CN100335752C - 陶瓷涡轮罩 - Google Patents
陶瓷涡轮罩 Download PDFInfo
- Publication number
- CN100335752C CN100335752C CNB031312942A CN03131294A CN100335752C CN 100335752 C CN100335752 C CN 100335752C CN B031312942 A CNB031312942 A CN B031312942A CN 03131294 A CN03131294 A CN 03131294A CN 100335752 C CN100335752 C CN 100335752C
- Authority
- CN
- China
- Prior art keywords
- gas turbine
- ceramic
- pin
- inner cover
- hook spare
- 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
Links
- 239000000919 ceramic Substances 0.000 title claims abstract description 34
- 238000013016 damping Methods 0.000 claims abstract description 10
- 229910052751 metal Inorganic materials 0.000 claims description 26
- 239000002184 metal Substances 0.000 claims description 26
- 239000012720 thermal barrier coating Substances 0.000 claims description 9
- 239000000835 fiber Substances 0.000 claims description 4
- 230000000712 assembly Effects 0.000 claims description 3
- 238000000429 assembly Methods 0.000 claims description 3
- 229910010293 ceramic material Inorganic materials 0.000 claims 1
- 239000007789 gas Substances 0.000 description 12
- 238000001816 cooling Methods 0.000 description 6
- 238000007789 sealing Methods 0.000 description 6
- 239000000567 combustion gas Substances 0.000 description 5
- 238000012856 packing Methods 0.000 description 3
- 239000011248 coating agent Substances 0.000 description 2
- 238000000576 coating method Methods 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 238000010304 firing Methods 0.000 description 2
- 241000628997 Flos Species 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 229910021645 metal ion Inorganic materials 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000003672 processing method Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
Images
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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
-
- 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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/12—Preventing 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
-
- 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
-
- 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
- F05D2260/00—Function
- F05D2260/30—Retaining components in desired mutual position
-
- 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
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)
- Gasket Seals (AREA)
- Inorganic Insulating Materials (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/144851 | 2002-05-15 | ||
| US10/144,851 US6726448B2 (en) | 2002-05-15 | 2002-05-15 | Ceramic turbine shroud |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1458393A CN1458393A (zh) | 2003-11-26 |
| CN100335752C true CN100335752C (zh) | 2007-09-05 |
Family
ID=29269733
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNB031312942A Expired - Fee Related CN100335752C (zh) | 2002-05-15 | 2003-05-13 | 陶瓷涡轮罩 |
Country Status (10)
| Country | Link |
|---|---|
| US (1) | US6726448B2 (enExample) |
| EP (1) | EP1362983B1 (enExample) |
| JP (1) | JP4308574B2 (enExample) |
| KR (1) | KR100776072B1 (enExample) |
| CN (1) | CN100335752C (enExample) |
| AT (1) | ATE437294T1 (enExample) |
| CZ (1) | CZ302320B6 (enExample) |
| DE (1) | DE60328432D1 (enExample) |
| ES (1) | ES2327726T3 (enExample) |
| RU (1) | RU2312224C2 (enExample) |
Families Citing this family (92)
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|---|---|---|---|---|
| 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 |
| US20050067788A1 (en) * | 2003-09-25 | 2005-03-31 | Siemens Westinghouse Power Corporation | Outer air seal assembly |
| US6942203B2 (en) * | 2003-11-04 | 2005-09-13 | General Electric Company | Spring mass damper system for turbine shrouds |
| US7090459B2 (en) * | 2004-03-31 | 2006-08-15 | General Electric Company | Hybrid seal and system and method incorporating the same |
