DE69926979D1 - Leitschaufelbefestigung - Google Patents

Leitschaufelbefestigung

Info

Publication number
DE69926979D1
DE69926979D1 DE69926979T DE69926979T DE69926979D1 DE 69926979 D1 DE69926979 D1 DE 69926979D1 DE 69926979 T DE69926979 T DE 69926979T DE 69926979 T DE69926979 T DE 69926979T DE 69926979 D1 DE69926979 D1 DE 69926979D1
Authority
DE
Germany
Prior art keywords
leitschaufelbefestigung
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
DE69926979T
Other languages
English (en)
Other versions
DE69926979T2 (de
Inventor
Konstantino Kouris
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies 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
Priority to US218351 priority Critical
Priority to US09/218,351 priority patent/US6164903A/en
Application filed by United Technologies Corp filed Critical United Technologies Corp
Publication of DE69926979D1 publication Critical patent/DE69926979D1/de
Application granted granted Critical
Publication of DE69926979T2 publication Critical patent/DE69926979T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
DE69926979T 1998-12-22 1999-11-03 Leitschaufelbefestigung Expired - Lifetime DE69926979T2 (de)

Priority Applications (2)

Application Number Priority Date Filing Date Title
US218351 1998-12-22
US09/218,351 US6164903A (en) 1998-12-22 1998-12-22 Turbine vane mounting arrangement

Publications (2)

Publication Number Publication Date
DE69926979D1 true DE69926979D1 (de) 2005-10-06
DE69926979T2 DE69926979T2 (de) 2006-06-29

Family

ID=22814764

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69926979T Expired - Lifetime DE69926979T2 (de) 1998-12-22 1999-11-03 Leitschaufelbefestigung

Country Status (4)

Country Link
US (1) US6164903A (de)
EP (1) EP1013885B1 (de)
JP (1) JP2000186506A (de)
DE (1) DE69926979T2 (de)

Families Citing this family (45)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6513781B1 (en) * 1998-08-12 2003-02-04 ETN Präzisionstechnik GmbH Support devices for the vanes of power units
EP1069281B1 (de) * 1999-07-16 2005-07-27 General Electric Company Vorgespannte Gasturbinenleitschaufel
US6375415B1 (en) * 2000-04-25 2002-04-23 General Electric Company Hook support for a closed circuit fluid cooled gas turbine nozzle stage segment
DE10161292A1 (de) * 2001-12-13 2003-06-26 Rolls Royce Deutschland Lagerring zur Lagerung von Schaufelfüßen von verstellbaren Statorschaufeln im Hochdruckverdichter einer Gasturbine
US6709230B2 (en) * 2002-05-31 2004-03-23 Siemens Westinghouse Power Corporation Ceramic matrix composite gas turbine vane
US6648597B1 (en) 2002-05-31 2003-11-18 Siemens Westinghouse Power Corporation Ceramic matrix composite turbine vane
US6854960B2 (en) 2002-06-24 2005-02-15 Electric Boat Corporation Segmented composite impeller/propeller arrangement and manufacturing method
US7093359B2 (en) 2002-09-17 2006-08-22 Siemens Westinghouse Power Corporation Composite structure formed by CMC-on-insulation process
US9068464B2 (en) * 2002-09-17 2015-06-30 Siemens Energy, Inc. Method of joining ceramic parts and articles so formed
US6884030B2 (en) * 2002-12-20 2005-04-26 General Electric Company Methods and apparatus for securing multi-piece nozzle assemblies
US6968702B2 (en) * 2003-12-08 2005-11-29 Ingersoll-Rand Energy Systems Corporation Nozzle bolting arrangement for a turbine
US7066717B2 (en) * 2004-04-22 2006-06-27 Siemens Power Generation, Inc. Ceramic matrix composite airfoil trailing edge arrangement
JP3892859B2 (ja) * 2004-05-31 2007-03-14 川崎重工業株式会社 タービンノズルの支持構造
US7104756B2 (en) * 2004-08-11 2006-09-12 United Technologies Corporation Temperature tolerant vane assembly
US7435058B2 (en) * 2005-01-18 2008-10-14 Siemens Power Generation, Inc. Ceramic matrix composite vane with chordwise stiffener
US7326030B2 (en) * 2005-02-02 2008-02-05 Siemens Power Generation, Inc. Support system for a composite airfoil in a turbine engine
US7452182B2 (en) * 2005-04-07 2008-11-18 Siemens Energy, Inc. Multi-piece turbine vane assembly
US7909569B2 (en) * 2005-06-09 2011-03-22 Pratt & Whitney Canada Corp. Turbine support case and method of manufacturing
US7563071B2 (en) * 2005-08-04 2009-07-21 Siemens Energy, Inc. Pin-loaded mounting apparatus for a refractory component in a combustion turbine engine
US7648336B2 (en) * 2006-01-03 2010-01-19 General Electric Company Apparatus and method for assembling a gas turbine stator
DE102006024085B4 (de) * 2006-05-23 2020-04-16 MTU Aero Engines AG Turboverdichter in Axialbauweise
US7722317B2 (en) * 2007-01-25 2010-05-25 Siemens Energy, Inc. CMC to metal attachment mechanism
FR2917458B1 (fr) * 2007-06-13 2009-09-25 Snecma Sa Moyeu de carter d'echappement comportant des nervures de repartition de contraintes
US20090016871A1 (en) * 2007-07-10 2009-01-15 United Technologies Corp. Systems and Methods Involving Variable Vanes
US8197209B2 (en) * 2007-12-19 2012-06-12 United Technologies Corp. Systems and methods involving variable throat area vanes
US8388307B2 (en) * 2009-07-21 2013-03-05 Honeywell International Inc. Turbine nozzle assembly including radially-compliant spring member for gas turbine engine
US8256088B2 (en) * 2009-08-24 2012-09-04 Siemens Energy, Inc. Joining mechanism with stem tension and interlocked compression ring
US8500392B2 (en) * 2009-10-01 2013-08-06 Pratt & Whitney Canada Corp. Sealing for vane segments
WO2011053198A1 (en) * 2009-10-27 2011-05-05 Volvo Aero Corporation Gas turbine engine component
US8966755B2 (en) 2011-01-20 2015-03-03 United Technologies Corporation Assembly fixture for a stator vane assembly
EP2859189B1 (de) * 2012-05-30 2017-12-27 United Technologies Corporation Montagearmatur für leitschaufelanordnung
FR2974593B1 (fr) * 2011-04-28 2015-11-13 Snecma Moteur a turbine comportant une protection metallique d'une piece composite
US9335051B2 (en) * 2011-07-13 2016-05-10 United Technologies Corporation Ceramic matrix composite combustor vane ring assembly
FR2978197B1 (fr) * 2011-07-22 2015-12-25 Snecma Distributeur de turbine de turbomachine et turbine comportant un tel distributeur
US9127557B2 (en) * 2012-06-08 2015-09-08 General Electric Company Nozzle mounting and sealing assembly for a gas turbine system and method of mounting and sealing
US9546557B2 (en) * 2012-06-29 2017-01-17 General Electric Company Nozzle, a nozzle hanger, and a ceramic to metal attachment system
US9447693B2 (en) 2012-07-30 2016-09-20 United Technologies Corporation Compliant assembly
US9970307B2 (en) * 2014-03-19 2018-05-15 Honeywell International Inc. Turbine nozzles with slip joints impregnated by oxidation-resistant sealing material and methods for the production thereof
US10072516B2 (en) * 2014-09-24 2018-09-11 United Technologies Corporation Clamped vane arc segment having load-transmitting features
US9970317B2 (en) * 2014-10-31 2018-05-15 Rolls-Royce North America Technologies Inc. Vane assembly for a gas turbine engine
US9845692B2 (en) * 2015-05-05 2017-12-19 General Electric Company Turbine component connection with thermally stress-free fastener
US20170051619A1 (en) * 2015-08-18 2017-02-23 General Electric Company Cmc nozzles with split endwalls for gas turbine engines
US10570760B2 (en) * 2017-04-13 2020-02-25 General Electric Company Turbine nozzle with CMC aft band
US10301953B2 (en) 2017-04-13 2019-05-28 General Electric Company Turbine nozzle with CMC aft Band
US10458260B2 (en) * 2017-05-24 2019-10-29 General Electric Company Nozzle airfoil decoupled from and attached outside of flow path boundary

