IL96976A - Nozzle band overhang cooling - Google Patents
Nozzle band overhang coolingInfo
- Publication number
- IL96976A IL96976A IL96976A IL9697691A IL96976A IL 96976 A IL96976 A IL 96976A IL 96976 A IL96976 A IL 96976A IL 9697691 A IL9697691 A IL 9697691A IL 96976 A IL96976 A IL 96976A
- Authority
- IL
- Israel
- Prior art keywords
- nozzle band
- band overhang
- cooling
- overhang cooling
- nozzle
- Prior art date
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
- F01D9/00—Stators
- F01D9/06—Fluid supply conduits to nozzles or the like
- F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
-
- 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
- F01D5/187—Convection cooling
-
- 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
- F05D2240/00—Components
- F05D2240/80—Platforms for stationary or moving blades
- F05D2240/81—Cooled platforms
-
- 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
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/221—Improvement of heat transfer
- F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
- F05D2260/22141—Improvement of heat transfer by increasing the heat transfer surface using fins or ribs
-
- 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)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/531,413 US5197852A (en) | 1990-05-31 | 1990-05-31 | Nozzle band overhang cooling |
Publications (2)
Publication Number | Publication Date |
---|---|
IL96976A0 IL96976A0 (en) | 1992-03-29 |
IL96976A true IL96976A (en) | 1993-07-08 |
Family
ID=24117533
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IL96976A IL96976A (en) | 1990-05-31 | 1991-01-21 | Nozzle band overhang cooling |
Country Status (7)
Country | Link |
---|---|
US (1) | US5197852A (ja) |
JP (1) | JPH04231605A (ja) |
CA (1) | CA2039820A1 (ja) |
DE (1) | DE4102033A1 (ja) |
FR (1) | FR2662742A1 (ja) |
GB (1) | GB2244520A (ja) |
IL (1) | IL96976A (ja) |
Families Citing this family (74)
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US5252026A (en) * | 1993-01-12 | 1993-10-12 | General Electric Company | Gas turbine engine nozzle |
US5649806A (en) * | 1993-11-22 | 1997-07-22 | United Technologies Corporation | Enhanced film cooling slot for turbine blade outer air seals |
US5413458A (en) * | 1994-03-29 | 1995-05-09 | United Technologies Corporation | Turbine vane with a platform cavity having a double feed for cooling fluid |
DE69505407T2 (de) * | 1994-08-24 | 1999-05-27 | Westinghouse Electric Corp., Pittsburgh, Pa. | Gasturbinenschaufel mit gekühlter plattform |
EP0791127B1 (en) * | 1994-11-10 | 2000-03-08 | Siemens Westinghouse Power Corporation | Gas turbine vane with a cooled inner shroud |
US5560198A (en) * | 1995-05-25 | 1996-10-01 | United Technologies Corporation | Cooled gas turbine engine augmentor fingerseal assembly |
RU2168558C2 (ru) * | 1995-07-25 | 2001-06-10 | Сименс Акциенгезелльшафт | Изделие с металлическим основным телом и способ его изготовления |
US5931641A (en) * | 1997-04-25 | 1999-08-03 | General Electric Company | Steam turbine blade having areas of different densities |
WO1999060253A1 (de) * | 1998-05-18 | 1999-11-25 | Siemens Aktiengesellschaft | Gekühlte turbinenschaufelplattform |
US6077036A (en) * | 1998-08-20 | 2000-06-20 | General Electric Company | Bowed nozzle vane with selective TBC |
DE19963377A1 (de) * | 1999-12-28 | 2001-07-12 | Abb Alstom Power Ch Ag | Turbinenschaufel mit aktiv gekühltem Deckbandelement |
DE10016081A1 (de) * | 2000-03-31 | 2001-10-04 | Alstom Power Nv | Plattenförmiger, auskragender Bauteilabschnitt einer Gasturbine |
US6402471B1 (en) * | 2000-11-03 | 2002-06-11 | General Electric Company | Turbine blade for gas turbine engine and method of cooling same |