| US7195452B2 (en) * | 2004-09-27 | 2007-03-27 | Honeywell International, Inc. | Compliant mounting system for turbine shrouds |
| US7329101B2 (en) * | 2004-12-29 | 2008-02-12 | General Electric Company | Ceramic composite with integrated compliance/wear layer |
| DE102005013796A1 (de) | 2005-03-24 | 2006-09-28 | Alstom Technology Ltd. | Wärmestausegment |
| DE102005013797A1 (de) * | 2005-03-24 | 2006-09-28 | Alstom Technology Ltd. | Wärmestausegment |
| DE502005010381D1 (de) * | 2005-04-28 | 2010-11-25 | Siemens Ag | Verfahren und Vorrichtung zur Einstellung eines Radialspaltes eines axial durchströmten Verdichters einer Strömungsmaschine |
| US7338253B2 (en) * | 2005-09-15 | 2008-03-04 | General Electric Company | Resilient seal on trailing edge of turbine inner shroud and method for shroud post impingement cavity sealing |
| US7278820B2 (en) * | 2005-10-04 | 2007-10-09 | Siemens Power Generation, Inc. | Ring seal system with reduced cooling requirements |
| FR2906295B1 (fr) * | 2006-09-22 | 2011-11-18 | Snecma | Dispositif de toles isolantes sur carter pour amelioration du jeu en sommet d'aube |
| EP2118082B1 (en) | 2007-02-23 | 2014-10-01 | Gilead Sciences, Inc. | Modulators of pharmacokinetic properties of therapeutics |
| US8528339B2 (en) | 2007-04-05 | 2013-09-10 | Siemens Energy, Inc. | Stacked laminate gas turbine component |
| US7758307B2 (en) * | 2007-05-17 | 2010-07-20 | Siemens Energy, Inc. | Wear minimization system for a compressor diaphragm |
| US7766609B1 (en) | 2007-05-24 | 2010-08-03 | Florida Turbine Technologies, Inc. | Turbine vane endwall with float wall heat shield |
| US7811054B2 (en) * | 2007-05-30 | 2010-10-12 | General Electric Company | Shroud configuration having sloped seal |
| US20090053045A1 (en) * | 2007-08-22 | 2009-02-26 | General Electric Company | Turbine Shroud for Gas Turbine Assemblies and Processes for Forming the Shroud |
| US8534995B2 (en) * | 2009-03-05 | 2013-09-17 | United Technologies Corporation | Turbine engine sealing arrangement |
| US8393858B2 (en) * | 2009-03-13 | 2013-03-12 | Honeywell International Inc. | Turbine shroud support coupling assembly |
| JP5384983B2 (ja) * | 2009-03-27 | 2014-01-08 | 本田技研工業株式会社 | タービンシュラウド |
| US20110243725A1 (en) * | 2010-03-31 | 2011-10-06 | General Electric Company | Turbine shroud mounting apparatus with anti-rotation feature |
| US8740552B2 (en) * | 2010-05-28 | 2014-06-03 | General Electric Company | Low-ductility turbine shroud and mounting apparatus |
| US8926270B2 (en) | 2010-12-17 | 2015-01-06 | General Electric Company | Low-ductility turbine shroud flowpath and mounting arrangement therefor |
| US8845272B2 (en) | 2011-02-25 | 2014-09-30 | General Electric Company | Turbine shroud and a method for manufacturing the turbine shroud |
| US9062558B2 (en) * | 2011-07-15 | 2015-06-23 | United Technologies Corporation | Blade outer air seal having partial coating |
| US9995165B2 (en) | 2011-07-15 | 2018-06-12 | United Technologies Corporation | Blade outer air seal having partial coating |
| US20130034436A1 (en) * | 2011-08-02 | 2013-02-07 | General Electric Company | Systems, Method, and Apparatus for Modifying a Turbine Casing |
| US9726043B2 (en) | 2011-12-15 | 2017-08-08 | General Electric Company | Mounting apparatus for low-ductility turbine shroud |
| EP2831306B1 (en) | 2012-03-28 | 2017-06-28 | Ansaldo Energia IP UK Limited | Method for separating a metal part from a ceramic part |
| EP2830805B1 (en) * | 2012-03-28 | 2019-07-31 | Ansaldo Energia IP UK Limited | Method for processing a modular hybrid component |
| US9316109B2 (en) * | 2012-04-10 | 2016-04-19 | General Electric Company | Turbine shroud assembly and method of forming |
| US9181877B2 (en) * | 2012-09-27 | 2015-11-10 | United Technologies Corporation | Seal hook mount structure with overlapped coating |
