JP4386891B2 - 傾斜スキーラ先端を有するタービンブレード - Google Patents
傾斜スキーラ先端を有するタービンブレード Download PDFInfo
- Publication number
- JP4386891B2 JP4386891B2 JP2005507636A JP2005507636A JP4386891B2 JP 4386891 B2 JP4386891 B2 JP 4386891B2 JP 2005507636 A JP2005507636 A JP 2005507636A JP 2005507636 A JP2005507636 A JP 2005507636A JP 4386891 B2 JP4386891 B2 JP 4386891B2
- Authority
- JP
- Japan
- Prior art keywords
- tip
- rib
- tip rib
- turbine blade
- 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.)
- Expired - Fee Related
Links
- 238000001816 cooling Methods 0.000 claims description 27
- 239000000567 combustion gas Substances 0.000 claims description 26
- 239000007789 gas Substances 0.000 claims description 9
- 230000004323 axial length Effects 0.000 claims description 7
- 230000001154 acute effect Effects 0.000 description 5
- 238000012986 modification Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000011144 upstream manufacturing Methods 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 230000008646 thermal stress 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
- F01D5/14—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
- F01D5/145—Means for influencing boundary layers or secondary circulations
-
- 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
- F01D5/20—Specially-shaped blade tips to seal space between tips and stator
-
- 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
- F05D2250/20—Three-dimensional
- F05D2250/29—Three-dimensional machined; miscellaneous
- F05D2250/292—Three-dimensional machined; miscellaneous tapered
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/196,623 US6672829B1 (en) | 2002-07-16 | 2002-07-16 | Turbine blade having angled squealer tip |
| PCT/US2003/022663 WO2005014978A1 (en) | 2002-07-16 | 2003-07-16 | Turbine blade having angled squealer tip |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2006511757A JP2006511757A (ja) | 2006-04-06 |
| JP2006511757A5 JP2006511757A5 (enExample) | 2006-09-07 |
| JP4386891B2 true JP4386891B2 (ja) | 2009-12-16 |
Family
ID=29735375
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2005507636A Expired - Fee Related JP4386891B2 (ja) | 2002-07-16 | 2003-07-16 | 傾斜スキーラ先端を有するタービンブレード |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US6672829B1 (enExample) |
| EP (1) | EP1529153B1 (enExample) |
| JP (1) | JP4386891B2 (enExample) |
| DE (1) | DE60321575D1 (enExample) |
| WO (1) | WO2005014978A1 (enExample) |
Families Citing this family (90)
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|---|---|---|---|---|
| GB2387186B (en) * | 2002-03-18 | 2005-10-26 | Bj Services Co | Conductor torquing system |
| GB0228443D0 (en) * | 2002-12-06 | 2003-01-08 | Rolls Royce Plc | Blade cooling |
| US6790005B2 (en) * | 2002-12-30 | 2004-09-14 | General Electric Company | Compound tip notched blade |
| US6991430B2 (en) * | 2003-04-07 | 2006-01-31 | General Electric Company | Turbine blade with recessed squealer tip and shelf |
| US7147440B2 (en) * | 2003-10-31 | 2006-12-12 | General Electric Company | Methods and apparatus for cooling gas turbine engine rotor assemblies |
| US7029235B2 (en) * | 2004-04-30 | 2006-04-18 | Siemens Westinghouse Power Corporation | Cooling system for a tip of a turbine blade |
