JP2005030403A - タービンバケット用の翼形部形状 - Google Patents
タービンバケット用の翼形部形状 Download PDFInfo
- Publication number
- JP2005030403A JP2005030403A JP2004202671A JP2004202671A JP2005030403A JP 2005030403 A JP2005030403 A JP 2005030403A JP 2004202671 A JP2004202671 A JP 2004202671A JP 2004202671 A JP2004202671 A JP 2004202671A JP 2005030403 A JP2005030403 A JP 2005030403A
- Authority
- JP
- Japan
- Prior art keywords
- airfoil
- distance
- inches
- turbine
- bucket
- 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.)
- Withdrawn
Links
- 238000004519 manufacturing process Methods 0.000 description 4
- 238000000576 coating method Methods 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 238000004904 shortening Methods 0.000 description 2
- 239000011248 coating agent Substances 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000010348 incorporation Methods 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 230000013011 mating 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
- F01D5/18—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
- 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
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/202—Heat transfer, e.g. cooling by film cooling
-
- 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
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S416/00—Fluid reaction surfaces, i.e. impellers
- Y10S416/02—Formulas of curves
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Materials For Photolithography (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/616,911 US6769879B1 (en) | 2003-07-11 | 2003-07-11 | Airfoil shape for a turbine bucket |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JP2005030403A true JP2005030403A (ja) | 2005-02-03 |
| JP2005030403A5 JP2005030403A5 (enExample) | 2007-08-16 |
Family
ID=32772300
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2004202671A Withdrawn JP2005030403A (ja) | 2003-07-11 | 2004-07-09 | タービンバケット用の翼形部形状 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US6769879B1 (enExample) |
| EP (1) | EP1496202A1 (enExample) |
| JP (1) | JP2005030403A (enExample) |
| CN (1) | CN100362211C (enExample) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2021534346A (ja) * | 2018-08-21 | 2021-12-09 | クロマロイ ガス タービン エルエルシー | 改善された第1段タービンブレード |
Families Citing this family (42)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6854961B2 (en) * | 2003-05-29 | 2005-02-15 | General Electric Company | Airfoil shape for a turbine bucket |
| US6769879B1 (en) * | 2003-07-11 | 2004-08-03 | General Electric Company | Airfoil shape for a turbine bucket |
| US6857855B1 (en) * | 2003-08-04 | 2005-02-22 | General Electric Company | Airfoil shape for a turbine bucket |
| US7186090B2 (en) * | 2004-08-05 | 2007-03-06 | General Electric Company | Air foil shape for a compressor blade |
| ITMI20041804A1 (it) * | 2004-09-21 | 2004-12-21 | Nuovo Pignone Spa | Pala di un rutore di un primo stadio di una turbina a gas |
| US20060216144A1 (en) | 2005-03-28 | 2006-09-28 | Sullivan Michael A | First and second stage turbine airfoil shapes |
| US7722329B2 (en) | 2005-12-29 | 2010-05-25 | Rolls-Royce Power Engineering Plc | Airfoil for a third stage nozzle guide vane |
| US7625184B2 (en) * | 2005-12-29 | 2009-12-01 | Rolls-Royce Power Engineering Plc | Second stage turbine airfoil |
| US7648334B2 (en) * | 2005-12-29 | 2010-01-19 | Rolls-Royce Power Engineering Plc | Airfoil for a second stage nozzle guide vane |
