JPS5330847B2 - - Google Patents

Info

Publication number
JPS5330847B2
JPS5330847B2 JP5479475A JP5479475A JPS5330847B2 JP S5330847 B2 JPS5330847 B2 JP S5330847B2 JP 5479475 A JP5479475 A JP 5479475A JP 5479475 A JP5479475 A JP 5479475A JP S5330847 B2 JPS5330847 B2 JP S5330847B2
Authority
JP
Japan
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
Application number
JP5479475A
Other languages
Japanese (ja)
Other versions
JPS50155819A (en
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 JPS50155819A publication Critical patent/JPS50155819A/ja
Publication of JPS5330847B2 publication Critical patent/JPS5330847B2/ja
Expired 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
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
JP5479475A 1974-05-14 1975-05-12 Expired JPS5330847B2 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US469928A US3892497A (en) 1974-05-14 1974-05-14 Axial flow turbine stationary blade and blade ring locking arrangement

Publications (2)

Publication Number Publication Date
JPS50155819A JPS50155819A (en) 1975-12-16
JPS5330847B2 true JPS5330847B2 (en) 1978-08-30

Family

ID=23865587

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5479475A Expired JPS5330847B2 (en) 1974-05-14 1975-05-12

Country Status (6)

Country Link
US (1) US3892497A (en)
JP (1) JPS5330847B2 (en)
CA (1) CA1015665A (en)
FR (1) FR2271400B3 (en)
GB (1) GB1476553A (en)
IT (1) IT1038116B (en)

Families Citing this family (56)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3981609A (en) * 1975-06-02 1976-09-21 United Technologies Corporation Coolable blade tip shroud
US3975112A (en) * 1975-06-09 1976-08-17 United Technologies Corporation Apparatus for sealing a gas turbine flow path
GB1501916A (en) * 1975-06-20 1978-02-22 Rolls Royce Matching thermal expansions of components of turbo-machines
US3975114A (en) * 1975-09-23 1976-08-17 Westinghouse Electric Corporation Seal arrangement for turbine diaphragms and the like
DE2617024C2 (en) * 1976-04-17 1985-09-26 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Gas turbine engine
US4247248A (en) * 1978-12-20 1981-01-27 United Technologies Corporation Outer air seal support structure for gas turbine engine
DE2907748A1 (en) * 1979-02-28 1980-09-04 Motoren Turbinen Union DEVICE FOR MINIMIZING AND MAINTAINING THE SHOVEL TIP GAMES EXISTING WITH AXIAL TURBINES, IN PARTICULAR FOR GAS TURBINE ENGINES
US4537024A (en) * 1979-04-23 1985-08-27 Solar Turbines, Incorporated Turbine engines
US4355952A (en) * 1979-06-29 1982-10-26 Westinghouse Electric Corp. Combustion turbine vane assembly
US4832568A (en) * 1982-02-26 1989-05-23 General Electric Company Turbomachine airfoil mounting assembly
US4492517A (en) * 1983-01-06 1985-01-08 General Electric Company Segmented inlet nozzle for gas turbine, and methods of installation
DE3333436C1 (en) * 1983-09-16 1985-02-14 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Device for the axial and circumferential securing of static housing components for flow machines
IT1167241B (en) * 1983-10-03 1987-05-13 Nuovo Pignone Spa IMPROVED SYSTEM FOR FIXING STATOR NOZZLES TO THE CASE OF A POWER TURBINE
US4688988A (en) * 1984-12-17 1987-08-25 United Technologies Corporation Coolable stator assembly for a gas turbine engine
FR2577281B1 (en) * 1985-02-13 1987-03-20 Snecma TURBOMACHINE HOUSING ASSOCIATED WITH A DEVICE FOR ADJUSTING THE GAP BETWEEN MOBILE BLADES AND HOUSING
US4749333A (en) * 1986-05-12 1988-06-07 The United States Of America As Represented By The Secretary Of The Air Force Vane platform sealing and retention means
US4728257A (en) * 1986-06-18 1988-03-01 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Thermal stress minimized, two component, turbine shroud seal
FR2607198B1 (en) * 1986-11-26 1990-05-04 Snecma COMPRESSOR HOUSING SUITABLE FOR ACTIVE PILOTAGE OF ITS EXPANSIONS AND MANUFACTURING METHOD THEREOF
GB2206651B (en) * 1987-07-01 1991-05-08 Rolls Royce Plc Turbine blade shroud structure
US4816213A (en) * 1987-08-24 1989-03-28 Westinghouse Electric Corp. Thermal distortion isolation system for turbine blade rings
US4920742A (en) * 1988-05-31 1990-05-01 General Electric Company Heat shield for gas turbine engine frame
US4957412A (en) * 1988-09-06 1990-09-18 Westinghouse Electric Corp. Apparatus and method for supporting the torque load on a gas turbine vane
US4921401A (en) * 1989-02-23 1990-05-01 United Technologies Corporation Casting for a rotary machine
GB2239678B (en) * 1989-12-08 1993-03-03 Rolls Royce Plc Gas turbine engine blade shroud assembly
US5158430A (en) * 1990-09-12 1992-10-27 United Technologies Corporation Segmented stator vane seal
US5224824A (en) * 1990-09-12 1993-07-06 United Technologies Corporation Compressor case construction
US5127797A (en) * 1990-09-12 1992-07-07 United Technologies Corporation Compressor case attachment means
SE500743C2 (en) * 1992-04-01 1994-08-22 Abb Carbon Ab Method and apparatus for mounting axial flow machine
EP0591565B1 (en) * 1992-10-05 1996-01-24 Asea Brown Boveri Ag Stator blade fastening for axial through-flow turbomachines
US5320486A (en) * 1993-01-21 1994-06-14 General Electric Company Apparatus for positioning compressor liner segments
US5412939A (en) * 1993-12-20 1995-05-09 Alliedsignal Inc. Seal compression tool for gas turbine engine
US5503490A (en) * 1994-05-13 1996-04-02 United Technologies Corporation Thermal load relief ring for engine case
US5618161A (en) * 1995-10-17 1997-04-08 Westinghouse Electric Corporation Apparatus for restraining motion of a turbo-machine stationary vane
WO1998058158A1 (en) * 1997-06-19 1998-12-23 Mitsubishi Heavy Industries, Ltd. Device for sealing gas turbine stator blades
WO2000057033A1 (en) 1999-03-24 2000-09-28 Siemens Aktiengesellschaft Covering element and arrangement with a covering element and a support structure
US6343912B1 (en) * 1999-12-07 2002-02-05 General Electric Company Gas turbine or jet engine stator vane frame
JP2002213207A (en) * 2001-01-15 2002-07-31 Mitsubishi Heavy Ind Ltd Gas turbine segment
FR2829525B1 (en) * 2001-09-13 2004-03-12 Snecma Moteurs ASSEMBLY OF SECTORS OF A TURBINE DISTRIBUTOR TO A CRANKCASE
US7094029B2 (en) * 2003-05-06 2006-08-22 General Electric Company Methods and apparatus for controlling gas turbine engine rotor tip clearances
DE102005013796A1 (en) * 2005-03-24 2006-09-28 Alstom Technology Ltd. Heat shield
DE102005013797A1 (en) * 2005-03-24 2006-09-28 Alstom Technology Ltd. Heat shield
JP4648139B2 (en) * 2005-09-14 2011-03-09 三菱重工業株式会社 Gas turbine blade tip clearance management structure
US7604456B2 (en) * 2006-04-11 2009-10-20 Siemens Energy, Inc. Vane shroud through-flow platform cover
ITMI20091872A1 (en) * 2009-10-28 2011-04-29 Alstom Technology Ltd "ENVELOPE SYSTEM FOR A STEAM TURBINE"
US9835171B2 (en) * 2010-08-20 2017-12-05 Siemens Energy, Inc. Vane carrier assembly
JP5751950B2 (en) 2011-06-20 2015-07-22 三菱日立パワーシステムズ株式会社 Gas turbine and gas turbine repair method
US20130330187A1 (en) * 2012-06-11 2013-12-12 General Electric Company Method and apparatus for mitigating out of roundness effects at a turbine
JP5461636B2 (en) * 2012-08-24 2014-04-02 三菱重工業株式会社 Turbine split ring
US9188062B2 (en) 2012-08-30 2015-11-17 Mitsubishi Hitachi Power Systems, Ltd. Gas turbine
US10451204B2 (en) * 2013-03-15 2019-10-22 United Technologies Corporation Low leakage duct segment using expansion joint assembly
DE102014202746A1 (en) * 2014-02-14 2015-08-20 Siemens Aktiengesellschaft Cast-in steel ring in cast iron housing for steam turbines
US10138749B2 (en) 2016-03-16 2018-11-27 United Technologies Corporation Seal anti-rotation feature
EP3330497B1 (en) * 2016-11-30 2019-06-26 Rolls-Royce Corporation Turbine shroud assembly with locating pads
US20180149030A1 (en) * 2016-11-30 2018-05-31 Rolls-Royce Corporation Turbine shroud with hanger attachment
DE102018210600A1 (en) * 2018-06-28 2020-01-02 MTU Aero Engines AG COAT RING ARRANGEMENT FOR A FLOWING MACHINE
US11111796B1 (en) * 2020-05-18 2021-09-07 Rolls-Royce North American Technologies Inc. Turbine shroud assembly with dovetail retention system

