DE60119628T2 - Methode um den durch ein Bauteil strömenden Kühlluftstrom zu regeln - Google Patents

Methode um den durch ein Bauteil strömenden Kühlluftstrom zu regeln Download PDF

Info

Publication number
DE60119628T2
DE60119628T2 DE60119628T DE60119628T DE60119628T2 DE 60119628 T2 DE60119628 T2 DE 60119628T2 DE 60119628 T DE60119628 T DE 60119628T DE 60119628 T DE60119628 T DE 60119628T DE 60119628 T2 DE60119628 T2 DE 60119628T2
Authority
DE
Germany
Prior art keywords
cooling holes
airflow
component
thermal barrier
barrier coating
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
DE60119628T
Other languages
German (de)
English (en)
Other versions
DE60119628D1 (de
Inventor
James Michael Alexandria Caldwell
Gilbert Cincinnati Farmer
Karl Stephen Wilder Fessenden
Xuenan Loveland Wang
Jerald Michael Middletown Kauffman
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of DE60119628D1 publication Critical patent/DE60119628D1/de
Application granted granted Critical
Publication of DE60119628T2 publication Critical patent/DE60119628T2/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
    • F01D5/186—Film cooling
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/04—Coating on selected surface areas, e.g. using masks
    • C23C14/046—Coating cavities or hollow spaces, e.g. interior of tubes; Infiltration of porous substrates
    • 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
    • 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
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/288—Protective coatings for blades
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P2700/00—Indexing scheme relating to the articles being treated, e.g. manufactured, repaired, assembled, connected or other operations covered in the subgroups
    • B23P2700/06—Cooling passages of turbine components, e.g. unblocking or preventing blocking of cooling passages of turbine components
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)
  • Sorption Type Refrigeration Machines (AREA)
  • Separation By Low-Temperature Treatments (AREA)
DE60119628T 2000-07-18 2001-07-18 Methode um den durch ein Bauteil strömenden Kühlluftstrom zu regeln Expired - Lifetime DE60119628T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US618571 2000-07-18
US09/618,571 US6408610B1 (en) 2000-07-18 2000-07-18 Method of adjusting gas turbine component cooling air flow

Publications (2)

Publication Number Publication Date
DE60119628D1 DE60119628D1 (de) 2006-06-22
DE60119628T2 true DE60119628T2 (de) 2007-03-08

Family

ID=24478242

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60119628T Expired - Lifetime DE60119628T2 (de) 2000-07-18 2001-07-18 Methode um den durch ein Bauteil strömenden Kühlluftstrom zu regeln

Country Status (6)

Country Link
US (1) US6408610B1 (enExample)
EP (1) EP1174587B1 (enExample)
JP (1) JP4776822B2 (enExample)
AT (1) ATE326617T1 (enExample)
CA (1) CA2352698C (enExample)
DE (1) DE60119628T2 (enExample)

