DE60121558D1 - Gasturbinengehäuse - Google Patents

Gasturbinengehäuse

Info

Publication number
DE60121558D1
DE60121558D1 DE60121558T DE60121558T DE60121558D1 DE 60121558 D1 DE60121558 D1 DE 60121558D1 DE 60121558 T DE60121558 T DE 60121558T DE 60121558 T DE60121558 T DE 60121558T DE 60121558 D1 DE60121558 D1 DE 60121558D1
Authority
DE
Germany
Prior art keywords
gas turbine
turbine housing
housing
gas
turbine
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 - Lifetime
Application number
DE60121558T
Other languages
English (en)
Other versions
DE60121558T2 (de
Inventor
Daniel Toomey
Ellis Clouse
Thomas Hogan
Robert Jacobson
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Application granted granted Critical
Publication of DE60121558D1 publication Critical patent/DE60121558D1/de
Publication of DE60121558T2 publication Critical patent/DE60121558T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • 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
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/16—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means
    • F01D11/18—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means using stator or rotor components with predetermined thermal response, e.g. selective insulation, thermal inertia, differential expansion
    • 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
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line
    • 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
    • F01D25/243—Flange connections; Bolting arrangements
DE60121558T 2000-03-29 2001-03-23 Gasturbinengehäuse Expired - Lifetime DE60121558T2 (de)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US19282900P 2000-03-29 2000-03-29
US192829P 2000-03-29
US715325 2000-11-17
US09/715,325 US6439842B1 (en) 2000-03-29 2000-11-17 Gas turbine engine stator case
PCT/US2001/009415 WO2001073268A1 (en) 2000-03-29 2001-03-23 Gas turbine engine stator case

Publications (2)

Publication Number Publication Date
DE60121558D1 true DE60121558D1 (de) 2006-08-31
DE60121558T2 DE60121558T2 (de) 2007-06-21

Family

ID=26888408

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60121558T Expired - Lifetime DE60121558T2 (de) 2000-03-29 2001-03-23 Gasturbinengehäuse

Country Status (5)

Country Link
US (1) US6439842B1 (de)
EP (1) EP1268982B1 (de)
JP (1) JP5095062B2 (de)
DE (1) DE60121558T2 (de)
WO (1) WO2001073268A1 (de)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0411850D0 (en) * 2004-05-27 2004-06-30 Rolls Royce Plc Spacing arrangement
GB0425595D0 (en) * 2004-11-20 2004-12-22 Rolls Royce Plc A laminate material
US7652489B2 (en) * 2005-12-06 2010-01-26 General Electric Company Multi-range clearance measurement system and method of operation
GB2442238B (en) * 2006-09-29 2008-10-01 Rolls Royce Plc Sheet metal blank
US8092168B2 (en) * 2009-04-10 2012-01-10 General Electric Company Patch plug repair of a compressor case stator ring hook, near the horizontal joint
EP2900941B1 (de) * 2012-09-26 2016-12-14 United Technologies Corporation Kombination aus hochdruckturbinengehäuse und turbinenzwischengehäuse
GB201309580D0 (en) * 2013-05-29 2013-07-10 Siemens Ag Rotor tip clearance
FR3008912B1 (fr) * 2013-07-29 2017-12-15 Snecma Carter de turbomachine et procede de fabrication
EP3009604B1 (de) 2014-09-19 2018-08-08 United Technologies Corporation Radial befestigtes fest-verstellbares schaufelsystem

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE471415A (de) * 1946-02-25
US4264274A (en) 1977-12-27 1981-04-28 United Technologies Corporation Apparatus maintaining rotor and stator clearance
DE3315914A1 (de) * 1983-05-02 1984-11-08 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Gasturbinentriebwerk mit einrichtungen zur schaufelspaltminimierung
US4893983A (en) 1988-04-07 1990-01-16 General Electric Company Clearance control system
US5063661A (en) * 1990-07-05 1991-11-12 The United States Of America As Represented By The Secretary Of The Air Force Method of fabricating a split compressor case
US5211537A (en) * 1992-03-02 1993-05-18 United Technologies Corporation Compressor vane lock
JPH07208110A (ja) * 1994-01-06 1995-08-08 Ishikawajima Harima Heavy Ind Co Ltd 分割式タービンケーシングの構造
FR2766231B1 (fr) 1997-07-18 1999-08-20 Snecma Dispositif d'echauffement ou de refroidissement d'un carter circulaire

Also Published As

Publication number Publication date
DE60121558T2 (de) 2007-06-21
EP1268982A1 (de) 2003-01-02
JP5095062B2 (ja) 2012-12-12
JP2003529015A (ja) 2003-09-30
US6439842B1 (en) 2002-08-27
EP1268982B1 (de) 2006-07-19
WO2001073268A1 (en) 2001-10-04

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition