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DE60007985D1 - Gegossene einspritzdüse mit veränderbarem durchströmten querschnitt - Google Patents

Gegossene einspritzdüse mit veränderbarem durchströmten querschnitt

Info

Publication number
DE60007985D1
DE60007985D1 DE60007985T DE60007985T DE60007985D1 DE 60007985 D1 DE60007985 D1 DE 60007985D1 DE 60007985 T DE60007985 T DE 60007985T DE 60007985 T DE60007985 T DE 60007985T DE 60007985 D1 DE60007985 D1 DE 60007985D1
Authority
DE
Germany
Prior art keywords
changeable
section
injection nozzle
molded injection
flowed cross
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
DE60007985T
Other languages
English (en)
Other versions
DE60007985T2 (de
Inventor
F Glasspoole
Yvan Schraenen
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.)
Pratt and Whitney Canada Corp
Original Assignee
Pratt and Whitney Canada 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 Pratt and Whitney Canada Corp filed Critical Pratt and Whitney Canada Corp
Application granted granted Critical
Publication of DE60007985D1 publication Critical patent/DE60007985D1/de
Publication of DE60007985T2 publication Critical patent/DE60007985T2/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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/08—Heating, heat-insulating or cooling means
    • 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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/08—Heating, heat-insulating or cooling means
    • F01D5/085—Heating, heat-insulating or cooling means cooling fluid circulating inside the rotor
    • F01D5/087—Heating, heat-insulating or cooling means cooling fluid circulating inside the rotor in the radial passages of the rotor disc
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
DE60007985T 1999-05-21 2000-05-18 Gegossene einspritzdüse mit veränderbarem durchströmten querschnitt Expired - Lifetime DE60007985T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US315957 1999-05-21
US09/315,957 US6183193B1 (en) 1999-05-21 1999-05-21 Cast on-board injection nozzle with adjustable flow area
PCT/CA2000/000571 WO2000071854A1 (en) 1999-05-21 2000-05-18 Cast on-board injection nozzle with adjustable flow area

Publications (2)

Publication Number Publication Date
DE60007985D1 true DE60007985D1 (de) 2004-03-04
DE60007985T2 DE60007985T2 (de) 2004-12-09

Family

ID=23226837

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60007985T Expired - Lifetime DE60007985T2 (de) 1999-05-21 2000-05-18 Gegossene einspritzdüse mit veränderbarem durchströmten querschnitt

Country Status (6)

Country Link
US (1) US6183193B1 (de)
EP (1) EP1183442B1 (de)
JP (1) JP2003500585A (de)
CA (1) CA2372928C (de)
DE (1) DE60007985T2 (de)
WO (1) WO2000071854A1 (de)