| US7118337B2 (en) * | 2004-06-17 | 2006-10-10 | Siemens Power Generation, Inc. | Gas turbine airfoil trailing edge corner |
| US7097419B2 (en) | 2004-07-26 | 2006-08-29 | General Electric Company | Common tip chamber blade |
| EP1624192A1 (de) * | 2004-08-06 | 2006-02-08 | Siemens Aktiengesellschaft | Verdichterschaufel für einen Verdichter und Verdichter |
| US7118342B2 (en) * | 2004-09-09 | 2006-10-10 | General Electric Company | Fluted tip turbine blade |
| US7320575B2 (en) * | 2004-09-28 | 2008-01-22 | General Electric Company | Methods and apparatus for aerodynamically self-enhancing rotor blades |
| US7270514B2 (en) * | 2004-10-21 | 2007-09-18 | General Electric Company | Turbine blade tip squealer and rebuild method |
| FR2885645A1 (fr) * | 2005-05-13 | 2006-11-17 | Snecma Moteurs Sa | Aube creuse de rotor pour la turbine d'un moteur a turbine a gaz, equipee d'une baignoire |
| FR2887581A1 (fr) * | 2005-06-24 | 2006-12-29 | Snecma Moteurs Sa | Aube creuse de turbomachine |
| US7510376B2 (en) * | 2005-08-25 | 2009-03-31 | General Electric Company | Skewed tip hole turbine blade |
| US7290986B2 (en) * | 2005-09-09 | 2007-11-06 | General Electric Company | Turbine airfoil with curved squealer tip |
| US7281894B2 (en) * | 2005-09-09 | 2007-10-16 | General Electric Company | Turbine airfoil curved squealer tip with tip shelf |
| EP1764477B1 (en) | 2005-09-14 | 2008-07-02 | General Electric Company | Fluted tip turbine blade |
| FR2891003B1 (fr) * | 2005-09-20 | 2011-05-06 | Snecma | Aube de turbomachine |
| US7287959B2 (en) * | 2005-12-05 | 2007-10-30 | General Electric Company | Blunt tip turbine blade |
| US7473073B1 (en) * | 2006-06-14 | 2009-01-06 | Florida Turbine Technologies, Inc. | Turbine blade with cooled tip rail |
| US7695243B2 (en) | 2006-07-27 | 2010-04-13 | General Electric Company | Dust hole dome blade |
| US7607893B2 (en) * | 2006-08-21 | 2009-10-27 | General Electric Company | Counter tip baffle airfoil |
| US8512003B2 (en) * | 2006-08-21 | 2013-08-20 | General Electric Company | Tip ramp turbine blade |
| US8500396B2 (en) * | 2006-08-21 | 2013-08-06 | General Electric Company | Cascade tip baffle airfoil |
| US7686578B2 (en) * | 2006-08-21 | 2010-03-30 | General Electric Company | Conformal tip baffle airfoil |
| US8632311B2 (en) * | 2006-08-21 | 2014-01-21 | General Electric Company | Flared tip turbine blade |
| US7597539B1 (en) | 2006-09-27 | 2009-10-06 | Florida Turbine Technologies, Inc. | Turbine blade with vortex cooled end tip rail |
| FR2907157A1 (fr) * | 2006-10-13 | 2008-04-18 | Snecma Sa | Aube mobile de turbomachine |
| US8425183B2 (en) | 2006-11-20 | 2013-04-23 | General Electric Company | Triforial tip cavity airfoil |
| US7857587B2 (en) * | 2006-11-30 | 2010-12-28 | General Electric Company | Turbine blades and turbine blade cooling systems and methods |
| US8016565B2 (en) * | 2007-05-31 | 2011-09-13 | General Electric Company | Methods and apparatus for assembling gas turbine engines |
| FR2934008B1 (fr) * | 2008-07-21 | 2015-06-05 | Turbomeca | Aube creuse de roue de turbine comportant une nervure |
| US8480372B2 (en) * | 2008-11-06 | 2013-07-09 | General Electric Company | System and method for reducing bucket tip losses |
