JP2005054791A - タービンノズル用の翼形形状 - Google Patents
タービンノズル用の翼形形状 Download PDFInfo
- Publication number
- JP2005054791A JP2005054791A JP2004223008A JP2004223008A JP2005054791A JP 2005054791 A JP2005054791 A JP 2005054791A JP 2004223008 A JP2004223008 A JP 2004223008A JP 2004223008 A JP2004223008 A JP 2004223008A JP 2005054791 A JP2005054791 A JP 2005054791A
- Authority
- JP
- Japan
- Prior art keywords
- airfoil
- turbine
- nozzle
- inches
- range
- 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- Withdrawn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
- 239000007789 gas Substances 0.000 description 14
- 238000000576 coating method Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 239000011248 coating agent Substances 0.000 description 2
- 230000003993 interaction Effects 0.000 description 2
- 239000000567 combustion gas Substances 0.000 description 1
- 230000001010 compromised effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000010348 incorporation Methods 0.000 description 1
- 238000005259 measurement Methods 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
- F01D5/142—Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
-
- 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
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 |
|---|---|---|---|
| US10/630,750 US6866477B2 (en) | 2003-07-31 | 2003-07-31 | Airfoil shape for a turbine nozzle |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JP2005054791A true JP2005054791A (ja) | 2005-03-03 |
| JP2005054791A5 JP2005054791A5 (enExample) | 2007-09-13 |
Family
ID=33541501
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2004223008A Withdrawn JP2005054791A (ja) | 2003-07-31 | 2004-07-30 | タービンノズル用の翼形形状 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US6866477B2 (enExample) |
| EP (1) | EP1503037A3 (enExample) |
| JP (1) | JP2005054791A (enExample) |
| CN (1) | CN100379942C (enExample) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2009036209A (ja) * | 2007-08-02 | 2009-02-19 | General Electric Co <Ge> | タービンバケット用の翼形及びそれを組込んだタービン |
| JP2021534344A (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2段タービンノズル |
Families Citing this family (37)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7001147B1 (en) * | 2004-07-28 | 2006-02-21 | General Electric Company | Airfoil shape and sidewall flowpath surfaces for a turbine nozzle |
| 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 |
| US7329093B2 (en) * | 2006-01-27 | 2008-02-12 | General Electric Company | Nozzle blade airfoil profile for a turbine |
| US7329092B2 (en) * | 2006-01-27 | 2008-02-12 | General Electric Company | Stator blade airfoil profile for a compressor |
| 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 |
| 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 |
| US7572104B2 (en) * | 2006-10-25 | 2009-08-11 | General Electric Company | Airfoil shape for a compressor |
| US7513748B2 (en) * | 2006-10-25 | 2009-04-07 | General Electric Company | Airfoil shape for a compressor |
| US7566202B2 (en) * | 2006-10-25 | 2009-07-28 | General Electric Company | Airfoil shape for a compressor |
| US7572105B2 (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 |
| US7695242B2 (en) * | 2006-12-05 | 2010-04-13 | Fuller Howard J | Wind turbine for generation of electric power |
| WO2010071499A1 (en) * | 2008-12-19 | 2010-06-24 | Volvo Aero Corporation | Spoke for a stator component, stator component and method for manufacturing a stator component |
| US8133016B2 (en) * | 2009-01-02 | 2012-03-13 | General Electric Company | Airfoil profile for a second stage turbine nozzle |
| US8573945B2 (en) * | 2009-11-13 | 2013-11-05 | Alstom Technology Ltd. | Compressor stator vane |
| US8757968B2 (en) * | 2010-07-26 | 2014-06-24 | Snecma | Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the third stage of a turbine |
