DE69423180D1 - Geometrie einer Turbomaschinenschaufel - Google Patents
Geometrie einer TurbomaschinenschaufelInfo
- Publication number
- DE69423180D1 DE69423180D1 DE69423180T DE69423180T DE69423180D1 DE 69423180 D1 DE69423180 D1 DE 69423180D1 DE 69423180 T DE69423180 T DE 69423180T DE 69423180 T DE69423180 T DE 69423180T DE 69423180 D1 DE69423180 D1 DE 69423180D1
- Authority
- DE
- Germany
- Prior art keywords
- geometry
- turbomachine blade
- turbomachine
- blade
- 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
- F01D5/14—Form or construction
- F01D5/141—Shape, i.e. outer, aerodynamic form
-
- 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
- F05D2250/00—Geometry
- F05D2250/70—Shape
- F05D2250/71—Shape curved
- F05D2250/713—Shape curved inflexed
-
- 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 |
---|---|---|---|
US08/157,714 US5352092A (en) | 1993-11-24 | 1993-11-24 | Light weight steam turbine blade |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69423180D1 true DE69423180D1 (de) | 2000-04-06 |
DE69423180T2 DE69423180T2 (de) | 2000-08-17 |
Family
ID=22564959
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69423180T Expired - Fee Related DE69423180T2 (de) | 1993-11-24 | 1994-11-23 | Geometrie einer Turbomaschinenschaufel |
Country Status (3)
Country | Link |
---|---|
US (2) | US5352092A (de) |
EP (1) | EP0654585B1 (de) |
DE (1) | DE69423180T2 (de) |
Families Citing this family (60)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB9417406D0 (en) * | 1994-08-30 | 1994-10-19 | Gec Alsthom Ltd | Turbine blade |
US5524341A (en) * | 1994-09-26 | 1996-06-11 | Westinghouse Electric Corporation | Method of making a row of mix-tuned turbomachine blades |
US5624234A (en) * | 1994-11-18 | 1997-04-29 | Itt Automotive Electrical Systems, Inc. | Fan blade with curved planform and high-lift airfoil having bulbous leading edge |
US5588804A (en) * | 1994-11-18 | 1996-12-31 | Itt Automotive Electrical Systems, Inc. | High-lift airfoil with bulbous leading edge |
WO1998019048A1 (en) * | 1996-10-28 | 1998-05-07 | Siemens Westinghouse Power Corporation | Airfoil for a turbomachine |
US5980209A (en) * | 1997-06-27 | 1999-11-09 | General Electric Co. | Turbine blade with enhanced cooling and profile optimization |
US6393617B1 (en) | 1998-01-16 | 2002-05-28 | Depuy Orthopaedics, Inc. | Head gear apparatus |
DE59907976D1 (de) * | 1998-02-20 | 2004-01-22 | Rolls Royce Deutschland | Anordnung von Axialturbinenschaufeln |
US6260794B1 (en) * | 1999-05-05 | 2001-07-17 | General Electric Company | Dolphin cascade vane |
GB0003676D0 (en) * | 2000-02-17 | 2000-04-05 | Abb Alstom Power Nv | Aerofoils |
DE10027084C2 (de) * | 2000-05-31 | 2002-07-18 | Honda Motor Co Ltd | Leitschaufel und Leitschaufelkaskade für einen Axialverdichter |
US6461110B1 (en) | 2001-07-11 | 2002-10-08 | General Electric Company | First-stage high pressure turbine bucket airfoil |
DE10054244C2 (de) * | 2000-11-02 | 2002-10-10 | Honda Motor Co Ltd | Turbinenblattanordnung und Turbinenblatt für eine Axialturbine |
JP2002213206A (ja) * | 2001-01-12 | 2002-07-31 | Mitsubishi Heavy Ind Ltd | ガスタービンにおける翼構造 |
US6457938B1 (en) | 2001-03-30 | 2002-10-01 | General Electric Company | Wide angle guide vane |
US6979178B2 (en) * | 2001-06-18 | 2005-12-27 | Bharat Heavy Electricals Ltd. | Cylindrical blades for axial steam turbines |
US6503054B1 (en) * | 2001-07-13 | 2003-01-07 | General Electric Company | Second-stage turbine nozzle airfoil |
US6461109B1 (en) * | 2001-07-13 | 2002-10-08 | General Electric Company | Third-stage turbine nozzle airfoil |
WO2003006797A1 (en) * | 2001-07-13 | 2003-01-23 | General Electric Company | Second-stage turbine nozzle airfoil |
JP4373629B2 (ja) * | 2001-08-31 | 2009-11-25 | 株式会社東芝 | 軸流タービン |