| US8092178B2 (en) * | 2008-11-28 | 2012-01-10 | Pratt & Whitney Canada Corp. | Turbine blade for a gas turbine engine |
| US20100135822A1 (en) * | 2008-11-28 | 2010-06-03 | Remo Marini | Turbine blade for a gas turbine engine |
| US8092179B2 (en) * | 2009-03-12 | 2012-01-10 | United Technologies Corporation | Blade tip cooling groove |
| US8172507B2 (en) * | 2009-05-12 | 2012-05-08 | Siemens Energy, Inc. | Gas turbine blade with double impingement cooled single suction side tip rail |
| US8157505B2 (en) * | 2009-05-12 | 2012-04-17 | Siemens Energy, Inc. | Turbine blade with single tip rail with a mid-positioned deflector portion |
| US8186965B2 (en) * | 2009-05-27 | 2012-05-29 | General Electric Company | Recovery tip turbine blade |
| US8313287B2 (en) | 2009-06-17 | 2012-11-20 | Siemens Energy, Inc. | Turbine blade squealer tip rail with fence members |
| US8182221B1 (en) * | 2009-07-29 | 2012-05-22 | Florida Turbine Technologies, Inc. | Turbine blade with tip sealing and cooling |
| US8777567B2 (en) | 2010-09-22 | 2014-07-15 | Honeywell International Inc. | Turbine blades, turbine assemblies, and methods of manufacturing turbine blades |
| DE102010050712A1 (de) | 2010-11-08 | 2012-05-10 | Mtu Aero Engines Gmbh | Bauelement einer Strömungsmaschine und Verfahren zum generativen Herstellen eines derartigen Bauelementes |
| US9181814B2 (en) | 2010-11-24 | 2015-11-10 | United Technology Corporation | Turbine engine compressor stator |
| FR2982903B1 (fr) * | 2011-11-17 | 2014-02-21 | Snecma | Aube de turbine a gaz a decalage vers l'intrados des sections de tete et a canaux de refroidissement |
| US9328617B2 (en) | 2012-03-20 | 2016-05-03 | United Technologies Corporation | Trailing edge or tip flag antiflow separation |
| US9228442B2 (en) * | 2012-04-05 | 2016-01-05 | United Technologies Corporation | Turbine airfoil tip shelf and squealer pocket cooling |
| US9284845B2 (en) | 2012-04-05 | 2016-03-15 | United Technologies Corporation | Turbine airfoil tip shelf and squealer pocket cooling |
| US9470096B2 (en) | 2012-07-26 | 2016-10-18 | General Electric Company | Turbine bucket with notched squealer tip |
| US9045988B2 (en) | 2012-07-26 | 2015-06-02 | General Electric Company | Turbine bucket with squealer tip |
| US10408066B2 (en) | 2012-08-15 | 2019-09-10 | United Technologies Corporation | Suction side turbine blade tip cooling |
| US9482101B2 (en) | 2012-11-28 | 2016-11-01 | United Technologies Corporation | Trailing edge and tip cooling |
| US10655473B2 (en) * | 2012-12-13 | 2020-05-19 | United Technologies Corporation | Gas turbine engine turbine blade leading edge tip trench cooling |
| US9453419B2 (en) * | 2012-12-28 | 2016-09-27 | United Technologies Corporation | Gas turbine engine turbine blade tip cooling |
| US8920124B2 (en) | 2013-02-14 | 2014-12-30 | Siemens Energy, Inc. | Turbine blade with contoured chamfered squealer tip |
| US10760499B2 (en) * | 2013-03-14 | 2020-09-01 | Pratt & Whitney Canada Corp. | Turbo-machinery rotors with rounded tip edge |
| US9856739B2 (en) * | 2013-09-18 | 2018-01-02 | Honeywell International Inc. | Turbine blades with tip portions having converging cooling holes |
| EP3055507B1 (en) * | 2013-10-08 | 2020-01-01 | United Technologies Corporation | Rotor blade with compound lean contour and corresponding gas turbine engine |