| CA2896500A1 (en) | 2013-01-29 | 2014-08-07 | Rolls-Royce Corporation | Turbine shroud |
| US9833869B2 (en) * | 2013-02-11 | 2017-12-05 | United Technologies Corporation | Blade outer air seal surface |
| CA2900687C (en) | 2013-03-05 | 2019-06-18 | Rolls-Royce Corporation | Structure and method for providing compliance and sealing between ceramic and metallic structures |
| WO2014143230A1 (en) | 2013-03-13 | 2014-09-18 | Landwehr Sean E | Turbine shroud |
| WO2014186099A1 (en) | 2013-05-17 | 2014-11-20 | General Electric Company | Cmc shroud support system of a gas turbine |
| CN105814282B (zh) | 2013-12-12 | 2018-06-05 | 通用电气公司 | Cmc护罩支撑系统 |
| CN105899764B (zh) * | 2014-01-17 | 2021-05-25 | 通用电气公司 | 用于cmc护罩的cmc悬挂器套筒 |
| US9416675B2 (en) | 2014-01-27 | 2016-08-16 | General Electric Company | Sealing device for providing a seal in a turbomachine |
| CN106460543B (zh) | 2014-06-12 | 2018-12-21 | 通用电气公司 | 多件式护罩悬挂器组件 |
| US11668207B2 (en) | 2014-06-12 | 2023-06-06 | General Electric Company | Shroud hanger assembly |
| CA2951638A1 (en) | 2014-06-12 | 2015-12-17 | General Electric Company | Shroud hanger assembly |
| US9945243B2 (en) | 2014-10-14 | 2018-04-17 | Rolls-Royce Corporation | Turbine shroud with biased blade track |
| US10190434B2 (en) | 2014-10-29 | 2019-01-29 | Rolls-Royce North American Technologies Inc. | Turbine shroud with locating inserts |
| US10099290B2 (en) | 2014-12-18 | 2018-10-16 | General Electric Company | Hybrid additive manufacturing methods using hybrid additively manufactured features for hybrid components |
| CA2915370A1 (en) | 2014-12-23 | 2016-06-23 | Rolls-Royce Corporation | Full hoop blade track with axially keyed features |
| CA2915246A1 (en) | 2014-12-23 | 2016-06-23 | Rolls-Royce Corporation | Turbine shroud |
| EP3045674B1 (en) | 2015-01-15 | 2018-11-21 | Rolls-Royce Corporation | Turbine shroud with tubular runner-locating inserts |
| CA2916710A1 (en) | 2015-01-29 | 2016-07-29 | Rolls-Royce Corporation | Seals for gas turbine engines |
| US9874104B2 (en) | 2015-02-27 | 2018-01-23 | General Electric Company | Method and system for a ceramic matrix composite shroud hanger assembly |
| US10422244B2 (en) | 2015-03-16 | 2019-09-24 | General Electric Company | System for cooling a turbine shroud |
| US10100649B2 (en) | 2015-03-31 | 2018-10-16 | Rolls-Royce North American Technologies Inc. | Compliant rail hanger |
| CA2924855A1 (en) | 2015-04-29 | 2016-10-29 | Rolls-Royce Corporation | Keystoned blade track |
| CA2925588A1 (en) | 2015-04-29 | 2016-10-29 | Rolls-Royce Corporation | Brazed blade track for a gas turbine engine |
| US9932901B2 (en) | 2015-05-11 | 2018-04-03 | General Electric Company | Shroud retention system with retention springs |
| US9945242B2 (en) | 2015-05-11 | 2018-04-17 | General Electric Company | System for thermally isolating a turbine shroud |
| US9828879B2 (en) | 2015-05-11 | 2017-11-28 | General Electric Company | Shroud retention system with keyed retention clips |
| US10132186B2 (en) | 2015-08-13 | 2018-11-20 | General Electric Company | System and method for supporting a turbine shroud |
| US9945257B2 (en) * | 2015-09-18 | 2018-04-17 | General Electric Company | Ceramic matrix composite ring shroud retention methods-CMC pin-head |
| US10443417B2 (en) | 2015-09-18 | 2019-10-15 | General Electric Company | Ceramic matrix composite ring shroud retention methods-finger seals with stepped shroud interface |
| US10094244B2 (en) | 2015-09-18 | 2018-10-09 | General Electric Company | Ceramic matrix composite ring shroud retention methods-wiggle strip spring seal |
| US10240476B2 (en) | 2016-01-19 | 2019-03-26 | Rolls-Royce North American Technologies Inc. | Full hoop blade track with interstage cooling air |
| US10422240B2 (en) | 2016-03-16 | 2019-09-24 | United Technologies Corporation | Turbine engine blade outer air seal with load-transmitting cover plate |