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US6398487B1 (en) * 2000-07-14 2002-06-04 General Electric Company Methods and apparatus for supplying cooling airflow in turbine engines
US6468032B2 (en) * 2000-12-18 2002-10-22 Pratt & Whitney Canada Corp. Further cooling of pre-swirl flow entering cooled rotor aerofoils
US6540477B2 (en) * 2001-05-21 2003-04-01 General Electric Company Turbine cooling circuit
US6575703B2 (en) 2001-07-20 2003-06-10 General Electric Company Turbine disk side plate
US6517314B1 (en) * 2001-11-05 2003-02-11 General Electric Company Method and apparatus for eliminating thermal bowing and axial thrust loads of steam turbine rotors
US6773225B2 (en) * 2002-05-30 2004-08-10 Mitsubishi Heavy Industries, Ltd. Gas turbine and method of bleeding gas therefrom
US6981841B2 (en) * 2003-11-20 2006-01-03 General Electric Company Triple circuit turbine cooling
US6960060B2 (en) 2003-11-20 2005-11-01 General Electric Company Dual coolant turbine blade
US7510371B2 (en) * 2005-06-06 2009-03-31 General Electric Company Forward tilted turbine nozzle
US7513102B2 (en) * 2005-06-06 2009-04-07 General Electric Company Integrated counterrotating turbofan
US7594388B2 (en) * 2005-06-06 2009-09-29 General Electric Company Counterrotating turbofan engine
US8277169B2 (en) * 2005-06-16 2012-10-02 Honeywell International Inc. Turbine rotor cooling flow system
US7918024B2 (en) * 2006-01-20 2011-04-05 General Electric Company Methods and apparatus for manufacturing components
US20080041064A1 (en) * 2006-08-17 2008-02-21 United Technologies Corporation Preswirl pollution air handling with tangential on-board injector for turbine rotor cooling
US7870742B2 (en) * 2006-11-10 2011-01-18 General Electric Company Interstage cooled turbine engine
US7926289B2 (en) * 2006-11-10 2011-04-19 General Electric Company Dual interstage cooled engine
US7743613B2 (en) * 2006-11-10 2010-06-29 General Electric Company Compound turbine cooled engine
US7870743B2 (en) * 2006-11-10 2011-01-18 General Electric Company Compound nozzle cooled engine
US8562285B2 (en) * 2007-07-02 2013-10-22 United Technologies Corporation Angled on-board injector
US7762086B2 (en) * 2008-03-12 2010-07-27 United Technologies Corporation Nozzle extension assembly for ground and flight testing
JP5502340B2 (ja) * 2009-02-25 2014-05-28 三菱重工業株式会社 タービンの冷却構造およびガスタービン
US8113784B2 (en) * 2009-03-20 2012-02-14 Hamilton Sundstrand Corporation Coolable airfoil attachment section
JP5566683B2 (ja) * 2009-12-25 2014-08-06 三菱重工業株式会社 ガスタービン
JP5439164B2 (ja) * 2009-12-25 2014-03-12 三菱重工業株式会社 ガスタービンの冷却流路構造、ガスタービンおよびガスタービンの冷却流路構造の調整方法
US8529195B2 (en) * 2010-10-12 2013-09-10 General Electric Company Inducer for gas turbine system
US20120183389A1 (en) * 2011-01-13 2012-07-19 Mhetras Shantanu P Seal system for cooling fluid flow through a rotor assembly in a gas turbine engine
US8899924B2 (en) 2011-06-20 2014-12-02 United Technologies Corporation Non-mechanically fastened TOBI heat shield
US9080449B2 (en) 2011-08-16 2015-07-14 United Technologies Corporation Gas turbine engine seal assembly having flow-through tube
US9038398B2 (en) 2012-02-27 2015-05-26 United Technologies Corporation Gas turbine engine buffer cooling system
US9435259B2 (en) 2012-02-27 2016-09-06 United Technologies Corporation Gas turbine engine cooling system
US9157325B2 (en) 2012-02-27 2015-10-13 United Technologies Corporation Buffer cooling system providing gas turbine engine architecture cooling
US9347374B2 (en) 2012-02-27 2016-05-24 United Technologies Corporation Gas turbine engine buffer cooling system
JP5901360B2 (ja) * 2012-03-06 2016-04-06 三菱重工業株式会社 タービンの冷却構造及びガスタービン
US9091173B2 (en) 2012-05-31 2015-07-28 United Technologies Corporation Turbine coolant supply system
US20140010649A1 (en) * 2012-07-09 2014-01-09 United Technologies Corporation Mid-turbine frame hpt seal support meshing
US9435206B2 (en) * 2012-09-11 2016-09-06 General Electric Company Flow inducer for a gas turbine system
WO2014051690A1 (en) * 2012-09-26 2014-04-03 United Technologies Corporation Fastened joint for a tangential on board injector
WO2014189589A2 (en) 2013-03-06 2014-11-27 Rolls-Royce North American Technologies, Inc. Gas turbine engine with soft mounted pre-swirl nozzle
WO2015023342A2 (en) 2013-06-04 2015-02-19 United Technologies Corporation Gas turbine engine with dove-tailed tobi vane
EP3036418B1 (de) 2013-08-19 2022-02-09 Raytheon Technologies Corporation Gasturbine
US10677161B2 (en) 2013-08-28 2020-06-09 Raytheon Technologies Corporation Gas turbine engine diffuser cooling and mixing arrangement
EP3044440B1 (de) 2013-09-10 2019-12-11 United Technologies Corporation Fluidinjektor zur kühlung eines gasturbinenmotorbauteils
WO2015073112A2 (en) * 2013-10-03 2015-05-21 United Technologies Corporation Feature to provide cooling flow to disk
US20150308449A1 (en) * 2014-03-11 2015-10-29 United Technologies Corporation Gas turbine engine component with brazed cover
US9945248B2 (en) 2014-04-01 2018-04-17 United Technologies Corporation Vented tangential on-board injector for a gas turbine engine
US10669852B2 (en) 2014-06-04 2020-06-02 Mitsubishi Hitachi Power Systems, Ltd. Gas turbine
US10167723B2 (en) 2014-06-06 2019-01-01 United Technologies Corporation Thermally isolated turbine section for a gas turbine engine
US10221708B2 (en) * 2014-12-03 2019-03-05 United Technologies Corporation Tangential on-board injection vanes
US10634055B2 (en) * 2015-02-05 2020-04-28 United Technologies Corporation Gas turbine engine having section with thermally isolated area
US9920652B2 (en) 2015-02-09 2018-03-20 United Technologies Corporation Gas turbine engine having section with thermally isolated area
US20170089213A1 (en) * 2015-09-28 2017-03-30 United Technologies Corporation Duct with additive manufactured seal
US10030519B2 (en) * 2015-10-26 2018-07-24 Rolls-Royce Corporation System and method to retain a turbine cover plate between nested turbines with a tie bolt and spanner nut
US10718220B2 (en) * 2015-10-26 2020-07-21 Rolls-Royce Corporation System and method to retain a turbine cover plate with a spanner nut
KR101953963B1 (ko) * 2017-01-24 2019-03-04 두산중공업 주식회사 가스터빈
US10718213B2 (en) * 2017-04-10 2020-07-21 United Technologies Corporation Dual cooling airflow to blades
US10927706B2 (en) 2018-11-01 2021-02-23 Raytheon Technologies Corporation Intercooled tangential air injector for gas turbine engines
CN110886654A (zh) * 2019-10-25 2020-03-17 南京航空航天大学 一种用于径向预旋系统的狭缝式接受孔结构
FR3108661B1 (fr) * 2020-03-25 2022-09-02 Safran Aircraft Engines Couronne d’injecteurs de turbine
US11466590B1 (en) * 2021-06-17 2022-10-11 Pratt & Whitney Canada Corp. Mid-turbine frame with intermediary plenum

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GB2118629B (en) 1982-04-21 1985-07-17 Rolls Royce Device for passing a fluid flow eg. cooling air through a barrier eg. bolted joint
US4526511A (en) 1982-11-01 1985-07-02 United Technologies Corporation Attachment for TOBI
US4708588A (en) 1984-12-14 1987-11-24 United Technologies Corporation Turbine cooling air supply system
US4674955A (en) * 1984-12-21 1987-06-23 The Garrett Corporation Radial inboard preswirl system
US4882902A (en) * 1986-04-30 1989-11-28 General Electric Company Turbine cooling air transferring apparatus
US4730978A (en) * 1986-10-28 1988-03-15 United Technologies Corporation Cooling air manifold for a gas turbine engine
US4822244A (en) 1987-10-15 1989-04-18 United Technologies Corporation Tobi
US5245821A (en) 1991-10-21 1993-09-21 General Electric Company Stator to rotor flow inducer
US5215435A (en) 1991-10-28 1993-06-01 General Electric Company Angled cooling air bypass slots in honeycomb seals
US5875549A (en) * 1997-03-17 1999-03-02 Siemens Westinghouse Power Corporation Method of forming internal passages within articles and articles formed by same
US5996331A (en) * 1997-09-15 1999-12-07 Alliedsignal Inc. Passive turbine coolant regulator responsive to engine load

Also Published As

Publication number Publication date
JP2003500585A (ja) 2003-01-07
EP1183442B1 (de) 2004-01-28
CA2372928C (en) 2007-12-11
DE60007985T2 (de) 2004-12-09
CA2372928A1 (en) 2000-11-30
US6183193B1 (en) 2001-02-06
EP1183442A1 (de) 2002-03-06
WO2000071854A1 (en) 2000-11-30

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