| US9879544B2 (en) | 2013-10-16 | 2018-01-30 | Honeywell International Inc. | Turbine rotor blades with improved tip portion cooling holes |
| US9816389B2 (en) | 2013-10-16 | 2017-11-14 | Honeywell International Inc. | Turbine rotor blades with tip portion parapet wall cavities |
| US9638041B2 (en) | 2013-10-23 | 2017-05-02 | General Electric Company | Turbine bucket having non-axisymmetric base contour |
| US9528379B2 (en) | 2013-10-23 | 2016-12-27 | General Electric Company | Turbine bucket having serpentine core |
| US9797258B2 (en) | 2013-10-23 | 2017-10-24 | General Electric Company | Turbine bucket including cooling passage with turn |
| US9670784B2 (en) | 2013-10-23 | 2017-06-06 | General Electric Company | Turbine bucket base having serpentine cooling passage with leading edge cooling |
| US9551226B2 (en) | 2013-10-23 | 2017-01-24 | General Electric Company | Turbine bucket with endwall contour and airfoil profile |
| US20150110617A1 (en) * | 2013-10-23 | 2015-04-23 | General Electric Company | Turbine airfoil including tip fillet |
| US10626730B2 (en) | 2013-12-17 | 2020-04-21 | United Technologies Corporation | Enhanced cooling for blade tip |
| EP3094824B1 (en) | 2014-01-17 | 2018-11-07 | General Electric Company | Ceramic matrix composite turbine blade squealer tip with flare and method thereof |
| US10041358B2 (en) | 2014-05-08 | 2018-08-07 | United Technologies Corporation | Gas turbine engine blade squealer pockets |
| JP6462332B2 (ja) * | 2014-11-20 | 2019-01-30 | 三菱重工業株式会社 | タービン動翼及びガスタービン |
| US10196913B1 (en) * | 2014-12-17 | 2019-02-05 | United Technologies Corporation | Featherseal having tapered radial portion |
| US10107108B2 (en) * | 2015-04-29 | 2018-10-23 | General Electric Company | Rotor blade having a flared tip |
| US10053992B2 (en) | 2015-07-02 | 2018-08-21 | United Technologies Corporation | Gas turbine engine airfoil squealer pocket cooling hole configuration |
| FR3043715B1 (fr) * | 2015-11-16 | 2020-11-06 | Snecma | Aube de turbine comprenant une pale avec baignoire comportant un intrados incurve dans la region du sommet de pale |
| US10253637B2 (en) | 2015-12-11 | 2019-04-09 | General Electric Company | Method and system for improving turbine blade performance |
| US10633983B2 (en) | 2016-03-07 | 2020-04-28 | General Electric Company | Airfoil tip geometry to reduce blade wear in gas turbine engines |
| US10385865B2 (en) | 2016-03-07 | 2019-08-20 | General Electric Company | Airfoil tip geometry to reduce blade wear in gas turbine engines |
| US10184342B2 (en) | 2016-04-14 | 2019-01-22 | General Electric Company | System for cooling seal rails of tip shroud of turbine blade |
| FR3053386B1 (fr) * | 2016-06-29 | 2020-03-20 | Safran Helicopter Engines | Roue de turbine |
| US10648346B2 (en) * | 2016-07-06 | 2020-05-12 | General Electric Company | Shroud configurations for turbine rotor blades |
| US10533429B2 (en) * | 2017-02-27 | 2020-01-14 | Rolls-Royce Corporation | Tip structure for a turbine blade with pressure side and suction side rails |
| US11434770B2 (en) | 2017-03-28 | 2022-09-06 | Raytheon Technologies Corporation | Tip cooling design |
| US11319819B2 (en) * | 2017-05-30 | 2022-05-03 | Siemens Energy Global GmbH & Co. KG | Turbine blade with squealer tip and densified oxide dispersion strengthened layer |
