GB1476553A - Gas turbine - Google Patents

Gas turbine

Info

Publication number
GB1476553A
GB1476553A GB2010275A GB2010275A GB1476553A GB 1476553 A GB1476553 A GB 1476553A GB 2010275 A GB2010275 A GB 2010275A GB 2010275 A GB2010275 A GB 2010275A GB 1476553 A GB1476553 A GB 1476553A
Authority
GB
United Kingdom
Prior art keywords
segments
plates
ring segments
casings
support segments
Prior art date
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
GB2010275A
Other languages
English (en)
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 GB1476553A publication Critical patent/GB1476553A/en
Expired legal-status Critical Current

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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; 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)
GB2010275A 1974-05-14 1975-05-13 Gas turbine Expired GB1476553A (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 (1)

Publication Number Publication Date
GB1476553A true GB1476553A (en) 1977-06-16

Family

ID=23865587

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2010275A Expired GB1476553A (en) 1974-05-14 1975-05-13 Gas turbine

Country Status (6)

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

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2948979A1 (de) * 1978-12-20 1980-07-10 United Technologies Corp Tragvorrichtung fuer die laufschaufelspitzenabdichtung in einem gasturbinentriebwerk
GB2228539A (en) * 1989-02-23 1990-08-29 United Technologies Corp Stator assembly for a rotary machine

Families Citing this family (55)

* 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 (de) * 1976-04-17 1985-09-26 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Gasturbinentriebwerk
DE2907748C2 (de) * 1979-02-28 1987-02-12 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Einrichtung zur Minimierung und Konstanthaltung des Schaufelspitzenspiels einer axial durchströmten Hochdruckturbine eines Gasturbinentriebwerks
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 (de) * 1983-09-16 1985-02-14 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Einrichtung zur Axial- und Umfangssicherung von statischen Gehaeusebauteilen fuer Stroemungsmaschinen
IT1167241B (it) * 1983-10-03 1987-05-13 Nuovo Pignone Spa Sistema perfezionato per il fissaggio degli ugelli statorici alla cassa di una turbina di potenza
US4688988A (en) * 1984-12-17 1987-08-25 United Technologies Corporation Coolable stator assembly for a gas turbine engine
FR2577281B1 (fr) * 1985-02-13 1987-03-20 Snecma Carter de turbomachine associe a un dispositif pour ajuster le jeu entre aubes mobiles et carter
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 (fr) * 1986-11-26 1990-05-04 Snecma Carter de compresseur adapte pour le pilotage actif de ses dilatations et son procede de fabrication
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
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 (sv) * 1992-04-01 1994-08-22 Abb Carbon Ab Sätt och anordning för montering av axialströmningsmaskin
DE59205187D1 (de) * 1992-10-05 1996-03-07 Asea Brown Boveri Leitschaufeleinhängung für axialdurchströmte Turbomaschine
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
EP0919700B1 (en) * 1997-06-19 2004-09-01 Mitsubishi Heavy Industries, Ltd. Device for sealing gas turbine stator blades
WO2000057033A1 (de) 1999-03-24 2000-09-28 Siemens Aktiengesellschaft Abdeckelement und anordnung mit einem abdeckelement und mit einer tragstruktur
US6343912B1 (en) * 1999-12-07 2002-02-05 General Electric Company Gas turbine or jet engine stator vane frame
JP2002213207A (ja) * 2001-01-15 2002-07-31 Mitsubishi Heavy Ind Ltd ガスタービン分割環
FR2829525B1 (fr) * 2001-09-13 2004-03-12 Snecma Moteurs Assemblage de secteurs d'un distributeur de turbine a un carter
US7094029B2 (en) * 2003-05-06 2006-08-22 General Electric Company Methods and apparatus for controlling gas turbine engine rotor tip clearances
DE102005013797A1 (de) * 2005-03-24 2006-09-28 Alstom Technology Ltd. Wärmestausegment
DE102005013796A1 (de) * 2005-03-24 2006-09-28 Alstom Technology Ltd. Wärmestausegment
JP4648139B2 (ja) * 2005-09-14 2011-03-09 三菱重工業株式会社 ガスタービンの翼端隙間管理構造
US7604456B2 (en) * 2006-04-11 2009-10-20 Siemens Energy, Inc. Vane shroud through-flow platform cover
ITMI20091872A1 (it) * 2009-10-28 2011-04-29 Alstom Technology Ltd "sistema di involucri per una turbina a vapore"
US9835171B2 (en) * 2010-08-20 2017-12-05 Siemens Energy, Inc. Vane carrier assembly
JP5751950B2 (ja) 2011-06-20 2015-07-22 三菱日立パワーシステムズ株式会社 ガスタービン及びガスタービンの補修方法
US20130330187A1 (en) * 2012-06-11 2013-12-12 General Electric Company Method and apparatus for mitigating out of roundness effects at a turbine
JP5461636B2 (ja) * 2012-08-24 2014-04-02 三菱重工業株式会社 タービン分割環
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 (de) * 2014-02-14 2015-08-20 Siemens Aktiengesellschaft Eingegossener Stahlring in Eisengussgehäuse für Dampfturbinen
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
EP3330498B1 (en) * 2016-11-30 2020-01-08 Rolls-Royce Corporation Turbine shroud with hanger attachment
DE102018210600A1 (de) * 2018-06-28 2020-01-02 MTU Aero Engines AG Mantelringanordnung für eine strömungsmaschine
CN109113798A (zh) * 2018-08-27 2019-01-01 广东惠州天然气发电有限公司 一种新型燃气轮机静叶环
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

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2948979A1 (de) * 1978-12-20 1980-07-10 United Technologies Corp Tragvorrichtung fuer die laufschaufelspitzenabdichtung in einem gasturbinentriebwerk
GB2228539A (en) * 1989-02-23 1990-08-29 United Technologies Corp Stator assembly for a rotary machine
GB2228539B (en) * 1989-02-23 1993-09-01 United Technologies Corp Casing for a rotary machine

Also Published As

Publication number Publication date
JPS50155819A (ja) 1975-12-16
FR2271400A1 (ja) 1975-12-12
CA1015665A (en) 1977-08-16
US3892497A (en) 1975-07-01
FR2271400B3 (ja) 1978-11-17
JPS5330847B2 (ja) 1978-08-30
IT1038116B (it) 1979-11-20

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19930513