FR2831615B1 - Redresseur fixe sectorise pour compresseur d'une turbomachine - Google Patents

Redresseur fixe sectorise pour compresseur d'une turbomachine

Info

Publication number
FR2831615B1
FR2831615B1 FR0114102A FR0114102A FR2831615B1 FR 2831615 B1 FR2831615 B1 FR 2831615B1 FR 0114102 A FR0114102 A FR 0114102A FR 0114102 A FR0114102 A FR 0114102A FR 2831615 B1 FR2831615 B1 FR 2831615B1
Authority
FR
France
Prior art keywords
turbomachine compressor
fixed rectifier
sectorized
sectorized fixed
rectifier
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
FR0114102A
Other languages
English (en)
Other versions
FR2831615A1 (fr
Inventor
Jean Louis Bertrand
Jean Marc Claude Perrollaz
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA Moteurs SA
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 FR0114102A priority Critical patent/FR2831615B1/fr
Application filed by SNECMA Moteurs SA filed Critical SNECMA Moteurs SA
Priority to JP2002309259A priority patent/JP4181375B2/ja
Priority to DE60214106T priority patent/DE60214106T2/de
Priority to EP02292634A priority patent/EP1308630B1/fr
Priority to ES02292634T priority patent/ES2266430T3/es
Priority to CA2409972A priority patent/CA2409972C/fr
Priority to RU2002129117/06A priority patent/RU2287090C2/ru
Priority to US10/283,279 priority patent/US6890151B2/en
Priority to UA2002108634A priority patent/UA75069C2/uk
Publication of FR2831615A1 publication Critical patent/FR2831615A1/fr
Application granted granted Critical
Publication of FR2831615B1 publication Critical patent/FR2831615B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246Fastening of diaphragms or stator-rings
    • 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
    • F01D9/042Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/52Casings; Connections of working fluid for axial pumps
    • F04D29/54Fluid-guiding means, e.g. diffusers
    • F04D29/541Specially adapted for elastic fluid pumps
    • F04D29/542Bladed diffusers
FR0114102A 2001-10-31 2001-10-31 Redresseur fixe sectorise pour compresseur d'une turbomachine Expired - Fee Related FR2831615B1 (fr)

Priority Applications (9)

Application Number Priority Date Filing Date Title
FR0114102A FR2831615B1 (fr) 2001-10-31 2001-10-31 Redresseur fixe sectorise pour compresseur d'une turbomachine
DE60214106T DE60214106T2 (de) 2001-10-31 2002-10-24 Statorsektor für einen Verdichter eines Turbotriebwerks
EP02292634A EP1308630B1 (fr) 2001-10-31 2002-10-24 Redresseur fixe sectorisé pour compresseur d'une turbomachine
ES02292634T ES2266430T3 (es) 2001-10-31 2002-10-24 Rectificador fijo sectorizado para compresor de una turbomaquina.
JP2002309259A JP4181375B2 (ja) 2001-10-31 2002-10-24 ターボ機械コンプレッサのための複数セクタに分かれた固定式ガイドベーン組立体
CA2409972A CA2409972C (fr) 2001-10-31 2002-10-28 Distributeur fixe separe en secteurs pour compresseur de turbomachine
RU2002129117/06A RU2287090C2 (ru) 2001-10-31 2002-10-30 Узел неподвижной лопатки, разделенный на секторы, для компрессора турбомашины
US10/283,279 US6890151B2 (en) 2001-10-31 2002-10-30 Fixed guide vane assembly separated into sectors for a turbomachine compressor
UA2002108634A UA75069C2 (en) 2001-10-31 2002-10-30 Fixed guide vane assembly separated into sectors for compressor of turbo-machine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0114102A FR2831615B1 (fr) 2001-10-31 2001-10-31 Redresseur fixe sectorise pour compresseur d'une turbomachine

Publications (2)

Publication Number Publication Date
FR2831615A1 FR2831615A1 (fr) 2003-05-02
FR2831615B1 true FR2831615B1 (fr) 2004-01-02

Family

ID=8868935

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0114102A Expired - Fee Related FR2831615B1 (fr) 2001-10-31 2001-10-31 Redresseur fixe sectorise pour compresseur d'une turbomachine

Country Status (9)

Country Link
US (1) US6890151B2 (fr)
EP (1) EP1308630B1 (fr)
JP (1) JP4181375B2 (fr)
CA (1) CA2409972C (fr)
DE (1) DE60214106T2 (fr)
ES (1) ES2266430T3 (fr)
FR (1) FR2831615B1 (fr)
RU (1) RU2287090C2 (fr)
UA (1) UA75069C2 (fr)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2859509B1 (fr) * 2003-09-10 2006-01-13 Snecma Moteurs Arret en rotation des secteurs d'aubes de redresseurs par des barrettes dans les plans de joint du carter
US7033135B2 (en) * 2003-11-10 2006-04-25 General Electric Company Method and apparatus for distributing fluid into a turbomachine
US7144218B2 (en) * 2004-04-19 2006-12-05 United Technologies Corporation Anti-rotation lock
FR2878293B1 (fr) * 2004-11-24 2009-08-21 Snecma Moteurs Sa Montage de secteurs de distributeur dans un compresseur axial
JP4918263B2 (ja) * 2006-01-27 2012-04-18 三菱重工業株式会社 軸流圧縮機の静翼環
US20080025838A1 (en) * 2006-07-25 2008-01-31 Siemens Power Generation, Inc. Ring seal for a turbine engine
US8128354B2 (en) * 2007-01-17 2012-03-06 Siemens Energy, Inc. Gas turbine engine
FR2913052B1 (fr) * 2007-02-22 2011-04-01 Snecma Commande des aubes a angle de calage variable
EP2211023A1 (fr) * 2009-01-21 2010-07-28 Siemens Aktiengesellschaft Distributeur pour turbomachine avec structure support d'aubes directrices segmentée
GB2468848B (en) * 2009-03-23 2011-10-26 Rolls Royce Plc An assembly for a turbomachine
FR2948736B1 (fr) * 2009-07-31 2011-09-23 Snecma Secteur de virole exterieure pour couronne aubagee de stator de turbomachine d'aeronef, comprenant des cales amortisseuses de vibrations
EP2339120B1 (fr) * 2009-12-22 2015-07-08 Techspace Aero S.A. Étage redresseur de turbomachine et compresseur associé
US8454303B2 (en) * 2010-01-14 2013-06-04 General Electric Company Turbine nozzle assembly
US20110243725A1 (en) * 2010-03-31 2011-10-06 General Electric Company Turbine shroud mounting apparatus with anti-rotation feature
FR2975124B1 (fr) * 2011-05-09 2013-05-24 Snecma Virole annulaire de moteur d'aeronef comportant une fenetre d'introduction d'aubes
US9074489B2 (en) 2012-03-26 2015-07-07 Pratt & Whitney Canada Corp. Connector assembly for variable inlet guide vanes and method
US10428832B2 (en) 2012-08-06 2019-10-01 United Technologies Corporation Stator anti-rotation lug
US10309235B2 (en) 2012-08-27 2019-06-04 United Technologies Corporation Shiplap cantilevered stator
US9353767B2 (en) 2013-01-08 2016-05-31 United Technologies Corporation Stator anti-rotation device
US9745864B2 (en) * 2014-04-16 2017-08-29 United Technologies Corporation Systems and methods for anti-rotational features
US10190434B2 (en) * 2014-10-29 2019-01-29 Rolls-Royce North American Technologies Inc. Turbine shroud with locating inserts
PL3215715T3 (pl) * 2014-11-03 2021-03-08 Nuovo Pignone S.R.L. Sektor montażu stopnia turbiny i odpowiadający sposób wytwarzania
BE1023619B1 (fr) * 2015-06-26 2017-05-18 Safran Aero Boosters S.A. Carter de compresseur de turbomachine axiale
US20190309641A1 (en) * 2018-04-04 2019-10-10 United Technologies Corporation Gas turbine engine having cantilevered stators with sealing members

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2945290A (en) * 1957-09-16 1960-07-19 Gen Electric Stator vane half ring assemblies
US3365173A (en) * 1966-02-28 1968-01-23 Gen Electric Stator structure
US4126914A (en) 1976-06-22 1978-11-28 Cotton, Incorporated Process and apparatus for treating fibrous materials for subsequent processing
US4126405A (en) 1976-12-16 1978-11-21 General Electric Company Turbine nozzle
US4889470A (en) * 1988-08-01 1989-12-26 Westinghouse Electric Corp. Compressor diaphragm assembly
US5197856A (en) * 1991-06-24 1993-03-30 General Electric Company Compressor stator
US5141395A (en) * 1991-09-05 1992-08-25 General Electric Company Flow activated flowpath liner seal
FR2728015B1 (fr) 1994-12-07 1997-01-17 Snecma Distributeur monobloc sectorise d'un stator de turbine de turbomachine
US5846050A (en) * 1997-07-14 1998-12-08 General Electric Company Vane sector spring
US6296443B1 (en) * 1999-12-03 2001-10-02 General Electric Company Vane sector seating spring and method of retaining same

Also Published As

Publication number Publication date
EP1308630A1 (fr) 2003-05-07
DE60214106T2 (de) 2007-04-12
JP2003161297A (ja) 2003-06-06
FR2831615A1 (fr) 2003-05-02
UA75069C2 (en) 2006-03-15
US20030082051A1 (en) 2003-05-01
CA2409972A1 (fr) 2003-04-30
US6890151B2 (en) 2005-05-10
RU2287090C2 (ru) 2006-11-10
JP4181375B2 (ja) 2008-11-12
EP1308630B1 (fr) 2006-08-23
DE60214106D1 (de) 2006-10-05
ES2266430T3 (es) 2007-03-01
CA2409972C (fr) 2011-04-12

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Legal Events

Date Code Title Description
CD Change of name or company name
ST Notification of lapse

Effective date: 20080630