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DE60020007D1 - Internes Luftkühlungssystem für Turbinenschaufeln - Google Patents

Internes Luftkühlungssystem für Turbinenschaufeln

Info

Publication number
DE60020007D1
DE60020007D1 DE60020007T DE60020007T DE60020007D1 DE 60020007 D1 DE60020007 D1 DE 60020007D1 DE 60020007 T DE60020007 T DE 60020007T DE 60020007 T DE60020007 T DE 60020007T DE 60020007 D1 DE60020007 D1 DE 60020007D1
Authority
DE
Germany
Prior art keywords
cooling system
air cooling
turbine blades
internal air
turbine
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
DE60020007T
Other languages
English (en)
Other versions
DE60020007T2 (de
Inventor
Martin Anthony James Emery
Kevin Paul Self
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of DE60020007D1 publication Critical patent/DE60020007D1/de
Application granted granted Critical
Publication of DE60020007T2 publication Critical patent/DE60020007T2/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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/007—Preventing corrosion
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/32—Collecting of condensation water; Drainage ; Removing solid particles
    • 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
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187—Convection cooling
    • F01D5/188—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
    • F01D5/189—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall the insert having a tubular cross-section, e.g. airfoil shape
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/30—Preventing corrosion or unwanted deposits in gas-swept spaces
    • 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
    • F05D2260/60—Fluid transfer
    • F05D2260/607—Preventing clogging or obstruction of flow paths by dirt, dust, or foreign particles

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE60020007T 1999-06-09 2000-05-26 Internes Luftkühlungssystem für Turbinenschaufeln Expired - Lifetime DE60020007T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB9913393 1999-06-09
GB9913393A GB2350867B (en) 1999-06-09 1999-06-09 Gas turbine airfoil internal air system

Publications (2)

Publication Number Publication Date
DE60020007D1 true DE60020007D1 (de) 2005-06-16
DE60020007T2 DE60020007T2 (de) 2006-03-16

Family

ID=10855004

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60020007T Expired - Lifetime DE60020007T2 (de) 1999-06-09 2000-05-26 Internes Luftkühlungssystem für Turbinenschaufeln

Country Status (4)

Country Link
US (1) US6318963B1 (de)
EP (1) EP1059418B8 (de)
DE (1) DE60020007T2 (de)
GB (1) GB2350867B (de)

