AU2001290455A1 - Gas turbine stator - Google Patents

Gas turbine stator

Info

Publication number
AU2001290455A1
AU2001290455A1 AU2001290455A AU9045501A AU2001290455A1 AU 2001290455 A1 AU2001290455 A1 AU 2001290455A1 AU 2001290455 A AU2001290455 A AU 2001290455A AU 9045501 A AU9045501 A AU 9045501A AU 2001290455 A1 AU2001290455 A1 AU 2001290455A1
Authority
AU
Australia
Prior art keywords
gas turbine
stator
turbine stator
stator structure
distance
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.)
Abandoned
Application number
AU2001290455A
Inventor
Bertil Jonsson
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.)
GKN Aerospace Sweden AB
Original Assignee
Volvo Aero 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 Volvo Aero AB filed Critical Volvo Aero AB
Publication of AU2001290455A1 publication Critical patent/AU2001290455A1/en
Abandoned 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
    • 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
    • F01D17/165—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for radial flow, i.e. the vanes turning around axes which are essentially parallel to the rotor centre line

Abstract

Stator ( 1 ) for a gas turbine including a stator structure ( 2 ) having a continuous through-duct ( 3 ) for a gas through-flow, a circumferential member ( 6 ), which is arranged at a radial distance from the stator structure and is operatively coupled to the stator structure, and at least one member for maintaining the distance between the stator structure and the circumferential member. The spacing member has resilient characteristics in the radial direction of the stator.
AU2001290455A 2000-11-15 2001-09-25 Gas turbine stator Abandoned AU2001290455A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
SE0004215A SE519353C2 (en) 2000-11-15 2000-11-15 Stator for a gas turbine
SE0004215 2000-11-15
PCT/SE2001/002057 WO2002040832A1 (en) 2000-11-15 2001-09-25 Gas turbine stator

Publications (1)

Publication Number Publication Date
AU2001290455A1 true AU2001290455A1 (en) 2002-05-27

Family

ID=20281861

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2001290455A Abandoned AU2001290455A1 (en) 2000-11-15 2001-09-25 Gas turbine stator

Country Status (9)

Country Link
US (1) US7128527B2 (en)
EP (1) EP1337740B1 (en)
AT (1) ATE318367T1 (en)
AU (1) AU2001290455A1 (en)
CA (1) CA2427060C (en)
DE (1) DE60117393T2 (en)
RU (1) RU2278274C2 (en)
SE (1) SE519353C2 (en)
WO (1) WO2002040832A1 (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10351202A1 (en) * 2003-11-03 2005-06-02 Mtu Aero Engines Gmbh Device for adjusting vanes
DE102005040574A1 (en) * 2005-08-26 2007-03-15 Rolls-Royce Deutschland Ltd & Co Kg Gap control device for a gas turbine
ATE403798T1 (en) * 2006-01-02 2008-08-15 Siemens Ag DEVICE FOR SUPPORTING AN ADJUSTING RING AROUND A CIRCULAR BLADE CARRIER
JP5180807B2 (en) 2008-12-24 2013-04-10 三菱重工業株式会社 1st-stage stationary blade cooling structure and gas turbine
JP5479058B2 (en) * 2009-12-07 2014-04-23 三菱重工業株式会社 Communication structure between combustor and turbine section, and gas turbine
IT1401664B1 (en) * 2010-08-31 2013-08-02 Nuova Pignone S R L CENTERING DEVICE AND GUIDE RING SYSTEM.
DE102011086031B4 (en) * 2010-11-23 2016-02-04 Bosch Mahle Turbo Systems Gmbh & Co. Kg Variable turbine geometry
US9284851B2 (en) * 2012-02-21 2016-03-15 Mitsubishi Heavy Industries, Ltd. Axial-flow fluid machine, and variable vane drive device thereof
US20140314549A1 (en) * 2013-04-17 2014-10-23 General Electric Company Flow manipulating arrangement for a turbine exhaust diffuser

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2029859A1 (en) * 1970-06-18 1972-02-03 Motoren Turbinen Union Adjusting guide device for turbo machines
JPS597708A (en) * 1982-07-07 1984-01-14 Hitachi Ltd Mounting angle variable device of stationary blade in axial flow machine
DE3613344A1 (en) * 1986-04-19 1987-10-22 Pfeiffer Vakuumtechnik TURBOMOLECULAR VACUUM PUMP FOR HIGHER PRESSURE
DE3623001C1 (en) * 1986-07-09 1987-07-09 Mtu Muenchen Gmbh Adjustment device for swiveling guide vanes of turbo engines
DE4102188C2 (en) * 1991-01-25 1994-09-22 Mtu Muenchen Gmbh Guide vane adjustment device of a turbine of a gas turbine engine
US5672047A (en) * 1995-04-12 1997-09-30 Dresser-Rand Company Adjustable stator vanes for turbomachinery

Also Published As

Publication number Publication date
RU2278274C2 (en) 2006-06-20
SE0004215D0 (en) 2000-11-15
DE60117393T2 (en) 2006-11-02
US20030165384A1 (en) 2003-09-04
US7128527B2 (en) 2006-10-31
EP1337740B1 (en) 2006-02-22
SE0004215L (en) 2002-05-16
CA2427060A1 (en) 2002-05-23
ATE318367T1 (en) 2006-03-15
EP1337740A1 (en) 2003-08-27
CA2427060C (en) 2008-12-09
WO2002040832A1 (en) 2002-05-23
RU2003115424A (en) 2005-01-20
DE60117393D1 (en) 2006-04-27
SE519353C2 (en) 2003-02-18

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