| US8602740B2 (en) | 2010-09-08 | 2013-12-10 | United Technologies Corporation | Turbine vane airfoil |
| US8393870B2 (en) | 2010-09-08 | 2013-03-12 | United Technologies Corporation | Turbine blade airfoil |
| US8814510B2 (en) * | 2010-12-21 | 2014-08-26 | Hamilton Sundstrand Corporation | Turbine nozzle for air cycle machine |
| US8814511B2 (en) | 2011-08-09 | 2014-08-26 | General Electric Company | Turbomachine component having an airfoil core shape |
| US8876485B2 (en) * | 2011-11-28 | 2014-11-04 | General Electric Company | Turbine nozzle airfoil profile |
| US8734116B2 (en) * | 2011-11-28 | 2014-05-27 | General Electric Company | Turbine bucket airfoil profile |
| US8807950B2 (en) * | 2011-11-28 | 2014-08-19 | General Electric Company | Turbine nozzle airfoil profile |
| US8821125B2 (en) * | 2012-02-06 | 2014-09-02 | Alstom Technology Ltd. | Turbine blade having improved flutter capability and increased turbine stage output |
| US10443392B2 (en) * | 2016-07-13 | 2019-10-15 | Safran Aircraft Engines | Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the second stage of a turbine |
| US10443393B2 (en) * | 2016-07-13 | 2019-10-15 | Safran Aircraft Engines | Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the seventh stage of a turbine |
| US10443389B2 (en) * | 2017-11-09 | 2019-10-15 | Douglas James Dietrich | Turbine blade having improved flutter capability and increased turbine stage output |
| US10837298B2 (en) * | 2018-08-21 | 2020-11-17 | Chromalloy Gas Turbine Llc | First stage turbine nozzle |
Family Cites Families (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5980209A (en) * | 1997-06-27 | 1999-11-09 | General Electric Co. | Turbine blade with enhanced cooling and profile optimization |
| GB0003676D0 (en) * | 2000-02-17 | 2000-04-05 | Abb Alstom Power Nv | Aerofoils |
| US6461110B1 (en) * | 2001-07-11 | 2002-10-08 | General Electric Company | First-stage high pressure turbine bucket airfoil |
| US6450770B1 (en) * | 2001-06-28 | 2002-09-17 | General Electric Company | Second-stage turbine bucket airfoil |
| 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 |
| 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 |
| US6722853B1 (en) * | 2002-11-22 | 2004-04-20 | General Electric Company | Airfoil shape for a turbine nozzle |
| US6736599B1 (en) * | 2003-05-14 | 2004-05-18 | General Electric Company | First stage turbine nozzle airfoil |
-
2003
- 2003-07-31 US US10/630,750 patent/US6866477B2/en not_active Expired - Lifetime
-
2004
- 2004-07-27 EP EP04254487A patent/EP1503037A3/en not_active Withdrawn
- 2004-07-30 CN CNB2004100587591A patent/CN100379942C/zh not_active Expired - Fee Related
- 2004-07-30 JP JP2004223008A patent/JP2005054791A/ja not_active Withdrawn
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2009036209A (ja) * | 2007-08-02 | 2009-02-19 | General Electric Co <Ge> | タービンバケット用の翼形及びそれを組込んだタービン |
| JP2021534344A (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2段タービンノズル |
| JP7399154B2 (ja) | 2018-08-21 | 2023-12-15 | クロマロイ ガス タービン エルエルシー | 改善された第2段タービンノズル |
Also Published As
| Publication number | Publication date |
|---|---|
| EP1503037A2 (en) | 2005-02-02 |
| EP1503037A3 (en) | 2012-04-18 |
| US20050025618A1 (en) | 2005-02-03 |
| CN1580500A (zh) | 2005-02-16 |
| CN100379942C (zh) | 2008-04-09 |
| US6866477B2 (en) | 2005-03-15 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| A521 | Written amendment |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20070725 |
|
| A621 | Written request for application examination |
Free format text: JAPANESE INTERMEDIATE CODE: A621 Effective date: 20070725 |
|
| A761 | Written withdrawal of application |
Free format text: JAPANESE INTERMEDIATE CODE: A761 Effective date: 20090917 |