EP1207268B1 (de) * | 2000-11-16 | 2005-02-09 | Siemens Aktiengesellschaft | Filmkühlung von Gasturbinenschaufeln mittels Schlitzen für Kühlluft |
US20030017359A1 (en) * | 2001-07-17 | 2003-01-23 | American Air Liquide, Inc. | Increased stability low concentration gases, products comprising same, and methods of making same |
DE60239339D1 (de) * | 2001-07-17 | 2011-04-14 | Air Liquide | Verfahren zur herstellung einer passivierten oberfläche |
US7832550B2 (en) * | 2001-07-17 | 2010-11-16 | American Air Liquide, Inc. | Reactive gases with concentrations of increased stability and processes for manufacturing same |
FR2833035B1 (fr) * | 2001-12-05 | 2004-08-06 | Snecma Moteurs | Plate-forme d'aube de distributeur pour moteur a turbine a gaz |
WO2003100410A1 (en) | 2002-05-29 | 2003-12-04 | L'air Liquide - Societe Anonyme A Directoire Et Conseil De Surveillance Pour L'etude Et L'exploitation Des Procedes Georges Claude | Reduced moisture compositions comprising an acid gas and a matrix gas, articles of manufacture comprising said compositions and processes for manufacturing same |
US6749396B2 (en) * | 2002-06-17 | 2004-06-15 | General Electric Company | Failsafe film cooled wall |
US7234304B2 (en) * | 2002-10-23 | 2007-06-26 | Pratt & Whitney Canada Corp | Aerodynamic trip to improve acoustic transmission loss and reduce noise level for gas turbine engine |
US7108479B2 (en) * | 2003-06-19 | 2006-09-19 | General Electric Company | Methods and apparatus for supplying cooling fluid to turbine nozzles |
US7029228B2 (en) * | 2003-12-04 | 2006-04-18 | General Electric Company | Method and apparatus for convective cooling of side-walls of turbine nozzle segments |
US7140835B2 (en) * | 2004-10-01 | 2006-11-28 | General Electric Company | Corner cooled turbine nozzle |
US7452184B2 (en) * | 2004-12-13 | 2008-11-18 | Pratt & Whitney Canada Corp. | Airfoil platform impingement cooling |
US7306859B2 (en) * | 2005-01-28 | 2007-12-11 | General Electric Company | Thermal barrier coating system and process therefor |
US7255536B2 (en) * | 2005-05-23 | 2007-08-14 | United Technologies Corporation | Turbine airfoil platform cooling circuit |
US8708658B2 (en) * | 2007-04-12 | 2014-04-29 | United Technologies Corporation | Local application of a protective coating on a shrouded gas turbine engine component |
US7766609B1 (en) | 2007-05-24 | 2010-08-03 | Florida Turbine Technologies, Inc. | Turbine vane endwall with float wall heat shield |
US8376706B2 (en) * | 2007-09-28 | 2013-02-19 | General Electric Company | Turbine airfoil concave cooling passage using dual-swirl flow mechanism and method |
US8296945B2 (en) * | 2007-12-29 | 2012-10-30 | General Electric Company | Method for repairing a turbine nozzle segment |
US20090169361A1 (en) * | 2007-12-29 | 2009-07-02 | Michael Scott Cole | Cooled turbine nozzle segment |
US8235652B2 (en) * | 2007-12-29 | 2012-08-07 | General Electric Company | Turbine nozzle segment |
EP2093381A1 (en) * | 2008-02-25 | 2009-08-26 | Siemens Aktiengesellschaft | Turbine blade or vane with cooled platform |
US8206101B2 (en) * | 2008-06-16 | 2012-06-26 | General Electric Company | Windward cooled turbine nozzle |
EP2211024A1 (en) * | 2009-01-23 | 2010-07-28 | Siemens Aktiengesellschaft | A gas turbine engine |
CH700320A1 (de) * | 2009-01-30 | 2010-07-30 | Alstom Technology Ltd | Verfahren zum herstellen eines bauteils einer gasturbine. |
US20100284800A1 (en) * | 2009-05-11 | 2010-11-11 | General Electric Company | Turbine nozzle with sidewall cooling plenum |
US8490408B2 (en) * | 2009-07-24 | 2013-07-23 | Pratt & Whitney Canada Copr. | Continuous slot in shroud |
GB201016423D0 (en) * | 2010-09-30 | 2010-11-17 | Rolls Royce Plc | Cooled rotor blade |
EP2458148A1 (en) * | 2010-11-25 | 2012-05-30 | Siemens Aktiengesellschaft | Turbo-machine component with a surface for cooling |
US8814518B2 (en) * | 2010-10-29 | 2014-08-26 | General Electric Company | Apparatus and methods for cooling platform regions of turbine rotor blades |
US8915712B2 (en) | 2011-06-20 | 2014-12-23 | General Electric Company | Hot gas path component |
US8376705B1 (en) | 2011-09-09 | 2013-02-19 | Siemens Energy, Inc. | Turbine endwall with grooved recess cavity |
US8845289B2 (en) | 2011-11-04 | 2014-09-30 | General Electric Company | Bucket assembly for turbine system |
US8870525B2 (en) | 2011-11-04 | 2014-10-28 | General Electric Company | Bucket assembly for turbine system |
US8840370B2 (en) | 2011-11-04 | 2014-09-23 | General Electric Company | Bucket assembly for turbine system |
US8864445B2 (en) | 2012-01-09 | 2014-10-21 | General Electric Company | Turbine nozzle assembly methods |
US9011079B2 (en) | 2012-01-09 | 2015-04-21 | General Electric Company | Turbine nozzle compartmentalized cooling system |
US9039350B2 (en) | 2012-01-09 | 2015-05-26 | General Electric Company | Impingement cooling system for use with contoured surfaces |
US8944751B2 (en) | 2012-01-09 | 2015-02-03 | General Electric Company | Turbine nozzle cooling assembly |
US9011078B2 (en) | 2012-01-09 | 2015-04-21 | General Electric Company | Turbine vane seal carrier with slots for cooling and assembly |
US9133724B2 (en) | 2012-01-09 | 2015-09-15 | General Electric Company | Turbomachine component including a cover plate |
US9297261B2 (en) | 2012-03-07 | 2016-03-29 | United Technologies Corporation | Airfoil with improved internal cooling channel pedestals |
US9109452B2 (en) | 2012-06-05 | 2015-08-18 | United Technologies Corporation | Vortex generators for improved film effectiveness |
US9175565B2 (en) | 2012-08-03 | 2015-11-03 | General Electric Company | Systems and apparatus relating to seals for turbine engines |
US20140196433A1 (en) | 2012-10-17 | 2014-07-17 | United Technologies Corporation | Gas turbine engine component platform cooling |
FR3013390B1 (fr) * | 2013-11-19 | 2019-01-25 | Safran Helicopter Engines | Turbomachine et procede de regulation |
US20160312654A1 (en) * | 2013-12-19 | 2016-10-27 | United Technologies Corporation | Turbine airfoil cooling |
US9765699B2 (en) * | 2014-12-30 | 2017-09-19 | General Electric Company | Gas turbine sealing |
EP3043024A1 (en) * | 2015-01-09 | 2016-07-13 | Siemens Aktiengesellschaft | Blade platform cooling and corresponding gas turbine |
DE102015110615A1 (de) * | 2015-07-01 | 2017-01-19 | Rolls-Royce Deutschland Ltd & Co Kg | Leitschaufel eines Gasturbinentriebwerks, insbesondere eines Flugtriebwerks |
US9988916B2 (en) | 2015-07-16 | 2018-06-05 | General Electric Company | Cooling structure for stationary blade |
US20170145834A1 (en) * | 2015-11-23 | 2017-05-25 | United Technologies Corporation | Airfoil platform cooling core circuits with one-wall heat transfer pedestals for a gas turbine engine component and systems for cooling an airfoil platform |
US10221694B2 (en) * | 2016-02-17 | 2019-03-05 | United Technologies Corporation | Gas turbine engine component having vascular engineered lattice structure |
JP6725273B2 (ja) | 2016-03-11 | 2020-07-15 | 三菱日立パワーシステムズ株式会社 | 翼、これを備えているガスタービン |
JP6936295B2 (ja) * | 2016-03-11 | 2021-09-15 | 三菱パワー株式会社 | 翼、ガスタービン、及び翼の製造方法 |
US10260356B2 (en) * | 2016-06-02 | 2019-04-16 | General Electric Company | Nozzle cooling system for a gas turbine engine |
CN105971674B (zh) * | 2016-07-29 | 2018-04-03 | 上海电气燃气轮机有限公司 | 燃气轮机轮缘密封结构及方法 |
KR101873156B1 (ko) * | 2017-04-12 | 2018-06-29 | 두산중공업 주식회사 | 터빈 베인 및 이를 포함하는 가스 터빈 |
US10370983B2 (en) | 2017-07-28 | 2019-08-06 | Rolls-Royce Corporation | Endwall cooling system |
US10577944B2 (en) | 2017-08-03 | 2020-03-03 | General Electric Company | Engine component with hollow turbulators |
US10590778B2 (en) | 2017-08-03 | 2020-03-17 | General Electric Company | Engine component with non-uniform chevron pins |
US20190085706A1 (en) * | 2017-09-18 | 2019-03-21 | General Electric Company | Turbine engine airfoil assembly |
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US2737366A (en) * | 1950-05-02 | 1956-03-06 | Simmering Graz Pauker Ag | Gas turbine |
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US3867065A (en) * | 1973-07-16 | 1975-02-18 | Westinghouse Electric Corp | Ceramic insulator for a gas turbine blade structure |
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US4012167A (en) * | 1975-10-14 | 1977-03-15 | United Technologies Corporation | Turbomachinery vane or blade with cooled platforms |
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GB1553701A (en) * | 1976-05-14 | 1979-09-26 | Rolls Royce | Nozzle guide vane for a gas turbine engine |
US4353679A (en) * | 1976-07-29 | 1982-10-12 | General Electric Company | Fluid-cooled element |
GB1605297A (en) * | 1977-05-05 | 1988-06-08 | Rolls Royce | Nozzle guide vane structure for a gas turbine engine |
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US4177004A (en) * | 1977-10-31 | 1979-12-04 | General Electric Company | Combined turbine shroud and vane support structure |
US4286924A (en) * | 1978-01-14 | 1981-09-01 | Rolls-Royce Limited | Rotor blade or stator vane for a gas turbine engine |
US4187054A (en) * | 1978-04-20 | 1980-02-05 | General Electric Company | Turbine band cooling system |
US4318672A (en) * | 1978-11-06 | 1982-03-09 | Nordisk Ventilator Co. A/S | Particle erosion resistant covering for fan blade leading edge |
GB2037901B (en) * | 1978-11-25 | 1982-07-28 | Rolls Royce | Nozzle guide vane assembly |
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US4712979A (en) * | 1985-11-13 | 1987-12-15 | The United States Of America As Represented By The Secretary Of The Air Force | Self-retained platform cooling plate for turbine vane |
US4798515A (en) * | 1986-05-19 | 1989-01-17 | The United States Of America As Represented By The Secretary Of The Air Force | Variable nozzle area turbine vane cooling |
US4821522A (en) * | 1987-07-02 | 1989-04-18 | United Technologies Corporation | Sealing and cooling arrangement for combustor vane interface |
JP2862536B2 (ja) * | 1987-09-25 | 1999-03-03 | 株式会社東芝 | ガスタービンの翼 |
GB2210935B (en) * | 1987-10-10 | 1992-05-27 | Rolls Royce Plc | Variable stator vane assembly |
JP2753235B2 (ja) * | 1987-10-23 | 1998-05-18 | 財団法人電力中央研究所 | 遮熱緩衝層製造方法 |
US4916022A (en) * | 1988-11-03 | 1990-04-10 | Allied-Signal Inc. | Titania doped ceramic thermal barrier coatings |
US4880614A (en) * | 1988-11-03 | 1989-11-14 | Allied-Signal Inc. | Ceramic thermal barrier coating with alumina interlayer |
-
1990
- 1990-05-31 US US07/531,413 patent/US5197852A/en not_active Expired - Lifetime
-
1991
- 1991-01-21 IL IL96976A patent/IL96976A/xx not_active IP Right Cessation
- 1991-01-23 FR FR9100752A patent/FR2662742A1/fr not_active Withdrawn
- 1991-01-23 JP JP3021343A patent/JPH04231605A/ja active Pending
- 1991-01-24 DE DE4102033A patent/DE4102033A1/de not_active Withdrawn
- 1991-01-25 GB GB9101638A patent/GB2244520A/en not_active Withdrawn
- 1991-04-04 CA CA002039820A patent/CA2039820A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
GB2244520A (en) | 1991-12-04 |
FR2662742A1 (fr) | 1991-12-06 |
DE4102033A1 (de) | 1991-12-05 |
CA2039820A1 (en) | 1991-12-01 |
GB9101638D0 (en) | 1991-03-06 |
IL96976A0 (en) | 1992-03-29 |
JPH04231605A (ja) | 1992-08-20 |
US5197852A (en) | 1993-03-30 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
RH | Patent void |