| JP6979382B2 (ja) * | 2018-03-29 | 2021-12-15 | 三菱重工業株式会社 | タービン動翼、及びガスタービン |
| US10787932B2 (en) | 2018-07-13 | 2020-09-29 | Honeywell International Inc. | Turbine blade with dust tolerant cooling system |
| US11118462B2 (en) * | 2019-01-24 | 2021-09-14 | Pratt & Whitney Canada Corp. | Blade tip pocket rib |
| US11371359B2 (en) | 2020-11-26 | 2022-06-28 | Pratt & Whitney Canada Corp. | Turbine blade for a gas turbine engine |
| HUE070259T2 (hu) * | 2020-12-08 | 2025-05-28 | General Electric Technology Gmbh | Eljárások kiugró szakasszal rendelkezõ alkatrész megalkotására vagy javítására, és a kapcsolódó turbógépalkatrész |
| CN116537886B (zh) * | 2023-06-14 | 2025-11-07 | 西北工业大学 | 一种具有提高冷却效率的叶顶结构及叶片 |
Family Cites Families (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1828409A (en) * | 1929-01-11 | 1931-10-20 | Westinghouse Electric & Mfg Co | Reaction blading |
| US5261789A (en) | 1992-08-25 | 1993-11-16 | General Electric Company | Tip cooled blade |
| JP3137527B2 (ja) | 1994-04-21 | 2001-02-26 | 三菱重工業株式会社 | ガスタービン動翼チップ冷却装置 |
| US5458461A (en) | 1994-12-12 | 1995-10-17 | General Electric Company | Film cooled slotted wall |
| JP3453268B2 (ja) | 1997-03-04 | 2003-10-06 | 三菱重工業株式会社 | ガスタービン翼 |
| US6027306A (en) | 1997-06-23 | 2000-02-22 | General Electric Company | Turbine blade tip flow discouragers |
| EP0945593B1 (de) | 1998-03-23 | 2003-05-07 | ALSTOM (Switzerland) Ltd | Filmkühlungsbohrung |
| US6176678B1 (en) | 1998-11-06 | 2001-01-23 | General Electric Company | Apparatus and methods for turbine blade cooling |
| US6059530A (en) | 1998-12-21 | 2000-05-09 | General Electric Company | Twin rib turbine blade |
| US6190129B1 (en) | 1998-12-21 | 2001-02-20 | General Electric Company | Tapered tip-rib turbine blade |
| US6086328A (en) | 1998-12-21 | 2000-07-11 | General Electric Company | Tapered tip turbine blade |
| US6179556B1 (en) | 1999-06-01 | 2001-01-30 | General Electric Company | Turbine blade tip with offset squealer |
| US6224336B1 (en) | 1999-06-09 | 2001-05-01 | General Electric Company | Triple tip-rib airfoil |
| JP2001055902A (ja) * | 1999-08-18 | 2001-02-27 | Toshiba Corp | タービン動翼 |
| US6164914A (en) | 1999-08-23 | 2000-12-26 | General Electric Company | Cool tip blade |
| US6382913B1 (en) | 2001-02-09 | 2002-05-07 | General Electric Company | Method and apparatus for reducing turbine blade tip region temperatures |
-
2002
- 2002-07-16 US US10/196,623 patent/US6672829B1/en not_active Expired - Lifetime
-
2003
- 2003-07-16 WO PCT/US2003/022663 patent/WO2005014978A1/en not_active Ceased
- 2003-07-16 EP EP03816841A patent/EP1529153B1/en not_active Expired - Lifetime
- 2003-07-16 JP JP2005507636A patent/JP4386891B2/ja not_active Expired - Fee Related
- 2003-07-16 DE DE60321575T patent/DE60321575D1/de not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| JP2006511757A (ja) | 2006-04-06 |
| DE60321575D1 (de) | 2008-07-24 |
| US20040013515A1 (en) | 2004-01-22 |
| WO2005014978A1 (en) | 2005-02-17 |
| EP1529153A1 (en) | 2005-05-11 |
| US6672829B1 (en) | 2004-01-06 |
| EP1529153B1 (en) | 2008-06-11 |
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| LAPS | Cancellation because of no payment of annual fees |