NL6916221A - - Google Patents

Info

Publication number
NL6916221A
NL6916221A NL6916221A NL6916221A NL6916221A NL 6916221 A NL6916221 A NL 6916221A NL 6916221 A NL6916221 A NL 6916221A NL 6916221 A NL6916221 A NL 6916221A NL 6916221 A NL6916221 A NL 6916221A
Authority
NL
Netherlands
Application number
NL6916221A
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 NL6916221A publication Critical patent/NL6916221A/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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005—Sealing means between non relatively rotating elements

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
NL6916221A 1968-10-30 1969-10-28 NL6916221A (enrdf_load_stackoverflow)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
NL6916221A true NL6916221A (enrdf_load_stackoverflow) 1970-05-04

Family

ID=25092733

Family Applications (1)

Application Number Title Priority Date Filing Date
NL6916221A NL6916221A (enrdf_load_stackoverflow) 1968-10-30 1969-10-28

Country Status (7)

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

Families Citing this family (26)

* 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 (enrdf_load_stackoverflow) * 1981-02-17 1982-08-21
US4435123A (en) 1982-04-19 1984-03-06 United Technologies Corporation Cooling system for turbines
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
EP2372165B1 (en) * 2008-12-25 2015-12-23 Mitsubishi Hitachi Power Systems, Ltd. Stator blade structure and gas turbine
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 (en) * 2014-06-26 2015-12-30 Siemens Aktiengesellschaft Turbomachine with an outer sealing and use of the turbomachine

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE187838C (enrdf_load_stackoverflow) *
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 (enrdf_load_stackoverflow) * 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
FR1339482A (fr) * 1961-11-28 1963-10-04 Licentia Gmbh Joint de rotor à segments annulaires d'étanchéité radialement mobiles, notammentpour turbo-moteurs
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
DE1950812C3 (de) 1978-12-21
US3529906A (en) 1970-09-22
GB1241358A (en) 1971-08-04
DE1950812B2 (de) 1977-09-29
DE1950812A1 (de) 1970-06-18
SE362470B (enrdf_load_stackoverflow) 1973-12-10
FR2021903A1 (enrdf_load_stackoverflow) 1970-07-24
CH498285A (de) 1970-10-31

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