DE59205187D1 - Leitschaufeleinhängung für axialdurchströmte Turbomaschine - Google Patents

Leitschaufeleinhängung für axialdurchströmte Turbomaschine

Info

Publication number
DE59205187D1
DE59205187D1 DE59205187T DE59205187T DE59205187D1 DE 59205187 D1 DE59205187 D1 DE 59205187D1 DE 59205187 T DE59205187 T DE 59205187T DE 59205187 T DE59205187 T DE 59205187T DE 59205187 D1 DE59205187 D1 DE 59205187D1
Authority
DE
Germany
Prior art keywords
turbomachine
guide blade
blade attachment
axially flow
axially
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 - Fee Related
Application number
DE59205187T
Other languages
English (en)
Inventor
Kamil Matyscak
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.)
ABB Schweiz Holding AG
ABB AB
Original Assignee
Asea Brown Boveri AG Switzerland
Asea Brown Boveri AB
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 Asea Brown Boveri AG Switzerland, Asea Brown Boveri AB filed Critical Asea Brown Boveri AG Switzerland
Application granted granted Critical
Publication of DE59205187D1 publication Critical patent/DE59205187D1/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005—Sealing means between non relatively rotating elements
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246—Fastening of diaphragms or stator-rings
DE59205187T 1992-10-05 1992-10-05 Leitschaufeleinhängung für axialdurchströmte Turbomaschine Expired - Fee Related DE59205187D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP92116970A EP0591565B1 (de) 1992-10-05 1992-10-05 Leitschaufeleinhängung für axialdurchströmte Turbomaschine

Publications (1)

Publication Number Publication Date
DE59205187D1 true DE59205187D1 (de) 1996-03-07

Family

ID=8210100

Family Applications (1)

Application Number Title Priority Date Filing Date
DE59205187T Expired - Fee Related DE59205187D1 (de) 1992-10-05 1992-10-05 Leitschaufeleinhängung für axialdurchströmte Turbomaschine

Country Status (4)

Country Link
US (1) US5387082A (de)
EP (1) EP0591565B1 (de)
JP (1) JPH06193403A (de)
DE (1) DE59205187D1 (de)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4436731A1 (de) * 1994-10-14 1996-04-18 Abb Management Ag Verdichter
EP1118806A1 (de) * 2000-01-20 2001-07-25 Siemens Aktiengesellschaft Thermisch belastbare Wand und Verfahren zur Abdichtung eines Spaltes in einer thermisch belasteten Wand
US6808363B2 (en) * 2002-12-20 2004-10-26 General Electric Company Shroud segment and assembly with circumferential seal at a planar segment surface
US6893214B2 (en) * 2002-12-20 2005-05-17 General Electric Company Shroud segment and assembly with surface recessed seal bridging adjacent members
EP1443275B1 (de) * 2003-01-29 2008-08-13 Siemens Aktiengesellschaft Brennkammer
US7255929B2 (en) * 2003-12-12 2007-08-14 General Electric Company Use of spray coatings to achieve non-uniform seal clearances in turbomachinery
FR2902843A1 (fr) * 2006-06-23 2007-12-28 Snecma Sa Secteur de redresseur de compresseur ou secteur de distributeur de turbomachine
US7762766B2 (en) * 2006-07-06 2010-07-27 Siemens Energy, Inc. Cantilevered framework support for turbine vane
US8240045B2 (en) * 2007-05-22 2012-08-14 Siemens Energy, Inc. Gas turbine transition duct coupling apparatus
FR2918444B1 (fr) * 2007-07-05 2013-06-28 Snecma Deflecteur de fond de chambre, chambre de combustion le comportant et moteur a turbine a gaz en etant equipe
US8616007B2 (en) * 2009-01-22 2013-12-31 Siemens Energy, Inc. Structural attachment system for transition duct outlet
US8231338B2 (en) * 2009-05-05 2012-07-31 General Electric Company Turbine shell with pin support
DE102010024289A1 (de) 2010-04-23 2011-10-27 Carl Freudenberg Kg Gleitringdichtung
US8651809B2 (en) 2010-10-13 2014-02-18 General Electric Company Apparatus and method for aligning a turbine casing
EP2700798A1 (de) * 2012-08-21 2014-02-26 Siemens Aktiengesellschaft Strömungsmaschine umfassend einen Rotor und ein Gehäuse
DE102014202744A1 (de) * 2014-02-14 2015-08-20 Siemens Aktiengesellschaft Schutz vor Erosion und Erosionskorrosion an Stegen von Gußgehäusen
US9631507B2 (en) * 2014-07-14 2017-04-25 Siemens Energy, Inc. Gas turbine sealing band arrangement having a locking pin
US10030541B2 (en) 2015-07-01 2018-07-24 Rolls-Royce North American Technologies Inc. Turbine shroud with clamped flange attachment
US11466700B2 (en) * 2017-02-28 2022-10-11 Unison Industries, Llc Fan casing and mount bracket for oil cooler
DE102018210601A1 (de) * 2018-06-28 2020-01-02 MTU Aero Engines AG Segmentring zur montage in einer strömungsmaschine
DE102018210600A1 (de) * 2018-06-28 2020-01-02 MTU Aero Engines AG Mantelringanordnung für eine strömungsmaschine

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB647384A (en) * 1948-10-05 1950-12-13 English Electric Co Ltd Improvements in and relating to gas turbine blading
FR1003299A (fr) * 1949-12-13 1952-03-17 Rateau Soc Perfectionnement aux turbines à gaz et autres turbo-machines axiales
GB786689A (en) * 1955-11-09 1957-11-20 Gen Motors Corp Improvements relating to elastic-fluid turbines
GB904138A (en) * 1959-01-23 1962-08-22 Bristol Siddeley Engines Ltd Improvements in or relating to stator structures, for example for axial flow gas turbine engines
US3004700A (en) * 1959-08-18 1961-10-17 Gen Electric Turbine engine casing
US3427000A (en) * 1966-11-14 1969-02-11 Westinghouse Electric Corp Axial flow turbine structure
US3542483A (en) * 1968-07-17 1970-11-24 Westinghouse Electric Corp Turbine stator structure
US3892497A (en) * 1974-05-14 1975-07-01 Westinghouse Electric Corp Axial flow turbine stationary blade and blade ring locking arrangement
CS174516B1 (de) * 1974-09-26 1977-04-29
US3981609A (en) * 1975-06-02 1976-09-21 United Technologies Corporation Coolable blade tip shroud
US5224824A (en) * 1990-09-12 1993-07-06 United Technologies Corporation Compressor case construction

Also Published As

Publication number Publication date
EP0591565B1 (de) 1996-01-24
JPH06193403A (ja) 1994-07-12
EP0591565A1 (de) 1994-04-13
US5387082A (en) 1995-02-07

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee