JP2004176723A - 長短の翼弦長と高低の高温性能と有するタービン翼形部列 - Google Patents
長短の翼弦長と高低の高温性能と有するタービン翼形部列 Download PDFInfo
- Publication number
- JP2004176723A JP2004176723A JP2003396596A JP2003396596A JP2004176723A JP 2004176723 A JP2004176723 A JP 2004176723A JP 2003396596 A JP2003396596 A JP 2003396596A JP 2003396596 A JP2003396596 A JP 2003396596A JP 2004176723 A JP2004176723 A JP 2004176723A
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- JP
- Japan
- Prior art keywords
- airfoils
- airfoil
- turbine
- chord length
- temperature performance
- 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.)
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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
-
- 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
- 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
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/12—Fluid guiding means, e.g. vanes
-
- 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
- F05D2250/30—Arrangement of components
- F05D2250/34—Arrangement of components translated
-
- 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
Abstract
【解決手段】 ガスタービンエンジンタービン段(19)は、第1翼弦長(CL1)を有する第1の複数(41)の第1翼形部(44)と該第1翼弦長より短い第2翼弦長(CL2)を有する第2の複数(43)の第2翼形部(46)とを含む、タービン翼形部(22)の環状列を有する。第2翼形部の少なくとも1つは、円周方向に第1翼形部の隣接する各対(66)の間に配置される。第2翼形部の第2前縁(47)は、第1翼形部の第1前縁(53)から下流に位置する。第1及び第2翼形部は、それぞれ異なる第1及び第2の高温性能を有しており、該第1の高温性能は、該第2の高温性能より高い。第1及び第2翼形部は、異なる合金から作られることができ、第2翼形部は、第1翼形部より少ない冷却空気流量を用いるように構成されることができる。
【選択図】 図1
Description
10 ガスタービンエンジン
12 多段式軸流圧縮機
14 燃焼器
16 2段式高圧タービン
18 空気
19 高圧タービンの第1段
20 高温燃焼ガス
21 高圧タービンの第2段
22 タービン翼形部
23 第1ノズル
27 第1ロータ段
28 高温ガス流路
29 ロータブレード
33 第2ノズル
35 第2ベーン列
37 第2ロータ段
39 第2ロータブレード列
42 フィルム冷却孔
51 下流方向
Claims (10)
- タービン翼形部(22)の環状列と、
第1翼弦長(CL1)を有する第1の複数(41)の第1翼形部(44)と、
前記第1翼弦長より短い第2翼弦長(CL2)を有する第2の複数(43)の第2翼形部(46)と、を含み、
前記第2翼形部の少なくとも1つが、円周方向に前記第1翼形部の各隣接対(66)の間に配置され、
前記第2翼形部の第2前縁(47)が、前記第1翼形部の第1前縁(53)から下流に位置し、
前記第1及び第2翼形部が、それぞれ異なる第1及び第2の高温性能を有しており、前記第1の高温性能が、前記第2の高温性能より高い、
ことを特徴とするガスタービンエンジンタービン段(19)組立体。 - 前記第1及び第2翼形部が、異なる合金から作られていることを特徴とする、請求項1に記載の組立体。
- 前記第2翼形部が、前記第1翼形部より少ない冷却空気流量を用いるように構成されていることを特徴とする、請求項1に記載の組立体。
- 前記第1及び第2翼形部が、異なる合金から作られ、前記第2翼形部が、前記第1翼形部より少ない冷却空気流量を用いるように構成されていることを特徴とする、請求項1に記載の組立体。
- 円周方向に前記第1翼形部の各隣接対(66)の間に配置された、前記第2翼形部の1つ又はそれ以上を更に含み、
前記第2翼形部の第2前縁(47)が、前記第1翼形部の第1前縁(53)から下流に位置し、
前記第1及び第2翼形部が、それぞれ異なる第1及び第2の高温性能を有しており、前記第1の高温性能が、前記第2の高温性能より高い、
ことを特徴とする、請求項1に記載の組立体。 - 前記第1及び第2翼形部が、異なる合金から作られていることを特徴とする、請求項5に記載の組立体。
- 前記第2翼形部が、前記第1翼形部より少ない冷却空気流量を用いるように構成されていることを特徴とする、請求項5に記載の組立体。
- 前記第1及び第2翼形部が、異なる合金から作られ、前記第2翼形部が、前記第1翼形部より少ない冷却空気流量を用いるように構成されていることを特徴とする、請求項5に記載の組立体。
- タービン翼形部(22)の、軸方向に隣接する環状の上流列(34)及び下流列(36)を含み、
前記タービン翼形部(22)の環状の下流列(36)が、第1翼弦長(CL1)を有する第1の複数(41)の第1翼形部(44)と前記第1翼弦長より短い第2翼弦長(CL2)を有する第2の複数(43)の第2翼形部(46)とを含み、
前記第2翼形部の各々の少なくとも1つが、円周方向に前記第1翼形部の各隣接対(66)の間に配置され、
前記第2翼形部の第2前縁(47)が、前記第1翼形部の第1前縁(53)から下流に位置し、
前記第1及び第2翼形部が、それぞれ異なる第1及び第2の高温性能を有しており、前記第1の高温性能が、前記第2の高温性能より高い、