| US10107129B2 (en) | 2016-03-16 | 2018-10-23 | United Technologies Corporation | Blade outer air seal with spring centering |
| US10161258B2 (en) | 2016-03-16 | 2018-12-25 | United Technologies Corporation | Boas rail shield |
| US10563531B2 (en) | 2016-03-16 | 2020-02-18 | United Technologies Corporation | Seal assembly for gas turbine engine |
| US10138749B2 (en) | 2016-03-16 | 2018-11-27 | United Technologies Corporation | Seal anti-rotation feature |
| US10138750B2 (en) * | 2016-03-16 | 2018-11-27 | United Technologies Corporation | Boas segmented heat shield |
| US10443616B2 (en) | 2016-03-16 | 2019-10-15 | United Technologies Corporation | Blade outer air seal with centrally mounted seal arc segments |
| US10513943B2 (en) | 2016-03-16 | 2019-12-24 | United Technologies Corporation | Boas enhanced heat transfer surface |
| US10415414B2 (en) | 2016-03-16 | 2019-09-17 | United Technologies Corporation | Seal arc segment with anti-rotation feature |
| US10337346B2 (en) | 2016-03-16 | 2019-07-02 | United Technologies Corporation | Blade outer air seal with flow guide manifold |
| US10422241B2 (en) | 2016-03-16 | 2019-09-24 | United Technologies Corporation | Blade outer air seal support for a gas turbine engine |
| US10132184B2 (en) | 2016-03-16 | 2018-11-20 | United Technologies Corporation | Boas spring loaded rail shield |
| US10443424B2 (en) | 2016-03-16 | 2019-10-15 | United Technologies Corporation | Turbine engine blade outer air seal with load-transmitting carriage |
| US10415415B2 (en) | 2016-07-22 | 2019-09-17 | Rolls-Royce North American Technologies Inc. | Turbine shroud with forward case and full hoop blade track |
| US10287906B2 (en) | 2016-05-24 | 2019-05-14 | Rolls-Royce North American Technologies Inc. | Turbine shroud with full hoop ceramic matrix composite blade track and seal system |
| US10378772B2 (en) | 2017-01-19 | 2019-08-13 | General Electric Company | Combustor heat shield sealing |
| US10648362B2 (en) | 2017-02-24 | 2020-05-12 | General Electric Company | Spline for a turbine engine |
| US10655495B2 (en) | 2017-02-24 | 2020-05-19 | General Electric Company | Spline for a turbine engine |
| US10544701B2 (en) | 2017-06-15 | 2020-01-28 | General Electric Company | Turbine shroud assembly |
| US10669895B2 (en) * | 2017-06-15 | 2020-06-02 | General Electric Company | Shroud dampening pin and turbine shroud assembly |
| US10526921B2 (en) | 2017-06-15 | 2020-01-07 | General Electric Company | Anti-rotation shroud dampening pin and turbine shroud assembly |
| US10280801B2 (en) * | 2017-06-15 | 2019-05-07 | General Electric Company | Turbine component and turbine shroud assembly |
| US10392957B2 (en) | 2017-10-05 | 2019-08-27 | Rolls-Royce Corporation | Ceramic matrix composite blade track with mounting system having load distribution features |
| US10982559B2 (en) * | 2018-08-24 | 2021-04-20 | General Electric Company | Spline seal with cooling features for turbine engines |
| US11125096B2 (en) * | 2019-05-03 | 2021-09-21 | Raytheon Technologies Corporation | CMC boas arrangement |
| US11149563B2 (en) * | 2019-10-04 | 2021-10-19 | Rolls-Royce Corporation | Ceramic matrix composite blade track with mounting system having axial reaction load distribution features |
| US12055058B2 (en) * | 2022-05-31 | 2024-08-06 | Pratt & Whitney Canada Corp. | Joint between gas turbine engine components with a spring element |
| US20250198306A1 (en) * | 2023-12-14 | 2025-06-19 | Rtx Corporation | Split case with coatable transistion feature |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3966356A (en) * | 1975-09-22 | 1976-06-29 | General Motors Corporation | Blade tip seal mount |
| US4087199A (en) * | 1976-11-22 | 1978-05-02 | General Electric Company | Ceramic turbine shroud assembly |