US6682301B2 (en) * | 2001-10-05 | 2004-01-27 | General Electric Company | Reduced shock transonic airfoil |
GB2384276A (en) * | 2002-01-18 | 2003-07-23 | Alstom | Gas turbine low pressure stage |
FR2845427B1 (fr) * | 2002-10-02 | 2005-05-06 | Alstom Switzerland Ltd | Roue de type francis et turbine hydraulique equipee d'une telle roue |
US6990691B2 (en) | 2003-07-18 | 2006-01-31 | Depuy Products, Inc. | Head gear apparatus |
GB2407136B (en) | 2003-10-15 | 2007-10-03 | Alstom | Turbine rotor blade for gas turbine engine |
US6957948B2 (en) * | 2004-01-21 | 2005-10-25 | Power Systems Mfg., Llc | Turbine blade attachment lightening holes |
US7930073B2 (en) * | 2004-06-23 | 2011-04-19 | Syracuse University | Method and system for controlling airfoil actuators |
DE102006026968A1 (de) * | 2006-06-09 | 2008-01-24 | Rolls-Royce Deutschland Ltd & Co Kg | Strömungsarbeitsmaschine mit Rotoren hoher spezifischer Energieabgabe |
JP4659008B2 (ja) * | 2007-09-13 | 2011-03-30 | ルネサスエレクトロニクス株式会社 | ホスト負荷調整機能付周辺回路 |
DE102008031781B4 (de) * | 2008-07-04 | 2020-06-10 | Man Energy Solutions Se | Schaufelgitter für eine Strömungsmaschine und Strömungsmaschine mit einem solchen Schaufelgitter |
US20130224034A1 (en) * | 2009-07-09 | 2013-08-29 | Mitsubishi Heavy Industries, Ltd. | Blade body and rotary machine |
US20110070072A1 (en) * | 2009-09-23 | 2011-03-24 | General Electric Company | Rotary machine tip clearance control mechanism |
US9593665B2 (en) | 2009-10-02 | 2017-03-14 | Jose Ramon Santana | Hydro-kinetic transport wheel |
US20110080002A1 (en) * | 2009-10-02 | 2011-04-07 | Jose Ramon Santana | Controlled momentum hydro-electric system |
US8360731B2 (en) * | 2009-12-04 | 2013-01-29 | United Technologies Corporation | Tip vortex control |
US8523531B2 (en) * | 2009-12-23 | 2013-09-03 | Alstom Technology Ltd | Airfoil for a compressor blade |
US9291059B2 (en) | 2009-12-23 | 2016-03-22 | Alstom Technology Ltd. | Airfoil for a compressor blade |
US10294795B2 (en) * | 2010-04-28 | 2019-05-21 | United Technologies Corporation | High pitch-to-chord turbine airfoils |
US20120070297A1 (en) * | 2010-09-21 | 2012-03-22 | Estes Matthew B | Aft loaded airfoil |
ES2796526T3 (es) * | 2010-11-30 | 2020-11-27 | Mtu Aero Engines Gmbh | Sistema de paletas para un motor de avión |
US8864457B2 (en) * | 2011-10-06 | 2014-10-21 | Siemens Energy, Inc. | Gas turbine with optimized airfoil element angles |
GB201119531D0 (en) * | 2011-11-14 | 2011-12-21 | Rolls Royce Plc | Aerofoils |
US9957801B2 (en) | 2012-08-03 | 2018-05-01 | United Technologies Corporation | Airfoil design having localized suction side curvatures |
US10626730B2 (en) * | 2013-12-17 | 2020-04-21 | United Technologies Corporation | Enhanced cooling for blade tip |
JP6396093B2 (ja) * | 2014-06-26 | 2018-09-26 | 三菱重工業株式会社 | タービン動翼列、タービン段落及び軸流タービン |
US10221708B2 (en) * | 2014-12-03 | 2019-03-05 | United Technologies Corporation | Tangential on-board injection vanes |
US20160160874A1 (en) * | 2014-12-04 | 2016-06-09 | Solar Turbines Incorporated | Airfoil for inlet guide vane (igv) of multistage compressor |
DE112016000685B4 (de) * | 2015-02-10 | 2023-10-05 | Mitsubishi Heavy Industries, Ltd. | Turbine und gasturbine |
WO2020028010A1 (en) * | 2018-08-02 | 2020-02-06 | Horton, Inc. | Low solidity vehicle cooling fan |
GB201818686D0 (en) * | 2018-11-16 | 2019-01-02 | Rolls Royce Plc | Boundary layer ingestion fan system |
GB201818687D0 (en) * | 2018-11-16 | 2019-01-02 | Rolls Royce Plc | Boundary layer ingestion fan system |
GB201818681D0 (en) * | 2018-11-16 | 2019-01-02 | Rolls Royce Plc | Boundary layer ingestion fan system |
GB201818680D0 (en) * | 2018-11-16 | 2019-01-02 | Rolls Royce Plc | Boundary layer ingestion fan system |
GB201818682D0 (en) * | 2018-11-16 | 2019-01-02 | Rolls Royce Plc | Boundary layer ingestion fan system |
