EP1605138A3 - Aube de rotor refroidie ayant un refroidissement par impact au niveau du bord d'attaque - Google Patents

Aube de rotor refroidie ayant un refroidissement par impact au niveau du bord d'attaque Download PDF

Info

Publication number
EP1605138A3
EP1605138A3 EP05253261A EP05253261A EP1605138A3 EP 1605138 A3 EP1605138 A3 EP 1605138A3 EP 05253261 A EP05253261 A EP 05253261A EP 05253261 A EP05253261 A EP 05253261A EP 1605138 A3 EP1605138 A3 EP 1605138A3
Authority
EP
European Patent Office
Prior art keywords
radial passage
rib
rotor blade
leading edge
root
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.)
Granted
Application number
EP05253261A
Other languages
German (de)
English (en)
Other versions
EP1605138A2 (fr
EP1605138B1 (fr
Inventor
Jeffrey R. Levine
Edward Pietraszkiewicz
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by United Technologies Corp filed Critical United Technologies Corp
Publication of EP1605138A2 publication Critical patent/EP1605138A2/fr
Publication of EP1605138A3 publication Critical patent/EP1605138A3/fr
Application granted granted Critical
Publication of EP1605138B1 publication Critical patent/EP1605138B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/201—Heat transfer, e.g. cooling by impingement of a fluid
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
EP05253261A 2004-05-27 2005-05-27 Aube de rotor refroidie ayant un refroidissement par impact au niveau du bord d'attaque Active EP1605138B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US855076 1992-03-23
US10/855,076 US20050265840A1 (en) 2004-05-27 2004-05-27 Cooled rotor blade with leading edge impingement cooling

Publications (3)

Publication Number Publication Date
EP1605138A2 EP1605138A2 (fr) 2005-12-14
EP1605138A3 true EP1605138A3 (fr) 2007-10-03
EP1605138B1 EP1605138B1 (fr) 2010-06-30

Family

ID=34941473

Family Applications (1)

Application Number Title Priority Date Filing Date
EP05253261A Active EP1605138B1 (fr) 2004-05-27 2005-05-27 Aube de rotor refroidie ayant un refroidissement par impact au niveau du bord d'attaque

Country Status (4)

Country Link
US (1) US20050265840A1 (fr)
EP (1) EP1605138B1 (fr)
JP (1) JP2005337257A (fr)
DE (1) DE602005022018D1 (fr)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7217094B2 (en) * 2004-10-18 2007-05-15 United Technologies Corporation Airfoil with large fillet and micro-circuit cooling
FR2918105B1 (fr) * 2007-06-27 2013-12-27 Snecma Aube refroidie de turbomachine comprenant des trous de refroidissement a distance d'impact variable.
US8840370B2 (en) 2011-11-04 2014-09-23 General Electric Company Bucket assembly for turbine system
JP2013100765A (ja) * 2011-11-08 2013-05-23 Ihi Corp インピンジ冷却機構、タービン翼及び燃焼器
US9151173B2 (en) * 2011-12-15 2015-10-06 General Electric Company Use of multi-faceted impingement openings for increasing heat transfer characteristics on gas turbine components
JP6169161B2 (ja) * 2012-03-22 2017-07-26 ゼネラル エレクトリック テクノロジー ゲゼルシャフト ミット ベシュレンクテル ハフツングＧｅｎｅｒａｌ Ｅｌｅｃｔｒｉｃ Ｔｅｃｈｎｏｌｏｇｙ ＧｍｂＨ タービン翼
US9279331B2 (en) * 2012-04-23 2016-03-08 United Technologies Corporation Gas turbine engine airfoil with dirt purge feature and core for making same
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
US10012090B2 (en) * 2014-07-25 2018-07-03 United Technologies Corporation Airfoil cooling apparatus
CN107109949A (zh) * 2014-11-11 2017-08-29 西门子公司 带有轴向叶顶冷却回路的涡轮叶片
KR101906701B1 (ko) * 2017-01-03 2018-10-10 두산중공업 주식회사 가스터빈 블레이드
US10787932B2 (en) * 2018-07-13 2020-09-29 Honeywell International Inc. Turbine blade with dust tolerant cooling system
US10895168B2 (en) 2019-05-30 2021-01-19 Solar Turbines Incorporated Turbine blade with serpentine channels

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5688104A (en) * 1993-11-24 1997-11-18 United Technologies Corporation Airfoil having expanded wall portions to accommodate film cooling holes
EP1022434A2 (fr) * 1999-01-25 2000-07-26 General Electric Company Configuration de refroidissement des aubes de turbine à gaz
EP1035302A2 (fr) * 1999-03-05 2000-09-13 General Electric Company Aube de turbomachine refroidie par impact multiple de jet d'air
EP1088964A2 (fr) * 1999-09-30 2001-04-04 General Electric Company Fente pour le refroidissement par impact du bord d'attaque d'une aube pour une turbomachine
EP1213442A1 (fr) * 2000-12-05 2002-06-12 United Technologies Corporation Structure d'aube refroidissable
US20030044277A1 (en) * 2001-08-28 2003-03-06 Snecma Moteurs Gas turbine blade cooling circuits
EP1496203A1 (fr) * 2003-07-11 2005-01-12 Rolls-Royce Deutschland Ltd & Co KG Aube de turbine à gaz avec refroidissement par impact

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3619082A (en) * 1968-07-05 1971-11-09 Gen Motors Corp Turbine blade
US3767322A (en) * 1971-07-30 1973-10-23 Westinghouse Electric Corp Internal cooling for turbine vanes
US5387086A (en) * 1993-07-19 1995-02-07 General Electric Company Gas turbine blade with improved cooling

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5688104A (en) * 1993-11-24 1997-11-18 United Technologies Corporation Airfoil having expanded wall portions to accommodate film cooling holes
EP1022434A2 (fr) * 1999-01-25 2000-07-26 General Electric Company Configuration de refroidissement des aubes de turbine à gaz
EP1035302A2 (fr) * 1999-03-05 2000-09-13 General Electric Company Aube de turbomachine refroidie par impact multiple de jet d'air
EP1088964A2 (fr) * 1999-09-30 2001-04-04 General Electric Company Fente pour le refroidissement par impact du bord d'attaque d'une aube pour une turbomachine
EP1213442A1 (fr) * 2000-12-05 2002-06-12 United Technologies Corporation Structure d'aube refroidissable
US20030044277A1 (en) * 2001-08-28 2003-03-06 Snecma Moteurs Gas turbine blade cooling circuits
EP1496203A1 (fr) * 2003-07-11 2005-01-12 Rolls-Royce Deutschland Ltd & Co KG Aube de turbine à gaz avec refroidissement par impact

Also Published As

Publication number Publication date
DE602005022018D1 (de) 2010-08-12
EP1605138A2 (fr) 2005-12-14
US20050265840A1 (en) 2005-12-01
EP1605138B1 (fr) 2010-06-30
JP2005337257A (ja) 2005-12-08

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