| US4245954A (en) * | 1978-12-01 | 1981-01-20 | Westinghouse Electric Corp. | Ceramic turbine stator vane and shroud support |
| US5645399A (en) * | 1995-03-15 | 1997-07-08 | United Technologies Corporation | Gas turbine engine case coated with thermal barrier coating to control axial airfoil clearance |
| CN1219215A (zh) * | 1996-05-20 | 1999-06-09 | 普瑞特和惠特尼加拿大公司 | 燃气轮机的罩盖密封组件 |
| US6113349A (en) * | 1998-09-28 | 2000-09-05 | General Electric Company | Turbine assembly containing an inner shroud |
| US6200091B1 (en) * | 1998-06-25 | 2001-03-13 | Societe Nationale d'Etude et de Construction de Moteurs d'Aviation “SNECMA” | High-pressure turbine stator ring for a turbine engine |
| US6315519B1 (en) * | 1998-09-28 | 2001-11-13 | General Electric Company | Turbine inner shroud and turbine assembly containing such inner shroud |
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|---|---|---|---|---|
| US4551064A (en) * | 1982-03-05 | 1985-11-05 | Rolls-Royce Limited | Turbine shroud and turbine shroud assembly |
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| GB8921003D0 (en) | 1989-09-15 | 1989-11-01 | Rolls Royce Plc | Improvements in or relating to shroud rings |
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-
2002
- 2002-05-15 US US10/144,851 patent/US6726448B2/en not_active Expired - Lifetime
-
2003
- 2003-03-27 CZ CZ20030887A patent/CZ302320B6/cs not_active IP Right Cessation
- 2003-05-13 CN CNB031312942A patent/CN100335752C/zh not_active Expired - Fee Related
- 2003-05-14 KR KR1020030030467A patent/KR100776072B1/ko not_active Expired - Fee Related
- 2003-05-14 JP JP2003135222A patent/JP4308574B2/ja not_active Expired - Fee Related
- 2003-05-14 RU RU2003114120/06A patent/RU2312224C2/ru not_active IP Right Cessation
- 2003-05-15 EP EP03253022A patent/EP1362983B1/en not_active Expired - Lifetime
- 2003-05-15 AT AT03253022T patent/ATE437294T1/de not_active IP Right Cessation
- 2003-05-15 DE DE60328432T patent/DE60328432D1/de not_active Expired - Lifetime
- 2003-05-15 ES ES03253022T patent/ES2327726T3/es not_active Expired - Lifetime
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3966356A (en) * | 1975-09-22 | 1976-06-29 | General Motors Corporation | Blade tip seal mount |
| US4087199A (en) * | 1976-11-22 | 1978-05-02 | General Electric Company | Ceramic turbine shroud assembly |
| US4245954A (en) * | 1978-12-01 | 1981-01-20 | Westinghouse Electric Corp. | Ceramic turbine stator vane and shroud support |
| US5645399A (en) * | 1995-03-15 | 1997-07-08 | United Technologies Corporation | Gas turbine engine case coated with thermal barrier coating to control axial airfoil clearance |
| CN1219215A (zh) * | 1996-05-20 | 1999-06-09 | 普瑞特和惠特尼加拿大公司 | 燃气轮机的罩盖密封组件 |
| US6200091B1 (en) * | 1998-06-25 | 2001-03-13 | Societe Nationale d'Etude et de Construction de Moteurs d'Aviation “SNECMA” | High-pressure turbine stator ring for a turbine engine |
| US6113349A (en) * | 1998-09-28 | 2000-09-05 | General Electric Company | Turbine assembly containing an inner shroud |
| US6315519B1 (en) * | 1998-09-28 | 2001-11-13 | General Electric Company | Turbine inner shroud and turbine assembly containing such inner shroud |
Also Published As
| Publication number | Publication date |
|---|---|
| JP2004003477A (ja) | 2004-01-08 |
| RU2312224C2 (ru) | 2007-12-10 |
| KR100776072B1 (ko) | 2007-11-15 |
| EP1362983A3 (en) | 2007-12-05 |
| ES2327726T3 (es) | 2009-11-03 |
| DE60328432D1 (de) | 2009-09-03 |
| CZ2003887A3 (cs) | 2003-12-17 |
| EP1362983B1 (en) | 2009-07-22 |
| CZ302320B6 (cs) | 2011-03-09 |
| US20030215328A1 (en) | 2003-11-20 |
| JP4308574B2 (ja) | 2009-08-05 |
| ATE437294T1 (de) | 2009-08-15 |
| US6726448B2 (en) | 2004-04-27 |
| EP1362983A2 (en) | 2003-11-19 |
| CN1458393A (zh) | 2003-11-26 |
| KR20030088878A (ko) | 2003-11-20 |
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