US8678771B2 (en) * 2009-12-14 2014-03-25 Siemens Energy, Inc. Process for manufacturing a component
US8571813B2 (en) * 2010-03-16 2013-10-29 Siemens Energy, Inc. Fiber optic sensor system for detecting surface wear
US20110232298A1 (en) * 2010-03-23 2011-09-29 General Electric Company System and method for cooling gas turbine components
US9279340B2 (en) 2010-03-23 2016-03-08 General Electric Company System and method for cooling gas turbine components
EP2418357A1 (en) * 2010-08-05 2012-02-15 Siemens Aktiengesellschaft Turbine airfoil and method for thermal barrier coating
US8347636B2 (en) 2010-09-24 2013-01-08 General Electric Company Turbomachine including a ceramic matrix composite (CMC) bridge
DE102010047254B4 (de) * 2010-10-01 2017-02-02 Doka Industrie Gmbh Holzverbundwerkstoff
US8790067B2 (en) 2011-04-27 2014-07-29 United Technologies Corporation Blade clearance control using high-CTE and low-CTE ring members
US8864492B2 (en) 2011-06-23 2014-10-21 United Technologies Corporation Reverse flow combustor duct attachment
US8739547B2 (en) 2011-06-23 2014-06-03 United Technologies Corporation Gas turbine engine joint having a metallic member, a CMC member, and a ceramic key
US9335051B2 (en) 2011-07-13 2016-05-10 United Technologies Corporation Ceramic matrix composite combustor vane ring assembly
US8920127B2 (en) 2011-07-18 2014-12-30 United Technologies Corporation Turbine rotor non-metallic blade attachment
DE102011081323B3 (de) * 2011-08-22 2012-06-21 Siemens Aktiengesellschaft Laufschaufel für eine Strömungsmaschine und Strömungsmaschine mit der Laufschaufel
JP6082755B2 (ja) 2011-12-19 2017-02-15 プラックセアー エス.ティ.テクノロジー、 インコーポレイテッド 遮熱及び耐環境コーティングを生成するための水性スラリー並びにこれを作製及び適用するための方法
US9325388B2 (en) 2012-06-21 2016-04-26 Siemens Energy, Inc. Wireless telemetry system including an induction power system
US20150004308A1 (en) * 2013-06-27 2015-01-01 Gary B. Merrill Method for creating a textured bond coat surface
US10072503B2 (en) 2013-08-14 2018-09-11 Elwha Llc Dual element turbine blade
US9420356B2 (en) 2013-08-27 2016-08-16 Siemens Energy, Inc. Wireless power-receiving assembly for a telemetry system in a high-temperature environment of a combustion turbine engine
FR3016188B1 (fr) 2014-01-09 2016-01-01 Snecma Protection contre le feu d'une piece en materiau composite tisse tridimensionnel
FR3023362A1 (fr) 2014-07-04 2016-01-08 Commissariat Energie Atomique Absorbeur solaire selectif a couche epaisse de passivation anticorrosion et barriere thermique pour des applications hautes temperatures et son procede de realisation.
US10401028B2 (en) * 2015-06-05 2019-09-03 Rolls-Royce American Technologies, Inc. Machinable CMC insert
US9810434B2 (en) * 2016-01-21 2017-11-07 Siemens Energy, Inc. Transition duct system with arcuate ceramic liner for delivering hot-temperature gases in a combustion turbine engine
JP6550000B2 (ja) 2016-02-26 2019-07-24 三菱日立パワーシステムズ株式会社 タービン翼
EP3333142A1 (en) * 2016-12-09 2018-06-13 Siemens Aktiengesellschaft Co-sintering a ceramic layer upon a cmc substrate
US10392946B2 (en) * 2016-12-21 2019-08-27 Rolls-Royce North American Technologies Inc. Turbine blade with reinforced platform for composite material construction
EP3480011A1 (en) * 2017-11-02 2019-05-08 Siemens Aktiengesellschaft Method to create a good bonding between a free standing thermal barrier coating and a green cmc
GB201804569D0 (en) 2018-03-22 2018-05-09 Rolls Royce Plc Casing assembly
GB201813080D0 (en) * 2018-08-10 2018-09-26 Rolls Royce Plc Effcient gas turbine engine
GB201813082D0 (en) 2018-08-10 2018-09-26 Rolls Royce Plc Efficient gas turbine engine
GB201813081D0 (en) 2018-08-10 2018-09-26 Rolls Royce Plc Efficient gas turbine engine
GB201813086D0 (en) 2018-08-10 2018-09-26 Rolls Royce Plc Efficient gas turbine engine
GB201813084D0 (en) * 2018-08-10 2018-09-26 Rolls Royce Plc Efficent gas turbine engine
GB201813079D0 (en) 2018-08-10 2018-09-26 Rolls Royce Plc Effcient gas turbine engine
EP3683406B1 (en) 2019-01-18 2023-11-29 Ansaldo Energia Switzerland AG Abradable hybrid material, particularly for seal elements in gas turbines, and manufacturing method thereof
US11060478B2 (en) * 2019-05-30 2021-07-13 Ford Global Technologies, Llc System for an integrated hybrid composite cylinder head and turbine
US11286792B2 (en) * 2019-07-30 2022-03-29 Rolls-Royce Plc Ceramic matrix composite vane with cooling holes and methods of making the same
US11333037B2 (en) * 2020-02-06 2022-05-17 Raytheon Technologies Corporation Vane arc segment load path
US11203947B2 (en) * 2020-05-08 2021-12-21 Raytheon Technologies Corporation Airfoil having internally cooled wall with liner and shell
US20240375394A1 (en) * 2023-05-12 2024-11-14 Raytheon Technologies Corporation Ceramic matrix composite sandwich structure reinforced with z-tows