| CA2633319C (en) * | 2005-12-29 | 2013-02-19 | Rolls-Royce Power Engineering Plc | First stage turbine airfoil |
| US7632072B2 (en) * | 2005-12-29 | 2009-12-15 | Rolls-Royce Power Engineering Plc | Third stage turbine airfoil |
| CA2633334C (en) | 2005-12-29 | 2014-11-25 | Rolls-Royce Power Engineering Plc | Airfoil for a first stage nozzle guide vane |
| US7329092B2 (en) * | 2006-01-27 | 2008-02-12 | General Electric Company | Stator blade airfoil profile for a compressor |
| US7329093B2 (en) * | 2006-01-27 | 2008-02-12 | General Electric Company | Nozzle blade airfoil profile for a turbine |
| US7306436B2 (en) * | 2006-03-02 | 2007-12-11 | Pratt & Whitney Canada Corp. | HP turbine blade airfoil profile |
| US7396211B2 (en) * | 2006-03-30 | 2008-07-08 | General Electric Company | Stator blade airfoil profile for a compressor |
| US7467926B2 (en) * | 2006-06-09 | 2008-12-23 | General Electric Company | Stator blade airfoil profile for a compressor |
| US7581930B2 (en) * | 2006-08-16 | 2009-09-01 | United Technologies Corporation | High lift transonic turbine blade |
| US7611326B2 (en) * | 2006-09-06 | 2009-11-03 | Pratt & Whitney Canada Corp. | HP turbine vane airfoil profile |
| US7572105B2 (en) * | 2006-10-25 | 2009-08-11 | General Electric Company | Airfoil shape for a compressor |
| US7566202B2 (en) * | 2006-10-25 | 2009-07-28 | General Electric Company | Airfoil shape for a compressor |
| US7517197B2 (en) * | 2006-10-25 | 2009-04-14 | General Electric Company | Airfoil shape for a compressor |
| US7510378B2 (en) * | 2006-10-25 | 2009-03-31 | General Electric Company | Airfoil shape for a compressor |
| US7513748B2 (en) * | 2006-10-25 | 2009-04-07 | General Electric Company | Airfoil shape for a compressor |
| US7572104B2 (en) * | 2006-10-25 | 2009-08-11 | General Electric Company | Airfoil shape for a compressor |
| US7568892B2 (en) * | 2006-11-02 | 2009-08-04 | General Electric Company | Airfoil shape for a compressor |
| US7497665B2 (en) * | 2006-11-02 | 2009-03-03 | General Electric Company | Airfoil shape for a compressor |
| US7559748B2 (en) * | 2006-11-28 | 2009-07-14 | Pratt & Whitney Canada Corp. | LP turbine blade airfoil profile |
| JP4665916B2 (ja) * | 2007-02-28 | 2011-04-06 | 株式会社日立製作所 | ガスタービンの第1段動翼 |
| US7862304B2 (en) * | 2007-10-12 | 2011-01-04 | Pratt & Whitney Canada Corp. | Compressor turbine blade airfoil profile |
| US7862303B2 (en) * | 2007-10-12 | 2011-01-04 | Pratt & Whitney Canada Corp. | Compressor turbine vane airfoil profile |
| US8007245B2 (en) * | 2007-11-29 | 2011-08-30 | General Electric Company | Shank shape for a turbine blade and turbine incorporating the same |
| CH699999A1 (de) * | 2008-11-26 | 2010-05-31 | Alstom Technology Ltd | Gekühlte schaufel für eine gasturbine. |
| US8393870B2 (en) | 2010-09-08 | 2013-03-12 | United Technologies Corporation | Turbine blade airfoil |
| US8602740B2 (en) | 2010-09-08 | 2013-12-10 | United Technologies Corporation | Turbine vane airfoil |
| EP2703600B1 (en) * | 2011-04-28 | 2024-01-17 | IHI Corporation | Turbine blade |
| US9011101B2 (en) * | 2011-11-28 | 2015-04-21 | General Electric Company | Turbine bucket airfoil profile |
| JP5999348B2 (ja) * | 2012-10-31 | 2016-09-28 | 株式会社Ihi | タービン翼 |
| US9896950B2 (en) * | 2013-09-09 | 2018-02-20 | Rolls-Royce Deutschland Ltd & Co Kg | Turbine guide wheel |
| CN103510998B (zh) * | 2013-09-26 | 2015-04-22 | 哈尔滨汽轮机厂有限责任公司 | 一种适用于20-30mw等级的燃机涡轮第一级动叶片 |
| US10480323B2 (en) | 2016-01-12 | 2019-11-19 | United Technologies Corporation | Gas turbine engine turbine blade airfoil profile |
| EP3502482B1 (en) * | 2017-12-20 | 2020-08-26 | Ansaldo Energia Switzerland AG | Compressor blade with modified stagger angle spanwise distribution |
Family Cites Families (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4431376A (en) * | 1980-10-27 | 1984-02-14 | United Technologies Corporation | Airfoil shape for arrays of airfoils |
| US5980209A (en) * | 1997-06-27 | 1999-11-09 | General Electric Co. | Turbine blade with enhanced cooling and profile optimization |
| US6461110B1 (en) * | 2001-07-11 | 2002-10-08 | General Electric Company | First-stage high pressure turbine bucket airfoil |
| DE10039642C2 (de) * | 2000-08-14 | 2002-06-13 | Honda Motor Co Ltd | Turbinenblattluftflügel und Turbinenblatt für eine Axialstromturbine |
| DE10054244C2 (de) * | 2000-11-02 | 2002-10-10 | Honda Motor Co Ltd | Turbinenblattanordnung und Turbinenblatt für eine Axialturbine |
| US6474948B1 (en) * | 2001-06-22 | 2002-11-05 | General Electric Company | Third-stage turbine bucket airfoil |
| US6450770B1 (en) * | 2001-06-28 | 2002-09-17 | General Electric Company | Second-stage turbine bucket airfoil |
| US6503059B1 (en) * | 2001-07-06 | 2003-01-07 | General Electric Company | Fourth-stage turbine bucket airfoil |
| US6558122B1 (en) * | 2001-11-14 | 2003-05-06 | General Electric Company | Second-stage turbine bucket airfoil |
| US6685434B1 (en) * | 2002-09-17 | 2004-02-03 | General Electric Company | Second stage turbine bucket airfoil |
| US6715990B1 (en) * | 2002-09-19 | 2004-04-06 | General Electric Company | First stage turbine bucket airfoil |
| US6722852B1 (en) * | 2002-11-22 | 2004-04-20 | General Electric Company | Third stage turbine bucket airfoil |
| US6722851B1 (en) * | 2003-03-12 | 2004-04-20 | General Electric Company | Internal core profile for a turbine bucket |
| US6779980B1 (en) * | 2003-03-13 | 2004-08-24 | General Electric Company | Airfoil shape for a turbine bucket |
| US6739838B1 (en) * | 2003-03-17 | 2004-05-25 | General Electric Company | Airfoil shape for a turbine bucket |
| US6739839B1 (en) * | 2003-03-31 | 2004-05-25 | General Electric Company | First-stage high pressure turbine bucket airfoil |
| US6769879B1 (en) * | 2003-07-11 | 2004-08-03 | General Electric Company | Airfoil shape for a turbine bucket |
-
2003
- 2003-07-11 US US10/616,911 patent/US6769879B1/en not_active Expired - Lifetime
-
2004
- 2004-07-07 EP EP04254059A patent/EP1496202A1/en not_active Withdrawn
- 2004-07-09 JP JP2004202671A patent/JP2005030403A/ja not_active Withdrawn
- 2004-07-12 CN CNB2004100635843A patent/CN100362211C/zh not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2021534346A (ja) * | 2018-08-21 | 2021-12-09 | クロマロイ ガス タービン エルエルシー | 改善された第1段タービンブレード |
| JP7358455B2 (ja) | 2018-08-21 | 2023-10-10 | クロマロイ ガス タービン エルエルシー | 改善された第1段タービンブレード |
Also Published As
| Publication number | Publication date |
|---|---|
| CN100362211C (zh) | 2008-01-16 |
| US6769879B1 (en) | 2004-08-03 |
| CN1576516A (zh) | 2005-02-09 |
| EP1496202A1 (en) | 2005-01-12 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| A521 | Written amendment |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20070629 |
|
| A621 | Written request for application examination |
Free format text: JAPANESE INTERMEDIATE CODE: A621 Effective date: 20070629 |
|
| A761 | Written withdrawal of application |
Free format text: JAPANESE INTERMEDIATE CODE: A761 Effective date: 20090917 |