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GB2365932B (en) * 2000-08-18 2004-05-05 Rolls Royce Plc Vane assembly
GB2366600A (en) * 2000-09-09 2002-03-13 Rolls Royce Plc Cooling arrangement for trailing edge of aerofoil
DE50208671D1 (de) * 2001-07-13 2006-12-21 Alstom Technology Ltd Gasturbinenteil mit Kühlluftbohrung
US6652220B2 (en) * 2001-11-15 2003-11-25 General Electric Company Methods and apparatus for cooling gas turbine nozzles
WO2003080998A1 (de) * 2002-03-25 2003-10-02 Alstom Technology Ltd Gekühlte turbinenschaufel
US6969237B2 (en) * 2003-08-28 2005-11-29 United Technologies Corporation Turbine airfoil cooling flow particle separator
GB2441771B (en) * 2006-09-13 2009-07-08 Rolls Royce Plc Cooling arrangement for a component of a gas turbine engine
US7762784B2 (en) * 2007-01-11 2010-07-27 United Technologies Corporation Insertable impingement rib
US7857588B2 (en) * 2007-07-06 2010-12-28 United Technologies Corporation Reinforced airfoils
US10286407B2 (en) 2007-11-29 2019-05-14 General Electric Company Inertial separator
JP2009162119A (ja) * 2008-01-08 2009-07-23 Ihi Corp タービン翼の冷却構造
US20100054915A1 (en) * 2008-08-28 2010-03-04 United Technologies Corporation Airfoil insert
US8157525B2 (en) * 2008-11-20 2012-04-17 General Electric Company Methods and apparatus relating to turbine airfoil cooling apertures
US8109724B2 (en) 2009-03-26 2012-02-07 United Technologies Corporation Recessed metering standoffs for airfoil baffle
US8079821B2 (en) * 2009-05-05 2011-12-20 Siemens Energy, Inc. Turbine airfoil with dual wall formed from inner and outer layers separated by a compliant structure
JP5675081B2 (ja) * 2009-11-25 2015-02-25 三菱重工業株式会社 翼体及びこの翼体を備えたガスタービン
US8449249B2 (en) * 2010-04-09 2013-05-28 Williams International Co., L.L.C. Turbine nozzle apparatus and associated method of manufacture
EP2392775A1 (de) * 2010-06-07 2011-12-07 Siemens Aktiengesellschaft Rotationsschaufel zur Verwendung in einem Fluidstrom einer Turbine und zugehörige Turbine
GB201103317D0 (de) 2011-02-28 2011-04-13 Rolls Royce Plc
EP2573325A1 (de) * 2011-09-23 2013-03-27 Siemens Aktiengesellschaft Aufprallkühlung von Turbinenschaufeln oder -flügeln
US9127560B2 (en) 2011-12-01 2015-09-08 General Electric Company Cooled turbine blade and method for cooling a turbine blade
US20140093392A1 (en) * 2012-10-03 2014-04-03 Rolls-Royce Plc Gas turbine engine component
WO2014133721A1 (en) * 2013-02-27 2014-09-04 United Technologies Corporation Gas turbine engine thin wall composite vane airfoil
EP2921649B1 (de) * 2014-03-19 2021-04-28 Ansaldo Energia IP UK Limited Blattprofilabschnitt eines Rotorblattes oder einer Leitschaufel einer Turbomaschine
FR3021698B1 (fr) * 2014-05-28 2021-07-02 Snecma Aube de turbine, comprenant un conduit central de refroidissement isole thermiquement de parois de l'aube par deux cavites laterales jointives en aval du conduit central
US11033845B2 (en) 2014-05-29 2021-06-15 General Electric Company Turbine engine and particle separators therefore
US9915176B2 (en) 2014-05-29 2018-03-13 General Electric Company Shroud assembly for turbine engine
WO2016025056A2 (en) 2014-05-29 2016-02-18 General Electric Company Turbine engine and particle separators therefore
EP3149310A2 (de) 2014-05-29 2017-04-05 General Electric Company Turbinenmotor, komponenten und verfahren zur kühlung davon
US9988913B2 (en) 2014-07-15 2018-06-05 United Technologies Corporation Using inserts to balance heat transfer and stress in high temperature alloys
US10167725B2 (en) 2014-10-31 2019-01-01 General Electric Company Engine component for a turbine engine
US10036319B2 (en) 2014-10-31 2018-07-31 General Electric Company Separator assembly for a gas turbine engine
US10260353B2 (en) * 2014-12-04 2019-04-16 Rolls-Royce Corporation Controlling exit side geometry of formed holes
FR3039199B1 (fr) * 2015-07-20 2019-12-13 Safran Helicopter Engines Aubage de distributeur haute pression avec un insert a geometrie variable
US10174620B2 (en) 2015-10-15 2019-01-08 General Electric Company Turbine blade
US10428664B2 (en) 2015-10-15 2019-10-01 General Electric Company Nozzle for a gas turbine engine
US9988936B2 (en) 2015-10-15 2018-06-05 General Electric Company Shroud assembly for a gas turbine engine
US10344619B2 (en) * 2016-07-08 2019-07-09 United Technologies Corporation Cooling system for a gaspath component of a gas powered turbine
US10704425B2 (en) 2016-07-14 2020-07-07 General Electric Company Assembly for a gas turbine engine
US10364685B2 (en) * 2016-08-12 2019-07-30 Gneral Electric Company Impingement system for an airfoil
US10408062B2 (en) * 2016-08-12 2019-09-10 General Electric Company Impingement system for an airfoil
US10436048B2 (en) * 2016-08-12 2019-10-08 General Electric Comapny Systems for removing heat from turbine components
US10443397B2 (en) * 2016-08-12 2019-10-15 General Electric Company Impingement system for an airfoil
GB2555632A (en) * 2016-11-07 2018-05-09 Rolls Royce Plc Self-sealing impingement cooling tube for a turbine vane
US20190301286A1 (en) * 2018-03-28 2019-10-03 United Technologies Corporation Airfoils for gas turbine engines
US10900362B2 (en) * 2019-01-14 2021-01-26 General Electric Company Insert system for an airfoil and method of installing same
US11085374B2 (en) * 2019-12-03 2021-08-10 General Electric Company Impingement insert with spring element for hot gas path component
US11525397B2 (en) * 2020-09-01 2022-12-13 General Electric Company Gas turbine component with ejection circuit for removing debris from cooling air supply
CN115075891A (zh) * 2022-05-29 2022-09-20 中国船舶重工集团公司第七0三研究所 一种压力侧排气的气冷涡轮导叶尾缘结构
CN114961875A (zh) * 2022-05-29 2022-08-30 中国船舶重工集团公司第七0三研究所 一种压力侧排气的气冷涡轮动叶尾缘结构

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US4063851A (en) * 1975-12-22 1977-12-20 United Technologies Corporation Coolable turbine airfoil
US4257734A (en) * 1978-03-22 1981-03-24 Rolls-Royce Limited Guide vanes for gas turbine engines
FR2473621A1 (fr) * 1980-01-10 1981-07-17 Snecma Aube de distributeur de turbine
GB2067674B (en) * 1980-01-23 1983-10-19 Rolls Royce Rotor blade for a gas turbine engine
US4820123A (en) * 1988-04-25 1989-04-11 United Technologies Corporation Dirt removal means for air cooled blades
US4962640A (en) * 1989-02-06 1990-10-16 Westinghouse Electric Corp. Apparatus and method for cooling a gas turbine vane
JPH0663442B2 (ja) * 1989-09-04 1994-08-22 株式会社日立製作所 タービン翼
US5403159A (en) * 1992-11-30 1995-04-04 United Technoligies Corporation Coolable airfoil structure
JPH07279612A (ja) * 1994-04-14 1995-10-27 Mitsubishi Heavy Ind Ltd 重質油焚き用ガスタービン冷却翼
DE19612840A1 (de) * 1996-03-30 1997-10-02 Abb Research Ltd Vorrichtung und Verfahren zur Kühlung einer einseitig von Heissgas umgebenen Wand
US5827043A (en) * 1997-06-27 1998-10-27 United Technologies Corporation Coolable airfoil
GB2343486B (en) * 1998-06-19 2000-09-20 Rolls Royce Plc Improvemnts in or relating to cooling systems for gas turbine engine airfoil
US6238182B1 (en) * 1999-02-19 2001-05-29 Meyer Tool, Inc. Joint for a turbine component

Also Published As

Publication number Publication date
US6318963B1 (en) 2001-11-20
EP1059418A2 (de) 2000-12-13
EP1059418B8 (de) 2006-11-15
EP1059418A3 (de) 2003-10-01
GB2350867B (en) 2003-03-19
DE60020007T2 (de) 2006-03-16
GB9913393D0 (en) 1999-08-11
GB2350867A (en) 2000-12-13
EP1059418B1 (de) 2005-05-11

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Legal Events

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8364 No opposition during term of opposition