JP3997575B2 - 翼 - Google Patents
翼 Download PDFInfo
- Publication number
- JP3997575B2 JP3997575B2 JP31254797A JP31254797A JP3997575B2 JP 3997575 B2 JP3997575 B2 JP 3997575B2 JP 31254797 A JP31254797 A JP 31254797A JP 31254797 A JP31254797 A JP 31254797A JP 3997575 B2 JP3997575 B2 JP 3997575B2
- Authority
- JP
- Japan
- Prior art keywords
- fillet
- pressure
- suction side
- wing
- passage
- 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 description 15
- 230000001154 acute effect Effects 0.000 description 13
- 230000008901 benefit Effects 0.000 description 4
- 239000000919 ceramic Substances 0.000 description 4
- 238000000926 separation method Methods 0.000 description 3
- 230000005856 abnormality Effects 0.000 description 2
- 238000005266 casting Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 241000270295 Serpentes Species 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000005495 investment casting Methods 0.000 description 1
- 239000011800 void material Substances 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
- F01D5/18—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
- 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)
- 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 |
|---|---|---|---|
| US08/713,321 | 1996-09-13 | ||
| US08/713,321 US5716192A (en) | 1996-09-13 | 1996-09-13 | Cooling duct turn geometry for bowed airfoil |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JPH10148104A JPH10148104A (ja) | 1998-06-02 |
| JPH10148104A5 JPH10148104A5 (2) | 2005-06-09 |
| JP3997575B2 true JP3997575B2 (ja) | 2007-10-24 |
Family
ID=24865681
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP31254797A Expired - Fee Related JP3997575B2 (ja) | 1996-09-13 | 1997-09-12 | 翼 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US5716192A (2) |
| EP (1) | EP0829619B1 (2) |
| JP (1) | JP3997575B2 (2) |
| KR (1) | KR100486055B1 (2) |
| DE (1) | DE69726519T2 (2) |
Families Citing this family (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH10184304A (ja) * | 1996-12-27 | 1998-07-14 | Toshiba Corp | 軸流タービンのタービンノズルおよびタービン動翼 |
| US6299412B1 (en) * | 1999-12-06 | 2001-10-09 | General Electric Company | Bowed compressor airfoil |
| DE50106970D1 (de) * | 2001-04-04 | 2005-09-08 | Siemens Ag | Turbinenschaufel und Turbine |
| US6589010B2 (en) * | 2001-08-27 | 2003-07-08 | General Electric Company | Method for controlling coolant flow in airfoil, flow control structure and airfoil incorporating the same |
| US7137782B2 (en) * | 2004-04-27 | 2006-11-21 | General Electric Company | Turbulator on the underside of a turbine blade tip turn and related method |
| GB0704426D0 (en) * | 2007-03-08 | 2007-04-18 | Rolls Royce Plc | Aerofoil members for a turbomachine |
| US8202054B2 (en) * | 2007-05-18 | 2012-06-19 | Siemens Energy, Inc. | Blade for a gas turbine engine |
| US10156143B2 (en) * | 2007-12-06 | 2018-12-18 | United Technologies Corporation | Gas turbine engines and related systems involving air-cooled vanes |
| EP2096261A1 (de) * | 2008-02-28 | 2009-09-02 | Siemens Aktiengesellschaft | Turbinenschaufel für eine stationäre Gasturbine |
| EP2257399A1 (de) * | 2008-03-31 | 2010-12-08 | ALSTOM Technology Ltd | Schaufel für eine gasturbine |
| WO2009150019A1 (de) | 2008-06-12 | 2009-12-17 | Alstom Technology Ltd. | Schaufel für eine gasturbine sowie verfahren zum gusstechnischen herstellen einer solchen schaufel |
| US9550267B2 (en) * | 2013-03-15 | 2017-01-24 | United Technologies Corporation | Tool for abrasive flow machining of airfoil clusters |
| US9695696B2 (en) * | 2013-07-31 | 2017-07-04 | General Electric Company | Turbine blade with sectioned pins |
| JP6203423B2 (ja) * | 2014-03-05 | 2017-09-27 | シーメンス アクチエンゲゼルシヤフトSiemens Aktiengesellschaft | 弓形ベーン用のタービン翼冷却システム |
| KR101901682B1 (ko) * | 2017-06-20 | 2018-09-27 | 두산중공업 주식회사 | 제이 타입 캔틸레버드 베인 및 이를 포함하는 가스터빈 |
| KR102048863B1 (ko) | 2018-04-17 | 2019-11-26 | 두산중공업 주식회사 | 인서트 지지부를 구비한 터빈 베인 |
| US11333171B2 (en) | 2018-11-27 | 2022-05-17 | Honeywell International Inc. | High performance wedge diffusers for compression systems |
| US10871170B2 (en) | 2018-11-27 | 2020-12-22 | Honeywell International Inc. | High performance wedge diffusers for compression systems |
| WO2022051760A1 (en) * | 2020-09-04 | 2022-03-10 | Siemens Energy Global GmbH & Co. KG | Guide vane in gas turbine engine |
| US11713679B1 (en) * | 2022-01-27 | 2023-08-01 | Raytheon Technologies Corporation | Tangentially bowed airfoil |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4257737A (en) * | 1978-07-10 | 1981-03-24 | United Technologies Corporation | Cooled rotor blade |
| US4826400A (en) * | 1986-12-29 | 1989-05-02 | General Electric Company | Curvilinear turbine airfoil |
| GB9014762D0 (en) * | 1990-07-03 | 1990-10-17 | Rolls Royce Plc | Cooled aerofoil vane |
| JP2684936B2 (ja) * | 1992-09-18 | 1997-12-03 | 株式会社日立製作所 | ガスタービン及びガスタービン翼 |
| US5525038A (en) * | 1994-11-04 | 1996-06-11 | United Technologies Corporation | Rotor airfoils to control tip leakage flows |
-
1996
- 1996-09-13 US US08/713,321 patent/US5716192A/en not_active Expired - Lifetime
-
1997
- 1997-09-09 DE DE69726519T patent/DE69726519T2/de not_active Expired - Lifetime
- 1997-09-09 EP EP97307032A patent/EP0829619B1/en not_active Expired - Lifetime
- 1997-09-12 KR KR1019970046984A patent/KR100486055B1/ko not_active Expired - Fee Related
- 1997-09-12 JP JP31254797A patent/JP3997575B2/ja not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| EP0829619A1 (en) | 1998-03-18 |
| EP0829619B1 (en) | 2003-12-03 |
| KR19980024573A (ko) | 1998-07-06 |
| JPH10148104A (ja) | 1998-06-02 |
| DE69726519T2 (de) | 2004-07-22 |
| DE69726519D1 (de) | 2004-01-15 |
| US5716192A (en) | 1998-02-10 |
| KR100486055B1 (ko) | 2005-06-16 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| A521 | Request for written amendment filed |
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| A621 | Written request for application examination |
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| A977 | Report on retrieval |
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| TRDD | Decision of grant or rejection written | ||
| A01 | Written decision to grant a patent or to grant a registration (utility model) |
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| A61 | First payment of annual fees (during grant procedure) |
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| R150 | Certificate of patent or registration of utility model |
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| FPAY | Renewal fee payment (event date is renewal date of database) |
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| LAPS | Cancellation because of no payment of annual fees |