DE69510295D1 - Keramische statorschaufel mit geringer thermischer spannung - Google Patents
Keramische statorschaufel mit geringer thermischer spannungInfo
- Publication number
- DE69510295D1 DE69510295D1 DE69510295T DE69510295T DE69510295D1 DE 69510295 D1 DE69510295 D1 DE 69510295D1 DE 69510295 T DE69510295 T DE 69510295T DE 69510295 T DE69510295 T DE 69510295T DE 69510295 D1 DE69510295 D1 DE 69510295D1
- Authority
- DE
- Germany
- Prior art keywords
- low thermal
- stator blade
- ceramic stator
- thermal tension
- tension
- 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
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
- F01D5/284—Selection of ceramic materials
-
- 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
- F01D5/186—Film cooling
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/20—Oxide or non-oxide ceramics
- F05D2300/21—Oxide ceramics
-
- 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)
- Ceramic Engineering (AREA)
- Materials Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US08/242,792 US5494402A (en) | 1994-05-16 | 1994-05-16 | Low thermal stress ceramic turbine nozzle |
PCT/US1995/005495 WO1995031631A1 (en) | 1994-05-16 | 1995-05-03 | Low thermal stress ceramic turbine nozzle |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69510295D1 true DE69510295D1 (de) | 1999-07-22 |
DE69510295T2 DE69510295T2 (de) | 2000-01-05 |
Family
ID=22916204
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69510295T Expired - Fee Related DE69510295T2 (de) | 1994-05-16 | 1995-05-03 | Keramische statorschaufel mit geringer thermischer spannung |
Country Status (5)
Country | Link |
---|---|
US (1) | US5494402A (de) |
EP (1) | EP0708876B1 (de) |
JP (1) | JPH09500946A (de) |
DE (1) | DE69510295T2 (de) |
WO (1) | WO1995031631A1 (de) |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2319307B (en) * | 1996-11-12 | 2000-11-08 | Rolls Royce Plc | Gas turbine engine cooling air flow control |
DE19756734A1 (de) * | 1997-12-19 | 1999-06-24 | Bmw Rolls Royce Gmbh | Passives Spalthaltungssystem einer Gasturbine |
JPH11336503A (ja) * | 1998-05-27 | 1999-12-07 | Mitsubishi Heavy Ind Ltd | 蒸気タービン静翼 |
KR100694370B1 (ko) * | 1999-05-14 | 2007-03-12 | 제너럴 일렉트릭 캄파니 | 터빈 노즐의 내측 및 외측 밴드에서 온도 부정합을 제어하는 장치 및 내측 또는 외측 밴드의 벽과 커버 사이의 온도 차이를 감소시키는 방법 |
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 |
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 |
US7008170B2 (en) * | 2004-03-26 | 2006-03-07 | Siemens Westinghouse Power Corporation | Compressor diaphragm with axial preload |
US7435058B2 (en) * | 2005-01-18 | 2008-10-14 | Siemens Power Generation, Inc. | Ceramic matrix composite vane with chordwise stiffener |
US7762766B2 (en) * | 2006-07-06 | 2010-07-27 | Siemens Energy, Inc. | Cantilevered framework support for turbine vane |
US7758307B2 (en) * | 2007-05-17 | 2010-07-20 | Siemens Energy, Inc. | Wear minimization system for a compressor diaphragm |
US8240045B2 (en) * | 2007-05-22 | 2012-08-14 | Siemens Energy, Inc. | Gas turbine transition duct coupling apparatus |
US8616007B2 (en) * | 2009-01-22 | 2013-12-31 | Siemens Energy, Inc. | Structural attachment system for transition duct outlet |
US8256088B2 (en) * | 2009-08-24 | 2012-09-04 | Siemens Energy, Inc. | Joining mechanism with stem tension and interlocked compression ring |
US8684689B2 (en) | 2011-01-14 | 2014-04-01 | Hamilton Sundstrand Corporation | Turbomachine shroud |
US9228450B2 (en) * | 2012-07-03 | 2016-01-05 | Solar Turbines Incorporated | Nozzle particle deflector for a gas turbine engine |
US20140248127A1 (en) * | 2012-12-29 | 2014-09-04 | United Technologies Corporation | Turbine engine component with dual purpose rib |
