DE69816578D1 - Turbinenschaufel mit Kühlung der Hinterkantenwurzel - Google Patents

Turbinenschaufel mit Kühlung der Hinterkantenwurzel

Info

Publication number
DE69816578D1
DE69816578D1 DE69816578T DE69816578T DE69816578D1 DE 69816578 D1 DE69816578 D1 DE 69816578D1 DE 69816578 T DE69816578 T DE 69816578T DE 69816578 T DE69816578 T DE 69816578T DE 69816578 D1 DE69816578 D1 DE 69816578D1
Authority
DE
Germany
Prior art keywords
cooling
trailing edge
turbine blade
edge root
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.)
Expired - Lifetime
Application number
DE69816578T
Other languages
English (en)
Other versions
DE69816578T2 (de
Inventor
George P Liang
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 DE69816578D1 publication Critical patent/DE69816578D1/de
Application granted granted Critical
Publication of DE69816578T2 publication Critical patent/DE69816578T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • 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
    • F01D5/186—Film 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
    • F01D5/20—Specially-shaped blade tips to seal space between tips and stator
    • 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
    • F05D2240/80—Platforms for stationary or moving blades
    • F05D2240/81—Cooled platforms
    • 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
    • F05D2260/221—Improvement of heat transfer
    • F05D2260/2212—Improvement of heat transfer by creating turbulence

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE69816578T 1997-12-17 1998-12-04 Turbinenschaufel mit Kühlung der Hinterkantenwurzel Expired - Lifetime DE69816578T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/993,023 US5975851A (en) 1997-12-17 1997-12-17 Turbine blade with trailing edge root section cooling
US993023 1997-12-17

Publications (2)

Publication Number Publication Date
DE69816578D1 true DE69816578D1 (de) 2003-08-28
DE69816578T2 DE69816578T2 (de) 2004-06-03

Family

ID=25539011

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69816578T Expired - Lifetime DE69816578T2 (de) 1997-12-17 1998-12-04 Turbinenschaufel mit Kühlung der Hinterkantenwurzel

Country Status (5)

Country Link
US (1) US5975851A (de)
EP (1) EP0924383B1 (de)
JP (1) JPH11247607A (de)
KR (1) KR100569765B1 (de)
DE (1) DE69816578T2 (de)

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JP2000034902A (ja) * 1998-07-17 2000-02-02 Mitsubishi Heavy Ind Ltd ガスタービン冷却動翼
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US6179565B1 (en) * 1999-08-09 2001-01-30 United Technologies Corporation Coolable airfoil structure
DE19939179B4 (de) * 1999-08-20 2007-08-02 Alstom Kühlbare Schaufel für eine Gasturbine
DE19963349A1 (de) * 1999-12-27 2001-06-28 Abb Alstom Power Ch Ag Schaufel für Gasturbinen mit Drosselquerschnitt an Hinterkante
JP2001234703A (ja) * 2000-02-23 2001-08-31 Mitsubishi Heavy Ind Ltd ガスタービン動翼
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EP1245785B1 (de) * 2001-03-26 2005-06-01 Siemens Aktiengesellschaft Verfahren zur Herstellung einer Turbinenschaufel
US6561758B2 (en) * 2001-04-27 2003-05-13 General Electric Company Methods and systems for cooling gas turbine engine airfoils
US6514037B1 (en) 2001-09-26 2003-02-04 General Electric Company Method for reducing cooled turbine element stress and element made thereby
US6599092B1 (en) * 2002-01-04 2003-07-29 General Electric Company Methods and apparatus for cooling gas turbine nozzles
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US7156619B2 (en) * 2004-12-21 2007-01-02 Pratt & Whitney Canada Corp. Internally cooled gas turbine airfoil and method
US7156620B2 (en) * 2004-12-21 2007-01-02 Pratt & Whitney Canada Corp. Internally cooled gas turbine airfoil and method
US7270515B2 (en) * 2005-05-26 2007-09-18 Siemens Power Generation, Inc. Turbine airfoil trailing edge cooling system with segmented impingement ribs
US7334992B2 (en) * 2005-05-31 2008-02-26 United Technologies Corporation Turbine blade cooling system
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US7780413B2 (en) * 2006-08-01 2010-08-24 Siemens Energy, Inc. Turbine airfoil with near wall inflow chambers
US7713027B2 (en) * 2006-08-28 2010-05-11 United Technologies Corporation Turbine blade with split impingement rib
US7625178B2 (en) * 2006-08-30 2009-12-01 Honeywell International Inc. High effectiveness cooled turbine blade
US20080085193A1 (en) * 2006-10-05 2008-04-10 Siemens Power Generation, Inc. Turbine airfoil cooling system with enhanced tip corner cooling channel
US7597540B1 (en) 2006-10-06 2009-10-06 Florida Turbine Technologies, Inc. Turbine blade with showerhead film cooling holes
US7607891B2 (en) * 2006-10-23 2009-10-27 United Technologies Corporation Turbine component with tip flagged pedestal cooling
US7780414B1 (en) 2007-01-17 2010-08-24 Florida Turbine Technologies, Inc. Turbine blade with multiple metering trailing edge cooling holes
US7914257B1 (en) 2007-01-17 2011-03-29 Florida Turbine Technologies, Inc. Turbine rotor blade with spiral and serpentine flow cooling circuit
US7670113B1 (en) 2007-05-31 2010-03-02 Florida Turbine Technologies, Inc. Turbine airfoil with serpentine trailing edge cooling circuit
US7806659B1 (en) 2007-07-10 2010-10-05 Florida Turbine Technologies, Inc. Turbine blade with trailing edge bleed slot arrangement
US7815414B2 (en) * 2007-07-27 2010-10-19 United Technologies Corporation Airfoil mini-core plugging devices
US7946816B2 (en) * 2008-01-10 2011-05-24 General Electric Company Turbine blade tip shroud
GB0815271D0 (en) * 2008-08-22 2008-09-24 Rolls Royce Plc A blade
US9630277B2 (en) * 2010-03-15 2017-04-25 Siemens Energy, Inc. Airfoil having built-up surface with embedded cooling passage
GB201105105D0 (en) * 2011-03-28 2011-05-11 Rolls Royce Plc Gas turbine engine component
US8628298B1 (en) * 2011-07-22 2014-01-14 Florida Turbine Technologies, Inc. Turbine rotor blade with serpentine cooling
US8882448B2 (en) 2011-09-09 2014-11-11 Siemens Aktiengesellshaft Cooling system in a turbine airfoil assembly including zigzag cooling passages interconnected with radial passageways
US8840363B2 (en) 2011-09-09 2014-09-23 Siemens Energy, Inc. Trailing edge cooling system in a turbine airfoil assembly
US8376705B1 (en) 2011-09-09 2013-02-19 Siemens Energy, Inc. Turbine endwall with grooved recess cavity
US8858176B1 (en) * 2011-12-13 2014-10-14 Florida Turbine Technologies, Inc. Turbine airfoil with leading edge cooling
US9051842B2 (en) * 2012-01-05 2015-06-09 General Electric Company System and method for cooling turbine blades
US10100645B2 (en) * 2012-08-13 2018-10-16 United Technologies Corporation Trailing edge cooling configuration for a gas turbine engine airfoil
WO2014116475A1 (en) 2013-01-23 2014-07-31 United Technologies Corporation Gas turbine engine component having contoured rib end
US9932837B2 (en) * 2013-03-11 2018-04-03 United Technologies Corporation Low pressure loss cooled blade
US8985949B2 (en) 2013-04-29 2015-03-24 Siemens Aktiengesellschaft Cooling system including wavy cooling chamber in a trailing edge portion of an airfoil assembly
EP3039247B1 (de) 2013-08-28 2020-09-30 United Technologies Corporation Kühlanordnung mit einer übergangs- und sockelrippe für eine gasturbinenmotorschaufel
FR3030333B1 (fr) * 2014-12-17 2017-01-20 Snecma Procede de fabrication d'une aube de turbomachine comportant un sommet pourvu d'une baignoire de type complexe
RU2586231C1 (ru) * 2015-03-13 2016-06-10 Открытое акционерное общество "Авиадвигатель" Охлаждаемая лопатка высокотемпературной турбины
US11021967B2 (en) * 2017-04-03 2021-06-01 General Electric Company Turbine engine component with a core tie hole
RU2647351C1 (ru) * 2017-05-03 2018-03-15 федеральное государственное бюджетное образовательное учреждение высшего образования "Национальный исследовательский университет "МЭИ" (ФГБОУ ВО "НИУ "МЭИ") Охлаждаемая лопатка газовой турбины
US11002138B2 (en) 2017-12-13 2021-05-11 Solar Turbines Incorporated Turbine blade cooling system with lower turning vane bank
US10655476B2 (en) * 2017-12-14 2020-05-19 Honeywell International Inc. Gas turbine engines with airfoils having improved dust tolerance
KR102161765B1 (ko) * 2019-02-22 2020-10-05 두산중공업 주식회사 터빈용 에어포일, 이를 포함하는 터빈
RU191925U1 (ru) * 2019-03-18 2019-08-28 Публичное Акционерное Общество "Одк-Сатурн" Охлаждаемая сопловая лопатка с вихревой матрицей высокотемпературной турбины

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Also Published As

Publication number Publication date
KR19990063132A (ko) 1999-07-26
US5975851A (en) 1999-11-02
DE69816578T2 (de) 2004-06-03
KR100569765B1 (ko) 2006-07-19
JPH11247607A (ja) 1999-09-14
EP0924383B1 (de) 2003-07-23
EP0924383A3 (de) 2000-01-12
EP0924383A2 (de) 1999-06-23

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Legal Events

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8364 No opposition during term of opposition