Families Citing this family (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6551061B2 (en) * 2001-03-27 2003-04-22 General Electric Company Process for forming micro cooling channels inside a thermal barrier coating system without masking material
US6499949B2 (en) * 2001-03-27 2002-12-31 Robert Edward Schafrik Turbine airfoil trailing edge with micro cooling channels
DE10143153A1 (de) 2001-09-03 2003-03-20 Rolls Royce Deutschland Turbinenschaufel für eine Gasturbine mit zumindest einer Kühlungsausnehmung
US6761956B2 (en) * 2001-12-20 2004-07-13 General Electric Company Ventilated thermal barrier coating
US6640546B2 (en) * 2001-12-20 2003-11-04 General Electric Company Foil formed cooling area enhancement
US6749396B2 (en) 2002-06-17 2004-06-15 General Electric Company Failsafe film cooled wall
US6723951B1 (en) 2003-06-04 2004-04-20 Siemens Westinghouse Power Corporation Method for reestablishing holes in a component
US7021892B2 (en) * 2003-11-19 2006-04-04 Massachusetts Institute Of Technology Method for assembling gas turbine engine components
RU2267615C1 (ru) * 2004-05-21 2006-01-10 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И. Баранова" Лопатка турбины
US20060016191A1 (en) * 2004-07-23 2006-01-26 Honeywell International Inc. Combined effusion and thick TBC cooling method
US7216485B2 (en) * 2004-09-03 2007-05-15 General Electric Company Adjusting airflow in turbine component by depositing overlay metallic coating
US7186091B2 (en) * 2004-11-09 2007-03-06 General Electric Company Methods and apparatus for cooling gas turbine engine components
GB2428608A (en) * 2005-07-30 2007-02-07 Siemens Ind Turbomachinery Ltd A method for production of a set of holes by monitoring fluid flow
GB2429515B (en) * 2005-08-11 2008-06-25 Rolls Royce Plc Cooling method and apparatus
US20090142548A1 (en) * 2007-10-18 2009-06-04 David Bruce Patterson Air cooled gas turbine components and methods of manufacturing and repairing the same
US20090226327A1 (en) * 2008-03-07 2009-09-10 Siemens Power Generation, Inc. Gas Turbine Engine Including Temperature Control Device and Method Using Memory Metal
FR2946555B1 (fr) * 2009-06-12 2012-06-01 Snecma Procede de reduction de diametre d'un orifice.
US20100329887A1 (en) * 2009-06-26 2010-12-30 Andy Eifert Coolable gas turbine engine component
US8460760B2 (en) 2010-11-30 2013-06-11 United Technologies Corporation Coating a perforated surface
US10060630B2 (en) * 2012-10-01 2018-08-28 Ansaldo Energia Ip Uk Limited Flamesheet combustor contoured liner
US20140174091A1 (en) * 2012-12-21 2014-06-26 United Technologies Corporation Repair procedure for a gas turbine engine via variable polarity welding
EP3055535A4 (en) * 2013-10-07 2016-10-05 United Technologies Corp COOLING PASS COVERED REAR
EP3058200A4 (en) * 2013-10-18 2016-11-16 United Technologies Corp TURBINE EXHAUST BOX WITH COOLING HOLES COATED
EP3066322B1 (en) * 2013-11-04 2019-11-13 United Technologies Corporation Coated cooling passage
US9744614B2 (en) 2013-11-18 2017-08-29 General Electric Company Method for modifying an aperture and system for modifying flow through a component
FR3014115B1 (fr) 2013-12-02 2017-04-28 Office National Detudes Et De Rech Aerospatiales Onera Procede et systeme de depot d'oxyde sur un composant poreux
FR3013996B1 (fr) 2013-12-02 2017-04-28 Office National Detudes Et De Rech Aerospatiales Onera Procede de reparation locale de barrieres thermiques
US9151175B2 (en) * 2014-02-25 2015-10-06 Siemens Aktiengesellschaft Turbine abradable layer with progressive wear zone multi level ridge arrays
US20160177733A1 (en) * 2014-04-25 2016-06-23 United Technologies Corporation Method of forming cooling holes
US10934853B2 (en) 2014-07-03 2021-03-02 Rolls-Royce Corporation Damage tolerant cooling of high temperature mechanical system component including a coating
US9869183B2 (en) * 2014-08-01 2018-01-16 United Technologies Corporation Thermal barrier coating inside cooling channels
EP3221643B1 (en) * 2014-11-21 2020-02-26 Ansaldo Energia IP UK Limited Combustion liner and method of reducing a recirculation zone of a combustion liner
US10829845B2 (en) * 2017-01-06 2020-11-10 General Electric Company Selective thermal coating of cooling holes with air flow
US10900377B2 (en) * 2018-04-23 2021-01-26 Honeywell International Inc. System and method for monitoring for sand plugging in gas turbine engines
US11286792B2 (en) * 2019-07-30 2022-03-29 Rolls-Royce Plc Ceramic matrix composite vane with cooling holes and methods of making the same
US11585224B2 (en) 2020-08-07 2023-02-21 General Electric Company Gas turbine engines and methods associated therewith

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2695835B2 (ja) * 1988-05-06 1998-01-14 株式会社日立製作所 セラミック被覆耐熱部材
US5247766A (en) * 1992-01-31 1993-09-28 Kildea Robert J Process for improving cooling hole flow control
US5350599A (en) * 1992-10-27 1994-09-27 General Electric Company Erosion-resistant thermal barrier coating
JPH07286503A (ja) * 1994-04-20 1995-10-31 Hitachi Ltd 高効率ガスタービン
EP0705911B1 (en) * 1994-10-04 2001-12-05 General Electric Company Thermal barrier coating
WO1996011288A1 (en) * 1994-10-05 1996-04-18 United Technologies Corporation Multiple nanolayer coating system
JP4245661B2 (ja) * 1995-06-26 2009-03-25 ゼネラル・エレクトリック・カンパニイ 多重被膜で保護した遮熱コーティング複合物
US5682747A (en) * 1996-04-10 1997-11-04 General Electric Company Gas turbine combustor heat shield of casted super alloy
US5724816A (en) * 1996-04-10 1998-03-10 General Electric Company Combustor for a gas turbine with cooling structure
US5771577A (en) * 1996-05-17 1998-06-30 General Electric Company Method for making a fluid cooled article with protective coating
US5822853A (en) * 1996-06-24 1998-10-20 General Electric Company Method for making cylindrical structures with cooling channels
US6365013B1 (en) 1997-11-03 2002-04-02 Siemens Aktiengesellschaft Coating method and device
GB9723762D0 (en) * 1997-11-12 1998-01-07 Rolls Royce Plc A method of coating a component
DE19859763A1 (de) * 1998-12-23 2000-06-29 Abb Alstom Power Ch Ag Verfahren zum Unschädlichmachen von beim Beschichten mit einer Schutzschicht entstehenden Verengungen in den Kühllöchern von gasgekühlten Teilen
US6210488B1 (en) * 1998-12-30 2001-04-03 General Electric Company Method of removing a thermal barrier coating
US6126400A (en) * 1999-02-01 2000-10-03 General Electric Company Thermal barrier coating wrap for turbine airfoil