GB201818684D0 (en) * | 2018-11-16 | 2019-01-02 | Rolls Royce Plc | Boundary layer ingestion fan system |
JP7232034B2 (ja) | 2018-12-18 | 2023-03-02 | 三菱重工業株式会社 | タービン翼及びこれを備えた蒸気タービン |
US20210062657A1 (en) * | 2019-08-30 | 2021-03-04 | General Electric Company | Control stage blades for turbines |
IT202000005146A1 (it) * | 2020-03-11 | 2021-09-11 | Ge Avio Srl | Motore a turbina con profilo aerodinamico avente alta accelerazione e bassa curva di paletta |
US11236628B1 (en) * | 2020-12-16 | 2022-02-01 | General Electric Company | Turbine nozzle airfoil profile |
US11459892B1 (en) * | 2021-04-30 | 2022-10-04 | General Electric Company | Compressor stator vane airfoils |
Family Cites Families (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2934259A (en) * | 1956-06-18 | 1960-04-26 | United Aircraft Corp | Compressor blading |
US3333817A (en) * | 1965-04-01 | 1967-08-01 | Bbc Brown Boveri & Cie | Blading structure for axial flow turbo-machines |
JPS55123301A (en) * | 1979-03-16 | 1980-09-22 | Hitachi Ltd | Turbine blade |
DE3029082C2 (de) * | 1980-07-31 | 1982-10-21 | Kraftwerk Union AG, 4330 Mülheim | Turbomaschinenschaufel |
DE3201436C1 (de) * | 1982-01-19 | 1983-04-21 | Kraftwerk Union AG, 4330 Mülheim | Turbomaschinenschaufel |
IE54653B1 (en) * | 1982-10-22 | 1989-12-20 | Westinghouse Electric Corp | Rotor blade for the first stage of a combustion turbine |
US4533298A (en) * | 1982-12-02 | 1985-08-06 | Westinghouse Electric Corp. | Turbine blade with integral shroud |
US4824328A (en) * | 1987-05-22 | 1989-04-25 | Westinghouse Electric Corp. | Turbine blade attachment |
US4765046A (en) * | 1987-05-22 | 1988-08-23 | Westinghouse Electric Corp. | Row assembly process for integral shroud blades |
US4919593A (en) * | 1988-08-30 | 1990-04-24 | Westinghouse Electric Corp. | Retrofitted rotor blades for steam turbines and method of making the same |
US4900230A (en) * | 1989-04-27 | 1990-02-13 | Westinghouse Electric Corp. | Low pressure end blade for a low pressure steam turbine |
SU1751430A1 (ru) * | 1989-05-03 | 1992-07-30 | Харьковский авиационный институт им.Н.Е.Жуковского | Лопатка осевого компрессора |
US5035578A (en) * | 1989-10-16 | 1991-07-30 | Westinghouse Electric Corp. | Blading for reaction turbine blade row |
US5088894A (en) * | 1990-05-02 | 1992-02-18 | Westinghouse Electric Corp. | Turbomachine blade fastening |
US5221181A (en) * | 1990-10-24 | 1993-06-22 | Westinghouse Electric Corp. | Stationary turbine blade having diaphragm construction |
US5211703A (en) * | 1990-10-24 | 1993-05-18 | Westinghouse Electric Corp. | Stationary blade design for L-OC row |
US5192190A (en) * | 1990-12-06 | 1993-03-09 | Westinghouse Electric Corp. | Envelope forged stationary blade for L-2C row |
US5156529A (en) * | 1991-03-28 | 1992-10-20 | Westinghouse Electric Corp. | Integral shroud blade design |
US5203676A (en) * | 1992-03-05 | 1993-04-20 | Westinghouse Electric Corp. | Ruggedized tapered twisted integral shroud blade |
US5277549A (en) * | 1992-03-16 | 1994-01-11 | Westinghouse Electric Corp. | Controlled reaction L-2R steam turbine blade |
-
1993
- 1993-11-24 US US08/157,714 patent/US5352092A/en not_active Expired - Fee Related
- 1993-12-09 US US08/164,372 patent/US5354178A/en not_active Expired - Fee Related
-
1994
- 1994-11-23 EP EP94308637A patent/EP0654585B1/de not_active Expired - Lifetime
- 1994-11-23 DE DE69423180T patent/DE69423180T2/de not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP0654585B1 (de) | 2000-03-01 |
DE69423180T2 (de) | 2000-08-17 |
US5352092A (en) | 1994-10-04 |
US5354178A (en) | 1994-10-11 |
EP0654585A1 (de) | 1995-05-24 |
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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 |