DE60213328D1 - Gekühlte hohle Schaufelspitzenabdeckung einer Turbinenschaufel - Google Patents

Gekühlte hohle Schaufelspitzenabdeckung einer Turbinenschaufel

Info

Publication number
DE60213328D1
DE60213328D1 DE60213328T DE60213328T DE60213328D1 DE 60213328 D1 DE60213328 D1 DE 60213328D1 DE 60213328 T DE60213328 T DE 60213328T DE 60213328 T DE60213328 T DE 60213328T DE 60213328 D1 DE60213328 D1 DE 60213328D1
Authority
DE
Germany
Prior art keywords
shovel
top cover
turbine
chilled hollow
chilled
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
DE60213328T
Other languages
English (en)
Other versions
DE60213328T2 (de
Inventor
J Tyson Balkcum Iii
George Liang
Timothy J Remley
Christopher Charles Williams
Hans R Przirembel
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
Application granted granted Critical
Publication of DE60213328D1 publication Critical patent/DE60213328D1/de
Publication of DE60213328T2 publication Critical patent/DE60213328T2/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
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
    • F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
    • 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
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/21—Manufacture essentially without removing material by casting
    • 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
    • F05D2260/202—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
    • F05D2260/203—Heat transfer, e.g. cooling by transpiration cooling

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE60213328T 2001-04-16 2002-04-16 Gekühlte hohle Schaufelspitzenabdeckung einer Turbinenschaufel Expired - Lifetime DE60213328T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US835426 2001-04-16
US09/835,426 US6471480B1 (en) 2001-04-16 2001-04-16 Thin walled cooled hollow tip shroud

Publications (2)

Publication Number Publication Date
DE60213328D1 true DE60213328D1 (de) 2006-09-07
DE60213328T2 DE60213328T2 (de) 2007-07-26

Family

ID=25269479

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60213328T Expired - Lifetime DE60213328T2 (de) 2001-04-16 2002-04-16 Gekühlte hohle Schaufelspitzenabdeckung einer Turbinenschaufel

Country Status (4)

Country Link
US (1) US6471480B1 (de)
EP (1) EP1267037B1 (de)
JP (1) JP2002349205A (de)
DE (1) DE60213328T2 (de)

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FR2853931A1 (fr) 2003-04-16 2004-10-22 Snecma Moteurs Reduction de jeux dans une turbine a gaz
ES2337800T3 (es) * 2004-03-30 2010-04-29 Alstom Technology Ltd Dispositivo para la presurizacion de aire de refrigeracion en un alabe de rodete.
US7118326B2 (en) * 2004-06-17 2006-10-10 Siemens Power Generation, Inc. Cooled gas turbine vane
AU2005284134B2 (en) * 2004-09-16 2008-10-09 General Electric Technology Gmbh Turbine engine vane with fluid cooled shroud
US7686581B2 (en) * 2006-06-07 2010-03-30 General Electric Company Serpentine cooling circuit and method for cooling tip shroud
US7572102B1 (en) 2006-09-20 2009-08-11 Florida Turbine Technologies, Inc. Large tapered air cooled turbine blade
US7568882B2 (en) * 2007-01-12 2009-08-04 General Electric Company Impingement cooled bucket shroud, turbine rotor incorporating the same, and cooling method
US7819629B2 (en) * 2007-02-15 2010-10-26 Siemens Energy, Inc. Blade for a gas turbine
US7871246B2 (en) * 2007-02-15 2011-01-18 Siemens Energy, Inc. Airfoil for a gas turbine
US7887295B2 (en) * 2007-11-08 2011-02-15 General Electric Company Z-Notch shape for a turbine blade
US7976280B2 (en) * 2007-11-28 2011-07-12 General Electric Company Turbine bucket shroud internal core profile
US10286407B2 (en) 2007-11-29 2019-05-14 General Electric Company Inertial separator
US7946816B2 (en) * 2008-01-10 2011-05-24 General Electric Company Turbine blade tip shroud
US7946817B2 (en) * 2008-01-10 2011-05-24 General Electric Company Turbine blade tip shroud
US8057177B2 (en) * 2008-01-10 2011-11-15 General Electric Company Turbine blade tip shroud
US8348612B2 (en) * 2008-01-10 2013-01-08 General Electric Company Turbine blade tip shroud
US20090180894A1 (en) * 2008-01-10 2009-07-16 General Electric Company Turbine blade tip shroud
US8322986B2 (en) * 2008-07-29 2012-12-04 General Electric Company Rotor blade and method of fabricating the same
CH699593A1 (de) * 2008-09-25 2010-03-31 Alstom Technology Ltd Schaufel für eine gasturbine.
US8096767B1 (en) * 2009-02-04 2012-01-17 Florida Turbine Technologies, Inc. Turbine blade with serpentine cooling circuit formed within the tip shroud
JP2010216321A (ja) * 2009-03-16 2010-09-30 Hitachi Ltd 蒸気タービンの動翼及びそれを用いた蒸気タービン
US8096772B2 (en) * 2009-03-20 2012-01-17 Siemens Energy, Inc. Turbine vane for a gas turbine engine having serpentine cooling channels within the inner endwall
CH700687A1 (de) * 2009-03-30 2010-09-30 Alstom Technology Ltd Gekühltes bauteil für eine gasturbine.
US20120195742A1 (en) * 2011-01-28 2012-08-02 Jain Sanjeev Kumar Turbine bucket for use in gas turbine engines and methods for fabricating the same
US8444372B2 (en) 2011-02-07 2013-05-21 General Electric Company Passive cooling system for a turbomachine
US9127560B2 (en) * 2011-12-01 2015-09-08 General Electric Company Cooled turbine blade and method for cooling a turbine blade
US9249667B2 (en) 2012-03-15 2016-02-02 General Electric Company Turbomachine blade with improved stiffness to weight ratio
US9429027B2 (en) 2012-04-05 2016-08-30 United Technologies Corporation Turbine airfoil tip shelf and squealer pocket cooling
US9759070B2 (en) 2013-08-28 2017-09-12 General Electric Company Turbine bucket tip shroud
US11033845B2 (en) 2014-05-29 2021-06-15 General Electric Company Turbine engine and particle separators therefore
WO2016025056A2 (en) 2014-05-29 2016-02-18 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
US10975731B2 (en) 2014-05-29 2021-04-13 General Electric Company Turbine engine, components, and methods of cooling same
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
US10202854B2 (en) * 2014-12-18 2019-02-12 Rolls-Royce North America Technologies, Inc. Abrasive tips for ceramic matrix composite blades and methods for making the same
US9822653B2 (en) 2015-07-16 2017-11-21 General Electric Company Cooling structure for stationary blade
JP6025941B1 (ja) * 2015-08-25 2016-11-16 三菱日立パワーシステムズ株式会社 タービン動翼、及び、ガスタービン
US9988936B2 (en) 2015-10-15 2018-06-05 General Electric Company Shroud assembly for a gas turbine engine
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
US9885243B2 (en) 2015-10-27 2018-02-06 General Electric Company Turbine bucket having outlet path in shroud
US10156145B2 (en) * 2015-10-27 2018-12-18 General Electric Company Turbine bucket having cooling passageway
US10184342B2 (en) 2016-04-14 2019-01-22 General Electric Company System for cooling seal rails of tip shroud of turbine blade
US10344599B2 (en) * 2016-05-24 2019-07-09 General Electric Company Cooling passage for gas turbine rotor blade
US10704425B2 (en) 2016-07-14 2020-07-07 General Electric Company Assembly for a gas turbine engine
US10746029B2 (en) 2017-02-07 2020-08-18 General Electric Company Turbomachine rotor blade tip shroud cavity
US10502069B2 (en) * 2017-06-07 2019-12-10 General Electric Company Turbomachine rotor blade
US10577945B2 (en) * 2017-06-30 2020-03-03 General Electric Company Turbomachine rotor blade
CN109630207B (zh) * 2018-12-10 2021-07-09 中国航发四川燃气涡轮研究院 一种带叶冠加强筋的空心涡轮转子叶片

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US3527544A (en) * 1968-12-12 1970-09-08 Gen Motors Corp Cooled blade shroud
GB1276200A (en) * 1969-12-02 1972-06-01 Rolls Royce Improvements in or relating to blades for fluid flow machines
GB1514613A (en) * 1976-04-08 1978-06-14 Rolls Royce Blade or vane for a gas turbine engine
US5350277A (en) * 1992-11-20 1994-09-27 General Electric Company Closed-circuit steam-cooled bucket with integrally cooled shroud for gas turbines and methods of steam-cooling the buckets and shrouds
US5344283A (en) * 1993-01-21 1994-09-06 United Technologies Corporation Turbine vane having dedicated inner platform cooling
GB2290833B (en) * 1994-07-02 1998-08-05 Rolls Royce Plc Turbine blade
US5634766A (en) * 1994-08-23 1997-06-03 General Electric Co. Turbine stator vane segments having combined air and steam cooling circuits
JPH10317904A (ja) * 1997-03-17 1998-12-02 Mitsubishi Heavy Ind Ltd タービンのシュラウド翼
DE69931088T2 (de) * 1998-02-04 2006-12-07 Mitsubishi Heavy Industries, Ltd. Gasturbinenlaufschaufel
DE59912323D1 (de) * 1998-12-24 2005-09-01 Alstom Technology Ltd Baden Turbinenschaufel mit aktiv gekühltem Deckbandelememt
EP1041247B1 (de) * 1999-04-01 2012-08-01 General Electric Company Gasturbinenschaufel mit einem offenen Kühlkreislauf

Also Published As

Publication number Publication date
US20020150474A1 (en) 2002-10-17
EP1267037A2 (de) 2002-12-18
DE60213328T2 (de) 2007-07-26
JP2002349205A (ja) 2002-12-04
EP1267037B1 (de) 2006-07-26
EP1267037A3 (de) 2004-02-04
US6471480B1 (en) 2002-10-29

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