US10760491B2 (en) * | 2013-02-28 | 2020-09-01 | Raytheon Technologies Corporation | Method and apparatus for handling pre-diffuser airflow for use in adjusting a temperature profile |
US10451084B2 (en) * | 2015-11-16 | 2019-10-22 | General Electric Company | Gas turbine engine with vane having a cooling inlet |
PL419827A1 (pl) * | 2016-12-16 | 2018-06-18 | General Electric Company | Rozpórki do ram wylotowych systemów turbin |
FR3065485B1 (fr) * | 2017-04-25 | 2019-07-05 | Safran Aircraft Engines | Etage de turbine de turbomachine |
US10920609B2 (en) | 2017-04-25 | 2021-02-16 | Safran Aircraft Engines | Turbine engine turbine assembly |
FR3065484B1 (fr) * | 2017-04-25 | 2019-07-05 | Safran Aircraft Engines | Ensemble de turbine de turbomachine |
CN107023317A (zh) * | 2017-05-25 | 2017-08-08 | 华能国际电力股份有限公司 | 一种再热式多级轴流透平及其工作方法 |
US12091982B2 (en) * | 2022-06-10 | 2024-09-17 | Ge Infrastructure Technology Llc | Turbine component with heated structure to reduce thermal stress |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2563269A (en) * | 1943-05-22 | 1951-08-07 | Lockheed Aircraft Corp | Gas turbine |
BE487115A (de) * | 1946-04-05 | |||
US2501614A (en) * | 1947-11-28 | 1950-03-21 | Lockheed Aircraft Corp | Compressor construction |
GB753224A (en) * | 1953-04-13 | 1956-07-18 | Rolls Royce | Improvements in or relating to blading for turbines or compressors |
US3291447A (en) * | 1965-02-15 | 1966-12-13 | Gen Electric | Steam turbine rotor cooling |
US3619077A (en) * | 1966-09-30 | 1971-11-09 | Gen Electric | High-temperature airfoil |
DE1938132A1 (de) * | 1969-07-26 | 1971-01-28 | Daimler Benz Ag | Leitschaufeln von Axialverdichtern |
US4245954A (en) * | 1978-12-01 | 1981-01-20 | Westinghouse Electric Corp. | Ceramic turbine stator vane and shroud support |
US4643636A (en) * | 1985-07-22 | 1987-02-17 | Avco Corporation | Ceramic nozzle assembly for gas turbine engine |
US4768924A (en) * | 1986-07-22 | 1988-09-06 | Pratt & Whitney Canada Inc. | Ceramic stator vane assembly |
SU1507991A1 (ru) * | 1988-01-13 | 1989-09-15 | Комсомольский-на-Амуре политехнический институт | Лопатка влажнопаровой ступени турбины |
DE4017861A1 (de) * | 1990-06-02 | 1991-12-05 | Mtu Muenchen Gmbh | Leitkranz fuer eine gasturbine |
US5090866A (en) * | 1990-08-27 | 1992-02-25 | United Technologies Corporation | High temperature leading edge vane insert |
US5098257A (en) * | 1990-09-10 | 1992-03-24 | Westinghouse Electric Corp. | Apparatus and method for minimizing differential thermal expansion of gas turbine vane structures |
US5142859A (en) * | 1991-02-22 | 1992-09-01 | Solar Turbines, Incorporated | Turbine cooling system |
FR2689176B1 (fr) * | 1992-03-25 | 1995-07-13 | Snecma | Aube refrigeree de turbo-machine. |
US5207556A (en) * | 1992-04-27 | 1993-05-04 | General Electric Company | Airfoil having multi-passage baffle |
US5380154A (en) * | 1994-03-18 | 1995-01-10 | Solar Turbines Incorporated | Turbine nozzle positioning system |
-
1994
- 1994-05-16 US US08/242,792 patent/US5494402A/en not_active Expired - Fee Related
-
1995
- 1995-05-03 DE DE69510295T patent/DE69510295T2/de not_active Expired - Fee Related
- 1995-05-03 EP EP95918932A patent/EP0708876B1/de not_active Expired - Lifetime
- 1995-05-03 WO PCT/US1995/005495 patent/WO1995031631A1/en active IP Right Grant
- 1995-05-03 JP JP7529688A patent/JPH09500946A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
WO1995031631A1 (en) | 1995-11-23 |
EP0708876A1 (de) | 1996-05-01 |
EP0708876B1 (de) | 1999-06-16 |
DE69510295T2 (de) | 2000-01-05 |
JPH09500946A (ja) | 1997-01-28 |
US5494402A (en) | 1996-02-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |