EP2241723A4 - Turbine blade-cascade end wall - Google Patents
Turbine blade-cascade end wallInfo
- Publication number
- EP2241723A4 EP2241723A4 EP08872470A EP08872470A EP2241723A4 EP 2241723 A4 EP2241723 A4 EP 2241723A4 EP 08872470 A EP08872470 A EP 08872470A EP 08872470 A EP08872470 A EP 08872470A EP 2241723 A4 EP2241723 A4 EP 2241723A4
- Authority
- EP
- European Patent Office
- Prior art keywords
- end wall
- turbine blade
- cascade end
- cascade
- turbine
- 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.)
- Granted
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
- F01D9/02—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
- F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
-
- 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
- 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
- F01D5/142—Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
- F01D5/143—Contour of the outer or inner working fluid flow path wall, i.e. shroud or hub contour
-
- 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
- F01D5/145—Means for influencing boundary layers or secondary circulations
-
- 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
-
- 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
- F05D2250/711—Shape curved convex
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Hydraulic Turbines (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2008030937A JP5291355B2 (en) | 2008-02-12 | 2008-02-12 | Turbine cascade endwall |
PCT/JP2008/067231 WO2009101722A1 (en) | 2008-02-12 | 2008-09-25 | Turbine blade-cascade end wall |
Publications (3)
Publication Number | Publication Date |
---|---|
EP2241723A1 EP2241723A1 (en) | 2010-10-20 |
EP2241723A4 true EP2241723A4 (en) | 2013-03-06 |
EP2241723B1 EP2241723B1 (en) | 2014-08-13 |
Family
ID=40956766
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP08872470.3A Active EP2241723B1 (en) | 2008-02-12 | 2008-09-25 | Turbine blade-cascade end wall |
Country Status (6)
Country | Link |
---|---|
US (1) | US20100284818A1 (en) |
EP (1) | EP2241723B1 (en) |
JP (1) | JP5291355B2 (en) |
KR (1) | KR20100097757A (en) |
CN (1) | CN101925723B (en) |
WO (1) | WO2009101722A1 (en) |
Families Citing this family (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8403645B2 (en) | 2009-09-16 | 2013-03-26 | United Technologies Corporation | Turbofan flow path trenches |
FR2950942B1 (en) * | 2009-10-02 | 2013-08-02 | Snecma | ROTOR OF A TURBOMACHINE COMPRESSOR WITH OPTIMIZED INTERNAL END WALL |
JP2012233406A (en) * | 2011-04-28 | 2012-11-29 | Hitachi Ltd | Gas turbine stator vane |
JP5842382B2 (en) | 2011-05-13 | 2016-01-13 | 株式会社Ihi | Gas turbine engine |
US8915706B2 (en) | 2011-10-18 | 2014-12-23 | General Electric Company | Transition nozzle |
US8967959B2 (en) | 2011-10-28 | 2015-03-03 | General Electric Company | Turbine of a turbomachine |
US9051843B2 (en) | 2011-10-28 | 2015-06-09 | General Electric Company | Turbomachine blade including a squeeler pocket |
US8992179B2 (en) * | 2011-10-28 | 2015-03-31 | General Electric Company | Turbine of a turbomachine |
US9255480B2 (en) | 2011-10-28 | 2016-02-09 | General Electric Company | Turbine of a turbomachine |
CN102536329B (en) * | 2011-12-31 | 2014-04-02 | 西北工业大学 | Modeling method for axis-asymmetric end wall of annular blade grid of air compressor or turbine |
US9103213B2 (en) | 2012-02-29 | 2015-08-11 | General Electric Company | Scalloped surface turbine stage with purge trough |
US9085985B2 (en) | 2012-03-23 | 2015-07-21 | General Electric Company | Scalloped surface turbine stage |
US9267386B2 (en) | 2012-06-29 | 2016-02-23 | United Technologies Corporation | Fairing assembly |
EP2696029B1 (en) * | 2012-08-09 | 2015-10-07 | MTU Aero Engines AG | Blade row with side wall contours and fluid flow engine |
SG11201407843UA (en) | 2012-08-17 | 2015-03-30 | United Technologies Corp | Contoured flowpath surface |
CN106089806A (en) * | 2016-05-30 | 2016-11-09 | 西北工业大学 | A kind of diffuser that reduces separates the end wall processing method of loss |
DE102016211315A1 (en) | 2016-06-23 | 2017-12-28 | MTU Aero Engines AG | Runner or vane with raised areas |
ES2819128T3 (en) * | 2017-03-03 | 2021-04-15 | MTU Aero Engines AG | Contouring of a pallet from a pallet rack |
EP3404211A1 (en) * | 2017-05-15 | 2018-11-21 | MTU Aero Engines GmbH | Blade cascade segment for a turbine with contoured platform surface, corresponding blade cascade, blade channel, platform, turbine and aircraft engine |
EP3404210A1 (en) * | 2017-05-15 | 2018-11-21 | MTU Aero Engines GmbH | Blade cascade segment for a turbomachine with non-axisymmetric platform surface, corresponding blade cascade, blade channel, platform, and turbomachine |
