BE685320A - - Google Patents

Info

Publication number
BE685320A
BE685320A BE685320DA BE685320A BE 685320 A BE685320 A BE 685320A BE 685320D A BE685320D A BE 685320DA BE 685320 A BE685320 A BE 685320A
Authority
BE
Belgium
Application number
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 filed Critical
Publication of BE685320A publication Critical patent/BE685320A/xx

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
    • 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
    • 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)
BE685320D 1965-05-03 1966-08-10 BE685320A (xx)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US452682A US3301527A (en) 1965-05-03 1965-05-03 Turbine diaphragm structure
NL6607360A NL6607360A (xx) 1965-05-03 1966-05-27
DEG0047206 1966-06-20

Publications (1)

Publication Number Publication Date
BE685320A true BE685320A (xx) 1967-01-16

Family

ID=27210660

Family Applications (1)

Application Number Title Priority Date Filing Date
BE685320D BE685320A (xx) 1965-05-03 1966-08-10

Country Status (6)

Country Link
US (1) US3301527A (xx)
BE (1) BE685320A (xx)
CH (1) CH463877A (xx)
DE (1) DE1476790A1 (xx)
GB (1) GB1101543A (xx)
NL (1) NL6607360A (xx)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1840331A1 (fr) * 2006-03-29 2007-10-03 Snecma Ensemble d'une aube et d'une chemise de refroidissement, distributeur de turbomachine comportant l'ensemble, turbomachine, procédé de montage et de réparation de l'ensemble
EP2050930A1 (fr) * 2007-10-19 2009-04-22 Snecma Aube refroidie de turbomachine
FR2928962A1 (fr) * 2008-03-19 2009-09-25 Snecma Sa Distributeur de turbine a pales creuses.
EP3617454A1 (en) * 2018-08-29 2020-03-04 United Technologies Corporation Variable heat transfer collector baffle

Families Citing this family (38)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3412979A (en) * 1965-12-10 1968-11-26 Rolls Royce Aerofoil-shaped blade for use in a fluid flow machine such as a turbine
GB1070480A (en) * 1966-02-01 1967-06-01 Rolls Royce Aerofoil shaped blade for a fluid flow machine such as a gas turbine engine
US3963368A (en) * 1967-12-19 1976-06-15 General Motors Corporation Turbine cooling
US3574481A (en) * 1968-05-09 1971-04-13 James A Pyne Jr Variable area cooled airfoil construction for gas turbines
US3529903A (en) * 1968-11-29 1970-09-22 Westinghouse Electric Corp Nozzle blade structure
US3715170A (en) * 1970-12-11 1973-02-06 Gen Electric Cooled turbine blade
US3802046A (en) * 1972-01-27 1974-04-09 Chromalloy American Corp Method of making or reconditioning a turbine-nozzle or the like assembly
US3920947A (en) * 1972-01-27 1975-11-18 Chromalloy American Corp Turbine-nozzle manufacturing apparatus and method
US3858290A (en) * 1972-11-21 1975-01-07 Avco Corp Method of making inserts for cooled turbine blades
US4288201A (en) * 1979-09-14 1981-09-08 United Technologies Corporation Vane cooling structure
DE3629910A1 (de) * 1986-09-03 1988-03-17 Mtu Muenchen Gmbh Metallisches hohlbauteil mit einem metallischen einsatz, insbesondere turbinenschaufel mit kuehleinsatz
FR2659689B1 (fr) * 1990-03-14 1992-06-05 Snecma Circuit de refroidissement interne d'une aube directrice de turbine.
US5145315A (en) * 1991-09-27 1992-09-08 Westinghouse Electric Corp. Gas turbine vane cooling air insert
US5493855A (en) * 1992-12-17 1996-02-27 Alfred E. Tisch Turbine having suspended rotor blades
US5611662A (en) * 1995-08-01 1997-03-18 General Electric Co. Impingement cooling for turbine stator vane trailing edge
US6237344B1 (en) 1998-07-20 2001-05-29 General Electric Company Dimpled impingement baffle
US6193465B1 (en) * 1998-09-28 2001-02-27 General Electric Company Trapped insert turbine airfoil
DE10004128B4 (de) 2000-01-31 2007-06-28 Alstom Technology Ltd. Luftgekühlte Turbinenschaufel
FR2872541B1 (fr) * 2004-06-30 2006-11-10 Snecma Moteurs Sa Aube fixe de turbine a refroidissement ameliore
FR2877390B1 (fr) * 2004-10-29 2010-09-03 Snecma Moteurs Secteur de distribution de turbine alimente en air de refroidissement
US20060099073A1 (en) * 2004-11-05 2006-05-11 Toufik Djeridane Aspherical dimples for heat transfer surfaces and method
US7930891B1 (en) * 2007-05-10 2011-04-26 Florida Turbine Technologies, Inc. Transition duct with integral guide vanes
US8109724B2 (en) * 2009-03-26 2012-02-07 United Technologies Corporation Recessed metering standoffs for airfoil baffle
US8449249B2 (en) 2010-04-09 2013-05-28 Williams International Co., L.L.C. Turbine nozzle apparatus and associated method of manufacture
JP2015527530A (ja) 2012-08-20 2015-09-17 アルストム テクノロジー リミテッドＡＬＳＴＯＭ Ｔｅｃｈｎｏｌｏｇｙ Ｌｔｄ 回転機械用の内部冷却される翼
EP2949871B1 (en) * 2014-05-07 2017-03-01 United Technologies Corporation Variable vane segment
US10781715B2 (en) * 2015-12-21 2020-09-22 Raytheon Technologies Corporation Impingement cooling baffle
JP6651378B2 (ja) * 2016-02-22 2020-02-19 三菱日立パワーシステムズ株式会社 インサート組品、翼、ガスタービン、および、翼の製造方法
EP3236009A1 (de) 2016-04-21 2017-10-25 Siemens Aktiengesellschaft Leitschaufel mit einem verbindungsrohr
US10450880B2 (en) * 2016-08-04 2019-10-22 United Technologies Corporation Air metering baffle assembly
US10309242B2 (en) * 2016-08-10 2019-06-04 General Electric Company Ceramic matrix composite component cooling
US11702941B2 (en) * 2018-11-09 2023-07-18 Raytheon Technologies Corporation Airfoil with baffle having flange ring affixed to platform
US10711620B1 (en) * 2019-01-14 2020-07-14 General Electric Company Insert system for an airfoil and method of installing same
US11371360B2 (en) * 2019-06-05 2022-06-28 Raytheon Technologies Corporation Components for gas turbine engines
US11448075B2 (en) * 2020-11-02 2022-09-20 Raytheon Technologies Corporation CMC vane arc segment with cantilevered spar
US11428166B2 (en) * 2020-11-12 2022-08-30 Solar Turbines Incorporated Fin for internal cooling of vane wall
FR3116466B1 (fr) * 2020-11-25 2022-11-25 Safran Ceram Préforme fibreuse d'un profil aérodynamique d'aube de turbomachine
US20230407753A1 (en) * 2022-06-17 2023-12-21 Raytheon Technologies Corporation Flow guides for internal cooling of a cmc airfoil

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE498667A (xx) * 1949-08-27
GB685769A (en) * 1949-11-22 1953-01-14 Rolls Royce Improvements relating to compressor and turbine blading
FR1262552A (fr) * 1950-03-02 1961-06-05 Structure et fixation de chemises pour le guidage du fluide assurant le refroidissement interne d'aubes creuses pour machines à écoulement de fluide
GB753224A (en) * 1953-04-13 1956-07-18 Rolls Royce Improvements in or relating to blading for turbines or compressors
US2879028A (en) * 1954-03-31 1959-03-24 Edward A Stalker Cooled turbine blades
US2920866A (en) * 1954-12-20 1960-01-12 A V Roe Canada Ltd Hollow air cooled sheet metal turbine blade
FR1177035A (fr) * 1957-05-28 1959-04-20 Snecma Procédé et dispositif de refroidissement d'organes de machines
US3045965A (en) * 1959-04-27 1962-07-24 Rolls Royce Turbine blades, vanes and the like

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1840331A1 (fr) * 2006-03-29 2007-10-03 Snecma Ensemble d'une aube et d'une chemise de refroidissement, distributeur de turbomachine comportant l'ensemble, turbomachine, procédé de montage et de réparation de l'ensemble
FR2899271A1 (fr) * 2006-03-29 2007-10-05 Snecma Sa Ensemble d'une aube et d'une chemise de refroidissement, distributeur de turbomachine comportant l'ensemble, turbomachine, procede de montage et de reparation de l'ensemble
US7819628B2 (en) 2006-03-29 2010-10-26 Snecma Assembly comprised of a vane and of a cooling liner, turbomachine nozzle guide vanes assembly comprising this assembly, turbomachine and method of fitting and of repairing this assembly
EP2050930A1 (fr) * 2007-10-19 2009-04-22 Snecma Aube refroidie de turbomachine
FR2922597A1 (fr) * 2007-10-19 2009-04-24 Snecma Sa Aube refroidie de turbomachine
US8162594B2 (en) 2007-10-19 2012-04-24 Snecma Cooled blade for a turbomachine
RU2489573C2 (ru) * 2007-10-19 2013-08-10 Снекма Охлаждаемая лопатка газотурбинного двигателя, способ ее сборки, направляющий сопловый аппарат газотурбинного двигателя, турбина, содержащая указанный аппарат, газотурбинный двигатель
FR2928962A1 (fr) * 2008-03-19 2009-09-25 Snecma Sa Distributeur de turbine a pales creuses.
EP3617454A1 (en) * 2018-08-29 2020-03-04 United Technologies Corporation Variable heat transfer collector baffle
US10662783B2 (en) 2018-08-29 2020-05-26 United Technologies Corporation Variable heat transfer collector baffle

Also Published As

Publication number Publication date
NL6607360A (xx) 1967-11-28
US3301527A (en) 1967-01-31
GB1101543A (en) 1968-01-31
CH463877A (de) 1968-10-15
DE1476790A1 (de) 1970-03-26

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