FR2893974B1 - Circuit de refroidissement central pour aube mobile de turbomachine - Google Patents
Circuit de refroidissement central pour aube mobile de turbomachineInfo
- Publication number
- FR2893974B1 FR2893974B1 FR0512003A FR0512003A FR2893974B1 FR 2893974 B1 FR2893974 B1 FR 2893974B1 FR 0512003 A FR0512003 A FR 0512003A FR 0512003 A FR0512003 A FR 0512003A FR 2893974 B1 FR2893974 B1 FR 2893974B1
- Authority
- FR
- France
- Prior art keywords
- cooling circuit
- turbine drive
- central cooling
- mobile turbine
- mobile
- 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.)
- Active
Links
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
- 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
- F05D2250/71—Shape curved
- F05D2250/711—Shape curved convex
-
- 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
- F05D2250/71—Shape curved
- F05D2250/712—Shape curved concave
-
- 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
-
- 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
- F05D2260/221—Improvement of heat transfer
- F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
- F05D2260/22141—Improvement of heat transfer by increasing the heat transfer surface using fins or ribs
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0512003A FR2893974B1 (fr) | 2005-11-28 | 2005-11-28 | Circuit de refroidissement central pour aube mobile de turbomachine |
EP06124041.2A EP1790819B1 (fr) | 2005-11-28 | 2006-11-14 | Aube mobile de turbomachine comprenant un circuit de refroidissement |
US11/562,726 US7661930B2 (en) | 2005-11-28 | 2006-11-22 | Central cooling circuit for a moving blade of a turbomachine |
JP2006316844A JP4823872B2 (ja) | 2005-11-28 | 2006-11-24 | ターボ機械の移動ブレードのための中央冷却回路 |
CA2569566A CA2569566C (fr) | 2005-11-28 | 2006-11-27 | Circuit de refroidissement central pour aube mobile de turbomachine |
RU2006141862/06A RU2421623C2 (ru) | 2005-11-28 | 2006-11-27 | Регулируемая лопатка турбореактивного двигателя, турбореактивный двигатель, газотурбинный двигатель |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0512003A FR2893974B1 (fr) | 2005-11-28 | 2005-11-28 | Circuit de refroidissement central pour aube mobile de turbomachine |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2893974A1 FR2893974A1 (fr) | 2007-06-01 |
FR2893974B1 true FR2893974B1 (fr) | 2011-03-18 |
Family
ID=36829580
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0512003A Active FR2893974B1 (fr) | 2005-11-28 | 2005-11-28 | Circuit de refroidissement central pour aube mobile de turbomachine |
Country Status (6)
Country | Link |
---|---|
US (1) | US7661930B2 (fr) |
EP (1) | EP1790819B1 (fr) |
JP (1) | JP4823872B2 (fr) |
CA (1) | CA2569566C (fr) |
FR (1) | FR2893974B1 (fr) |
RU (1) | RU2421623C2 (fr) |
Families Citing this family (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7862299B1 (en) * | 2007-03-21 | 2011-01-04 | Florida Turbine Technologies, Inc. | Two piece hollow turbine blade with serpentine cooling circuits |
US7985049B1 (en) * | 2007-07-20 | 2011-07-26 | Florida Turbine Technologies, Inc. | Turbine blade with impingement cooling |
WO2009016744A1 (fr) * | 2007-07-31 | 2009-02-05 | Mitsubishi Heavy Industries, Ltd. | Pale pour turbine |
US10156143B2 (en) * | 2007-12-06 | 2018-12-18 | United Technologies Corporation | Gas turbine engines and related systems involving air-cooled vanes |
JP5953136B2 (ja) * | 2012-06-15 | 2016-07-20 | 三菱日立パワーシステムズ株式会社 | ガスタービン動翼およびガスタービン、ガスタービン動翼の調整方法 |
KR101411347B1 (ko) | 2012-11-16 | 2014-06-27 | 연세대학교 산학협력단 | 회전 블레이드에서 냉각성능 향상을 위한 블레이드 내부 유로 구조 |
US9376922B2 (en) * | 2013-01-09 | 2016-06-28 | General Electric Company | Interior configuration for turbine rotor blade |
EP2941543B1 (fr) * | 2013-03-13 | 2017-03-22 | Rolls-Royce Corporation | Agencement de trou de refroidissement à tranchée pour une ailette composite à matrice céramique |
JP5567180B1 (ja) * | 2013-05-20 | 2014-08-06 | 川崎重工業株式会社 | タービン翼の冷却構造 |
GB201314222D0 (en) * | 2013-08-08 | 2013-09-25 | Rolls Royce Plc | Aerofoil |
FR3020402B1 (fr) * | 2014-04-24 | 2019-06-14 | Safran Aircraft Engines | Aube pour turbine de turbomachine comprenant un circuit de refroidissement a homogeneite amelioree |