WO2019190539A1 (en) * | 2018-03-30 | 2019-10-03 | Siemens Aktiengesellschaft | Turbine stage platform with endwall contouring incorporating wavy mate face |
US11639666B2 (en) | 2021-09-03 | 2023-05-02 | Pratt & Whitney Canada Corp. | Stator with depressions in gaspath wall adjacent leading edges |
US11415012B1 (en) * | 2021-09-03 | 2022-08-16 | Pratt & Whitney Canada Corp. | Tandem stator with depressions in gaspath wall |
CN114542502B (en) * | 2022-01-26 | 2023-05-26 | 西北工业大学 | Adjustable compressor/turbine blade cascade experimental device of blade cascade front end wall vortex generator |
DE102022113750A1 (en) * | 2022-05-31 | 2023-11-30 | MTU Aero Engines AG | Annulus contouring |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB944166A (en) * | 1960-03-02 | 1963-12-11 | Werner Hausammann | Rotor for turbines or compressors |
WO2006067359A1 (en) * | 2004-12-21 | 2006-06-29 | Honeywell International, Inc. | Turbine wheel with backswept inducer |
EP1681438A2 (en) * | 2004-12-24 | 2006-07-19 | The General Electric Company | Turbine stage with scalloped surface platform |
JP2007247542A (en) * | 2006-03-16 | 2007-09-27 | Mitsubishi Heavy Ind Ltd | Turbine blade cascade end wall |
US20070258819A1 (en) * | 2006-05-02 | 2007-11-08 | United Technologies Corporation | Airfoil array with an endwall protrusion and components of the array |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB9417406D0 (en) * | 1994-08-30 | 1994-10-19 | Gec Alsthom Ltd | Turbine blade |
DE19650656C1 (en) * | 1996-12-06 | 1998-06-10 | Mtu Muenchen Gmbh | Turbo machine with transonic compressor stage |
CN2288271Y (en) * | 1997-05-13 | 1998-08-19 | 北京全三维动力工程有限公司 | Cambered stator blade grid for tangential turbine |
GB9823840D0 (en) | 1998-10-30 | 1998-12-23 | Rolls Royce Plc | Bladed ducting for turbomachinery |
US6419446B1 (en) * | 1999-08-05 | 2002-07-16 | United Technologies Corporation | Apparatus and method for inhibiting radial transfer of core gas flow within a core gas flow path of a gas turbine engine |
US6669445B2 (en) * | 2002-03-07 | 2003-12-30 | United Technologies Corporation | Endwall shape for use in turbomachinery |
US6969232B2 (en) * | 2002-10-23 | 2005-11-29 | United Technologies Corporation | Flow directing device |
JP4346412B2 (en) * | 2003-10-31 | 2009-10-21 | 株式会社東芝 | Turbine cascade |
EP1760257B1 (en) * | 2004-09-24 | 2012-12-26 | IHI Corporation | Wall shape of axial flow machine and gas turbine engine |
US7220100B2 (en) * | 2005-04-14 | 2007-05-22 | General Electric Company | Crescentic ramp turbine stage |
GB0518628D0 (en) * | 2005-09-13 | 2005-10-19 | Rolls Royce Plc | Axial compressor blading |
-
2008
- 2008-02-12 JP JP2008030937A patent/JP5291355B2/en active Active
- 2008-09-25 CN CN200880125635.7A patent/CN101925723B/en active Active
- 2008-09-25 US US12/812,115 patent/US20100284818A1/en not_active Abandoned
- 2008-09-25 EP EP08872470.3A patent/EP2241723B1/en active Active
- 2008-09-25 WO PCT/JP2008/067231 patent/WO2009101722A1/en active Application Filing
- 2008-09-25 KR KR1020107016954A patent/KR20100097757A/en active Search and Examination
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB944166A (en) * | 1960-03-02 | 1963-12-11 | Werner Hausammann | Rotor for turbines or compressors |
WO2006067359A1 (en) * | 2004-12-21 | 2006-06-29 | Honeywell International, Inc. | Turbine wheel with backswept inducer |
EP1681438A2 (en) * | 2004-12-24 | 2006-07-19 | The General Electric Company | Turbine stage with scalloped surface platform |
JP2007247542A (en) * | 2006-03-16 | 2007-09-27 | Mitsubishi Heavy Ind Ltd | Turbine blade cascade end wall |
US20070258819A1 (en) * | 2006-05-02 | 2007-11-08 | United Technologies Corporation | Airfoil array with an endwall protrusion and components of the array |
Non-Patent Citations (2)
Title |
---|
ROSE M ET AL: "THE EFFECT OF END-WALL PROFILING ON SECONDARY FLOW AND LOSS DEVELOPMENT IN A TURBINE CASCADE", PROCEEDINGS OF ASME TURBO EXPO 2002, GT-2002-30339, ASME,, 3 June 2002 (2002-06-03), pages 135 - 145, XP008138428 * |
See also references of WO2009101722A1 * |
Also Published As
Publication number | Publication date |
---|---|
CN101925723A (en) | 2010-12-22 |
WO2009101722A1 (en) | 2009-08-20 |
JP2009191656A (en) | 2009-08-27 |
CN101925723B (en) | 2016-06-01 |
JP5291355B2 (en) | 2013-09-18 |
EP2241723B1 (en) | 2014-08-13 |
US20100284818A1 (en) | 2010-11-11 |
EP2241723A1 (en) | 2010-10-20 |
CN104165070A (en) | 2014-11-26 |
KR20100097757A (en) | 2010-09-03 |
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