CH463877A - Turbinenleitrad - Google Patents

Turbinenleitrad

Info

Publication number
CH463877A
CH463877A CH792266A CH792266A CH463877A CH 463877 A CH463877 A CH 463877A CH 792266 A CH792266 A CH 792266A CH 792266 A CH792266 A CH 792266A CH 463877 A CH463877 A CH 463877A
Authority
CH
Switzerland
Prior art keywords
turbine nozzle
turbine
nozzle
Prior art date
Application number
CH792266A
Other languages
English (en)
Inventor
Max Kercher David
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of CH463877A publication Critical patent/CH463877A/de

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
CH792266A 1965-05-03 1966-06-01 Turbinenleitrad CH463877A (de)

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 (de) 1965-05-03 1966-05-27
DEG0047206 1966-06-20

Publications (1)

Publication Number Publication Date
CH463877A true CH463877A (de) 1968-10-15

Family

ID=27210660

Family Applications (1)

Application Number Title Priority Date Filing Date
CH792266A CH463877A (de) 1965-05-03 1966-06-01 Turbinenleitrad

Country Status (6)

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

Families Citing this family (42)

* 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
US3920947A (en) * 1972-01-27 1975-11-18 Chromalloy American Corp Turbine-nozzle manufacturing apparatus and method
US3802046A (en) * 1972-01-27 1974-04-09 Chromalloy American Corp Method of making or reconditioning a turbine-nozzle or the like assembly
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
FR2899271B1 (fr) 2006-03-29 2008-05-30 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
US7930891B1 (en) * 2007-05-10 2011-04-26 Florida Turbine Technologies, Inc. Transition duct with integral guide vanes
FR2922597B1 (fr) * 2007-10-19 2012-11-16 Snecma Aube refroidie de turbomachine
FR2928962B1 (fr) * 2008-03-19 2013-10-18 Snecma Distributeur de turbine a pales creuses.
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 (de) * 2014-05-07 2017-03-01 United Technologies Corporation Variables leitschaufelsegment
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
US10662783B2 (en) * 2018-08-29 2020-05-26 United Technologies Corporation Variable heat transfer collector baffle
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 (de) * 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

Also Published As

Publication number Publication date
DE1476790A1 (de) 1970-03-26
NL6607360A (de) 1967-11-28
BE685320A (de) 1967-01-16
GB1101543A (en) 1968-01-31
US3301527A (en) 1967-01-31

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