CN106844839B (zh) * | 2016-12-14 | 2020-01-31 | 中国长江动力集团有限公司 | 用于优化汽轮机叶片型线的方法 |
US10724391B2 (en) * | 2017-04-07 | 2020-07-28 | General Electric Company | Engine component with flow enhancer |
FR3067388B1 (fr) * | 2017-04-10 | 2020-01-17 | Safran | Aube a circuit de refroidissement perfectionne |
GB201806821D0 (en) * | 2018-04-26 | 2018-06-13 | Rolls Royce Plc | Coolant channel |
FR3095834B1 (fr) * | 2019-05-09 | 2021-06-04 | Safran | Aube de turbomachine à refroidissement amélioré |
FR3097786B1 (fr) * | 2019-06-27 | 2021-06-04 | Safran | Procede de percage d'une aube de turbomachine en fonction de la geometrie interne de l'aube et aube associee |
CN112943380A (zh) * | 2021-02-04 | 2021-06-11 | 大连理工大学 | 一种采用丁字形隔墙的回转式冷却通道涡轮叶片 |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH06102963B2 (ja) * | 1983-12-22 | 1994-12-14 | 株式会社東芝 | ガスタ−ビン空冷翼 |
JPH0233843B2 (ja) * | 1984-03-23 | 1990-07-31 | Kogyo Gijutsuin | Gasutaabindoyokunoreikyakukozo |
US5165852A (en) * | 1990-12-18 | 1992-11-24 | General Electric Company | Rotation enhanced rotor blade cooling using a double row of coolant passageways |
JPH05195704A (ja) * | 1992-01-22 | 1993-08-03 | Hitachi Ltd | タービン翼及びガスタービン |
US5356265A (en) * | 1992-08-25 | 1994-10-18 | General Electric Company | Chordally bifurcated turbine blade |
US6402471B1 (en) * | 2000-11-03 | 2002-06-11 | General Electric Company | Turbine blade for gas turbine engine and method of cooling same |
FR2829175B1 (fr) * | 2001-08-28 | 2003-11-07 | Snecma Moteurs | Circuits de refroidissement pour aube de turbine a gaz |
US6981840B2 (en) * | 2003-10-24 | 2006-01-03 | General Electric Company | Converging pin cooled airfoil |
US7097426B2 (en) * | 2004-04-08 | 2006-08-29 | General Electric Company | Cascade impingement cooled airfoil |
US7217092B2 (en) * | 2004-04-14 | 2007-05-15 | General Electric Company | Method and apparatus for reducing turbine blade temperatures |
US7442008B2 (en) * | 2004-08-25 | 2008-10-28 | Rolls-Royce Plc | Cooled gas turbine aerofoil |
FR2887287B1 (fr) * | 2005-06-21 | 2007-09-21 | Snecma Moteurs Sa | Circuits de refroidissement pour aube mobile de turbomachine |
-
2005
- 2005-11-28 FR FR0512003A patent/FR2893974B1/fr active Active
-
2006
- 2006-11-14 EP EP06124041.2A patent/EP1790819B1/fr active Active
- 2006-11-22 US US11/562,726 patent/US7661930B2/en active Active
- 2006-11-24 JP JP2006316844A patent/JP4823872B2/ja active Active
- 2006-11-27 RU RU2006141862/06A patent/RU2421623C2/ru active
- 2006-11-27 CA CA2569566A patent/CA2569566C/fr active Active
Also Published As
Publication number | Publication date |
---|---|
RU2421623C2 (ru) | 2011-06-20 |
EP1790819A1 (fr) | 2007-05-30 |
CA2569566A1 (fr) | 2007-05-28 |
EP1790819B1 (fr) | 2017-06-21 |
CA2569566C (fr) | 2013-12-24 |
US7661930B2 (en) | 2010-02-16 |
US20070122282A1 (en) | 2007-05-31 |
RU2006141862A (ru) | 2008-06-10 |
FR2893974A1 (fr) | 2007-06-01 |
JP4823872B2 (ja) | 2011-11-24 |
JP2007146842A (ja) | 2007-06-14 |
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Legal Events
Date | Code | Title | Description |
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CL | Concession to grant licences | ||
PLFP | Fee payment |
Year of fee payment: 11 |
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PLFP | Fee payment |
Year of fee payment: 12 |
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PLFP | Fee payment |
Year of fee payment: 13 |
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CD | Change of name or company name |
Owner name: SNECMA, FR Effective date: 20170713 |
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PLFP | Fee payment |
Year of fee payment: 14 |
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PLFP | Fee payment |
Year of fee payment: 15 |
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PLFP | Fee payment |
Year of fee payment: 16 |
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PLFP | Fee payment |
Year of fee payment: 17 |
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PLFP | Fee payment |
Year of fee payment: 18 |
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PLFP | Fee payment |
Year of fee payment: 19 |