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3053694A (en) 1961-02-20 1962-09-11 Gen Electric Abradable material
US3975165A (en) 1973-12-26 1976-08-17 Union Carbide Corporation Graded metal-to-ceramic structure for high temperature abradable seal applications and a method of producing said
GB1525037A (en) 1976-07-06 1978-09-20 Inst Vysokikh Temperatur Akade Manufacture of heat-resistant materials
US4177308A (en) 1978-08-10 1979-12-04 The United States Of America As Represented By The Secretary Of The Air Force Non-combustible high temperature abradable seal material
US4247249A (en) 1978-09-22 1981-01-27 General Electric Company Turbine engine shroud
US4269903A (en) 1979-09-06 1981-05-26 General Motors Corporation Abradable ceramic seal and method of making same
US4374173A (en) 1979-11-06 1983-02-15 Sherritt Gordon Mines Limited Composite powders sprayable to form abradable seal coatings
DE3018620C2 (de) 1980-05-16 1982-08-26 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Wärmedämmende und dichtende Auskleidung für eine thermische Turbomaschine
US4521496A (en) 1980-07-24 1985-06-04 Sara Raymond V Stress relieved metal/ceramic abradable seals
GB2130244A (en) 1982-03-05 1984-05-31 Rolls Royce Forming coatings by hot isostatic compaction
US4690763A (en) 1982-09-29 1987-09-01 Swiss Aluminium Ltd. Filter medium in the form of a stable porous body
US4704332A (en) 1982-11-01 1987-11-03 United Technologies Corporation Lightweight fiber reinforced high temperature stable glass-ceramic abradable seal
US4639388A (en) 1985-02-12 1987-01-27 Chromalloy American Corporation Ceramic-metal composites
US4867639A (en) 1987-09-22 1989-09-19 Allied-Signal Inc. Abradable shroud coating
US5064727A (en) 1990-01-19 1991-11-12 Avco Corporation Abradable hybrid ceramic wall structures
US5196471A (en) 1990-11-19 1993-03-23 Sulzer Plasma Technik, Inc. Thermal spray powders for abradable coatings, abradable coatings containing solid lubricants and methods of fabricating abradable coatings
WO1993024672A1 (en) 1992-05-29 1993-12-09 United Technologies Corporation Ceramic thermal barrier coating for rapid thermal cycling applications
US5472315A (en) 1993-11-09 1995-12-05 Sundstrand Corporation Abradable coating in a gas turbine engine
GB9513252D0 (en) * 1995-06-29 1995-09-06 Rolls Royce Plc An abradable composition

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KR20010042230A (ko) 2001-05-25
US6197424B1 (en) 2001-03-06
DE69901440T2 (de) 2002-11-21
DE69901440D1 (de) 2002-06-13
JP2002507688A (ja) 2002-03-12
EP1068161B1 (en) 2002-05-08
JP4318858B2 (ja) 2009-08-26
EP1068161A1 (en) 2001-01-17

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