Also Published As

Publication number Publication date
ATE326617T1 (de) 2006-06-15
JP2002097968A (ja) 2002-04-05
US6408610B1 (en) 2002-06-25
EP1174587A3 (en) 2003-11-12
CA2352698C (en) 2008-06-17
EP1174587A2 (en) 2002-01-23
EP1174587B1 (en) 2006-05-17
CA2352698A1 (en) 2002-01-18
DE60119628D1 (de) 2006-06-22
JP4776822B2 (ja) 2011-09-21

Similar Documents

Publication Publication Date Title
DE69804870T2 (de) Verfahren zum Bohren mittels Energiestrahlen sowie zur Kontrolle von Kühlmittelöffnungen
DE69800158T2 (de) Vorrichtung und Verfahren zum Wärmebehandeln
DE102008021240B4 (de) Vorrichtung zur thermischen Behandlung von Werkstücken und Verfahren zur Bestimmung der thermischen Prozessstabilität in einer solchen Vorrichtung
DE19856858C2 (de) Verfahren und Vorrichtung zur Wärmeermüdungsprüfung von Verbrennungsmotor-Brennräumen
DE102010045598B4 (de) Verfahren zum Prüfen von Prüfkörpern aus hochtemperaturfestem Material
EP1959115A2 (de) Verfahren zur automatischen Regelung einer oder mehrerer Feuerungstemperaturen einer Gasturbinenanlage und Verfahren zur Bestimmung des Wassergehalts im Arbeitsfluid einer Gasturbinenanlage
DE10230610A1 (de) Verfahren und Vorrichtung zur Verhinderung von Ablagerungen in Dampfsystemen
DE10331474A1 (de) Verfahren und Vorrichtung zur Simulation der Korrosionsbelastung
EP3180610A1 (de) Verfahren zur prüfung eines körpers mit sprödem materialverhalten
EP3182118B1 (de) Verfahren und messvorrichtung zur bestimmung von gaseigenschaften mittels korrelation
DE102018205604B3 (de) Verfahren und Vorrichtung zum Prüfen der Dauerhaltbarkeit eines AGR-Kühlers für einen Verbrennungsmotor
DE102013011149A1 (de) Messapparatur, Verfahren zum Untersuchen von Belägen auf einer Belagssonde, Verbrennungsanlage und Verfahren zum Betrieb einer derartigen Verbrennungsanlage
CH635938A5 (de) Vorrichtung zum kontinuierlichen messen der kohlenwasserstoff-konzentration in einer mehrzahl von separaten probenstroemen mittels flammen-ionisations-detektoren.
DE4237664A1 (de) Verfahren zum Betrieb eines Turboverdichters
EP2938926A1 (de) Brennstofflanzen mit wärmedämmbeschichtung
DE102006009465B4 (de) Verfahren zum Testen der Beständigkeit eines Schichtsystems, insbesondere eines Wärmedämmschicht-Systems, und Testvorrichtung
DE102019209509A1 (de) Verfahren und vorrichtung zur reinigung von bauteilen für die euv-mikrolithographie
AT521524B1 (de) Gasmischvorrichtung zur Kalibrierung von Gasanalysatoren
DE10035527A1 (de) Verfahren zur Messung des Kondensatgehaltes und zur Bestimmung der Taupunkte in Gasen sowie Vorrichtung zur Durchführung und Anwendung des Verfahrens
DE102006009951A1 (de) Simulation von Rauchgas bei Brandversuchen
DE102011117686A1 (de) Verfahren zum Prüfen einer auf einem Bauteil aufgebrachten Beschichtung und Vorrichtung zur Durchführung des Verfahrens
DE102016120179B4 (de) Verfahren zum Ermitteln der Aufteilung eines Gesamtluftstroms in einem Brennkammersystem und Brennkammersystem
DE102024110123A1 (de) Verfahren zur Ermittlung des Korrosionsverhaltens eines Wärmeüberträgers in einem Verdunstungskühlungssystems für ein Brennstoffzellensystem, Vorrichtung zur Ermittlung des Korrosionsverhaltens sowie die Verwendung des Verfahrens zur Korrosionsprüfung von Wärmeüberträgern in Verdunstungskühlungssystemen
DE102018116983A1 (de) Verfahren und Vorrichtung zum Betrieb einer Brennkraftmaschine mit einem Abgasrückführsystem
DE102018108641B4 (de) Verfahren zum Erzeugen von Dampf und Dampferzeuger

Legal Events

Date Code Title Description
8364 No opposition during term of opposition