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3275294A (en) * 1963-11-14 1966-09-27 Westinghouse Electric Corp Elastic fluid apparatus
US3262677A (en) * 1963-11-27 1966-07-26 Gen Electric Stator assembly
US3341172A (en) * 1965-06-24 1967-09-12 Westinghouse Electric Corp Fluid machine casing sealing structure
US3427000A (en) * 1966-11-14 1969-02-11 Westinghouse Electric Corp Axial flow turbine structure
US3519366A (en) * 1968-05-22 1970-07-07 Westinghouse Electric Corp Turbine diaphragm seal structure
US3542483A (en) * 1968-07-17 1970-11-24 Westinghouse Electric Corp Turbine stator structure
US3529904A (en) * 1968-10-28 1970-09-22 Westinghouse Electric Corp Diaphragm seal structure
US3752598A (en) * 1971-11-17 1973-08-14 United Aircraft Corp Segmented duct seal
US3781125A (en) * 1972-04-07 1973-12-25 Westinghouse Electric Corp Gas turbine nozzle vane structure
US3841787A (en) * 1973-09-05 1974-10-15 Westinghouse Electric Corp Axial flow turbine structure

Also Published As

Publication number Publication date
JPS50155819A (en) 1975-12-16
IT1038116B (en) 1979-11-20
CA1015665A (en) 1977-08-16
US3892497A (en) 1975-07-01
FR2271400A1 (en) 1975-12-12
GB1476553A (en) 1977-06-16
FR2271400B3 (en) 1978-11-17

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