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2914300A (en) * 1955-12-22 1959-11-24 Gen Electric Nozzle vane support for turbines
US3394919A (en) * 1966-11-22 1968-07-30 North American Rockwell Floating hot fluid turbine nozzle ring
US3966353A (en) * 1975-02-21 1976-06-29 Westinghouse Electric Corporation Ceramic-to-metal (or ceramic) cushion/seal for use with three piece ceramic stationary vane assembly
JPH0425404B2 (de) * 1984-09-10 1992-04-30 Mitsubishi Heavy Ind Ltd
JPH076366B2 (ja) * 1985-08-20 1995-01-30 三菱重工業株式会社 ガスタ−ビン静翼
JPS63223302A (en) * 1987-03-13 1988-09-16 Hitachi Ltd Ceramics stationary blade for gas turbine
US4907946A (en) * 1988-08-10 1990-03-13 General Electric Company Resiliently mounted outlet guide vane
US4987736A (en) * 1988-12-14 1991-01-29 General Electric Company Lightweight gas turbine engine frame with free-floating heat shield
GB2236809B (en) * 1989-09-22 1994-03-16 Rolls Royce Plc Improvements in or relating to gas turbine engines
JP2777609B2 (ja) * 1989-09-27 1998-07-23 株式会社日立製作所 セラミック静翼
US5634767A (en) * 1996-03-29 1997-06-03 General Electric Company Turbine frame having spindle mounted liner
US5630700A (en) * 1996-04-26 1997-05-20 General Electric Company Floating vane turbine nozzle
US6000906A (en) * 1997-09-12 1999-12-14 Alliedsignal Inc. Ceramic airfoil

Also Published As

Publication number Publication date
EP1013885B1 (de) 2005-08-31
EP1013885A2 (de) 2000-06-28
US6164903A (en) 2000-12-26
DE69926979T2 (de) 2006-06-29
JP2000186506A (ja) 2000-07-04
EP1013885A3 (de) 2001-08-01

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition