FR2021903A1 - - Google Patents

Info

Publication number
FR2021903A1
FR2021903A1 FR6936937A FR6936937A FR2021903A1 FR 2021903 A1 FR2021903 A1 FR 2021903A1 FR 6936937 A FR6936937 A FR 6936937A FR 6936937 A FR6936937 A FR 6936937A FR 2021903 A1 FR2021903 A1 FR 2021903A1
Authority
FR
France
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.)
Withdrawn
Application number
FR6936937A
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.)
CBS Corp
Original Assignee
Westinghouse Electric 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 Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Publication of FR2021903A1 publication Critical patent/FR2021903A1/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005Sealing means between non relatively rotating elements

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR6936937A 1968-10-30 1969-10-28 Withdrawn FR2021903A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US77171268A 1968-10-30 1968-10-30

Publications (1)

Publication Number Publication Date
FR2021903A1 true FR2021903A1 (fr) 1970-07-24

Family

ID=25092733

Family Applications (1)

Application Number Title Priority Date Filing Date
FR6936937A Withdrawn FR2021903A1 (fr) 1968-10-30 1969-10-28

Country Status (7)

Country Link
US (1) US3529906A (fr)
CH (1) CH498285A (fr)
DE (1) DE1950812C3 (fr)
FR (1) FR2021903A1 (fr)
GB (1) GB1241358A (fr)
NL (1) NL6916221A (fr)
SE (1) SE362470B (fr)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4355952A (en) * 1979-06-29 1982-10-26 Westinghouse Electric Corp. Combustion turbine vane assembly
DE2931766C2 (de) * 1979-08-04 1982-08-05 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Dichtungseinrichtung für die freien Schaufelenden eines Verstell-Leitapparates einer Gasturbine
SE448757B (sv) * 1980-05-19 1987-03-16 Avco Corp Munstycke for en gasturbinmotor
JPS57134302U (fr) * 1981-02-17 1982-08-21
US4576548A (en) * 1984-01-17 1986-03-18 Westinghouse Electric Corp. Self-aligning static seal for gas turbine stator vanes
US4688988A (en) * 1984-12-17 1987-08-25 United Technologies Corporation Coolable stator assembly for a gas turbine engine
US4916892A (en) * 1988-05-06 1990-04-17 General Electric Company High pressure seal
US4863343A (en) * 1988-05-16 1989-09-05 Westinghouse Electric Corp. Turbine vane shroud sealing system
US4897021A (en) * 1988-06-02 1990-01-30 United Technologies Corporation Stator vane asssembly for an axial flow rotary machine
US5149250A (en) * 1991-02-28 1992-09-22 General Electric Company Gas turbine vane assembly seal and support system
US5284347A (en) * 1991-03-25 1994-02-08 General Electric Company Gas bearing sealing means
GB2280935A (en) * 1993-06-12 1995-02-15 Rolls Royce Plc Cooled sealing strip for nozzle guide vane segments
GB2296295A (en) * 1994-12-23 1996-06-26 Rolls Royce Plc Sealing arrangement for a gas turbine engine
JP3999395B2 (ja) * 1999-03-03 2007-10-31 三菱重工業株式会社 ガスタービン分割環
US7000406B2 (en) * 2003-12-03 2006-02-21 Pratt & Whitney Canada Corp. Gas turbine combustor sliding joint
US7596954B2 (en) * 2004-07-09 2009-10-06 United Technologies Corporation Blade clearance control
US7384235B2 (en) * 2006-04-07 2008-06-10 General Electric Company Variable clearance positive pressure packing ring and carrier arrangement with leaf springs
US7704041B2 (en) * 2006-04-07 2010-04-27 General Electric Company Variable clearance positive pressure packing ring and carrier arrangement with coil type spring
US7836702B2 (en) * 2006-09-15 2010-11-23 Pratt & Whitney Canada Corp. Gas turbine combustor exit duct and HP vane interface
US8096746B2 (en) * 2007-12-13 2012-01-17 Pratt & Whitney Canada Corp. Radial loading element for turbine vane
US8240985B2 (en) * 2008-04-29 2012-08-14 Pratt & Whitney Canada Corp. Shroud segment arrangement for gas turbine engines
EP3054169B1 (fr) * 2008-12-25 2019-02-20 Mitsubishi Hitachi Power Systems, Ltd. Agencement d'aube de stator et turbine à gaz
US8684673B2 (en) 2010-06-02 2014-04-01 Siemens Energy, Inc. Static seal for turbine engine
RU2536443C2 (ru) 2011-07-01 2014-12-27 Альстом Текнолоджи Лтд Направляющая лопатка турбины
EP2960439A1 (fr) * 2014-06-26 2015-12-30 Siemens Aktiengesellschaft Turbomachine avec un scellement externe et utilisation de la turbomachine

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE187838C (fr) *
US2623357A (en) * 1945-09-06 1952-12-30 Birmann Rudolph Gas turbine power plant having means to cool and means to compress combustion products passing through the turbine
GB666537A (en) * 1949-08-27 1952-02-13 Armstrong Siddeley Motors Ltd Mounting of the stator blades of a gaseous fluid turbine
BE514728A (fr) * 1951-10-10
US2919891A (en) * 1957-06-17 1960-01-05 Gen Electric Gas turbine diaphragm assembly
US3129922A (en) * 1961-11-27 1964-04-21 Frederick A Rosenthal Self centering ring seal
CH397360A (de) * 1961-11-28 1965-08-15 Licentia Gmbh Rotordichtung mit radial beweglichen Dichtringsegmenten, insbesondere bei Turbomaschinen
US3224194A (en) * 1963-06-26 1965-12-21 Curtiss Wright Corp Gas turbine engine
US3383033A (en) * 1966-04-27 1968-05-14 Gen Electric Sealing means for axial flow compressor discharge
US3391904A (en) * 1966-11-02 1968-07-09 United Aircraft Corp Optimum response tip seal

Also Published As

Publication number Publication date
DE1950812A1 (de) 1970-06-18
SE362470B (fr) 1973-12-10
DE1950812C3 (de) 1978-12-21
NL6916221A (fr) 1970-05-04
US3529906A (en) 1970-09-22
CH498285A (de) 1970-10-31
GB1241358A (en) 1971-08-04
DE1950812B2 (de) 1977-09-29

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Legal Events

Date Code Title Description
ST Notification of lapse