ことを特徴とするガスタービンエンジンタービン段(19)組立体。 - 前記第1及び第2翼形部が、異なる合金から作られていることを特徴とする、請求項9に記載の組立体。
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/305,833 US7094027B2 (en) | 2002-11-27 | 2002-11-27 | Row of long and short chord length and high and low temperature capability turbine airfoils |
Publications (3)
Publication Number | Publication Date |
---|---|
JP2004176723A true JP2004176723A (ja) | 2004-06-24 |
JP2004176723A5 JP2004176723A5 (ja) | 2007-01-18 |
JP4366178B2 JP4366178B2 (ja) | 2009-11-18 |
Family
ID=32298066
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2003396596A Expired - Fee Related JP4366178B2 (ja) | 2002-11-27 | 2003-11-27 | 長短の翼弦長と高低の高温性能と有するタービン翼形部列 |
Country Status (4)
Country | Link |
---|---|
US (1) | US7094027B2 (ja) |
EP (1) | EP1424467A3 (ja) |
JP (1) | JP4366178B2 (ja) |
CA (1) | CA2449263C (ja) |
Cited By (6)
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JP2006029190A (ja) * | 2004-07-15 | 2006-02-02 | Mitsubishi Heavy Ind Ltd | ガスタービンにおける高温部品の寿命診断方法 |
JP2007170375A (ja) * | 2005-12-19 | 2007-07-05 | General Electric Co <Ge> | 逆冷却タービンノズル |
JP2008175207A (ja) * | 2007-01-18 | 2008-07-31 | Siemens Ag | 静翼を備えたガスタービン |
JP2010209911A (ja) * | 2009-03-10 | 2010-09-24 | General Electric Co <Ge> | ガスタービンエンジン温度管理の方法及び装置 |
JP2014020372A (ja) * | 2012-07-11 | 2014-02-03 | Alstom Technology Ltd | 軸流タービン用の固定ベーンアッセンブリ |
JP2017141822A (ja) * | 2016-02-12 | 2017-08-17 | ゼネラル・エレクトリック・カンパニイ | 流路の輪郭形成 |
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DE102004036594A1 (de) * | 2004-07-28 | 2006-03-23 | Mtu Aero Engines Gmbh | Strömungsstruktur für eine Gasturbine |
US7588413B2 (en) * | 2006-11-30 | 2009-09-15 | General Electric Company | Upstream plasma shielded film cooling |
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- 2003-11-13 CA CA2449263A patent/CA2449263C/en not_active Expired - Fee Related
- 2003-11-26 EP EP03257438A patent/EP1424467A3/en not_active Withdrawn
- 2003-11-27 JP JP2003396596A patent/JP4366178B2/ja not_active Expired - Fee Related
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JP2008175207A (ja) * | 2007-01-18 | 2008-07-31 | Siemens Ag | 静翼を備えたガスタービン |
JP4607195B2 (ja) * | 2007-01-18 | 2011-01-05 | シーメンス アクチエンゲゼルシヤフト | 静翼を備えたガスタービン |
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JP2010209911A (ja) * | 2009-03-10 | 2010-09-24 | General Electric Co <Ge> | ガスタービンエンジン温度管理の方法及び装置 |
JP2014020372A (ja) * | 2012-07-11 | 2014-02-03 | Alstom Technology Ltd | 軸流タービン用の固定ベーンアッセンブリ |
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Also Published As
Publication number | Publication date |
---|---|
US7094027B2 (en) | 2006-08-22 |
CA2449263A1 (en) | 2004-05-27 |
JP4366178B2 (ja) | 2009-11-18 |
US20040101405A1 (en) | 2004-05-27 |
EP1424467A2 (en) | 2004-06-02 |
EP1424467A3 (en) | 2006-09-27 |
CA2449263C (en) | 2010-11-09 |
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