FR2732416B1 - Agencement de raccordement de deux secteurs angulaires de turbomachine et joint concu pour servir dans cet agencement - Google Patents

Agencement de raccordement de deux secteurs angulaires de turbomachine et joint concu pour servir dans cet agencement

Info

Publication number
FR2732416B1
FR2732416B1 FR9503666A FR9503666A FR2732416B1 FR 2732416 B1 FR2732416 B1 FR 2732416B1 FR 9503666 A FR9503666 A FR 9503666A FR 9503666 A FR9503666 A FR 9503666A FR 2732416 B1 FR2732416 B1 FR 2732416B1
Authority
FR
France
Prior art keywords
arrangement
turbomachine
angular sectors
joint designed
connection arrangement
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
FR9503666A
Other languages
English (en)
Other versions
FR2732416A1 (fr
Inventor
Josette Benoist
Paul Martyez
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
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Priority to FR9503666A priority Critical patent/FR2732416B1/fr
Priority to US08/618,720 priority patent/US5707207A/en
Priority to DE69600179T priority patent/DE69600179T2/de
Priority to EP96400661A priority patent/EP0735242B1/fr
Publication of FR2732416A1 publication Critical patent/FR2732416A1/fr
Application granted granted Critical
Publication of FR2732416B1 publication Critical patent/FR2732416B1/fr
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
FR9503666A 1995-03-29 1995-03-29 Agencement de raccordement de deux secteurs angulaires de turbomachine et joint concu pour servir dans cet agencement Expired - Fee Related FR2732416B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR9503666A FR2732416B1 (fr) 1995-03-29 1995-03-29 Agencement de raccordement de deux secteurs angulaires de turbomachine et joint concu pour servir dans cet agencement
US08/618,720 US5707207A (en) 1995-03-29 1996-03-20 Layout for connecting two angular sectors of a turbomachine, and seal designed for use in this layout
DE69600179T DE69600179T2 (de) 1995-03-29 1996-03-28 Dichtung zwischen Segmenten eines Leitschaufelkranzes
EP96400661A EP0735242B1 (fr) 1995-03-29 1996-03-28 Agencement de raccordement de deux secteurs angulaires de turbomachine et joint conçu pour servir dans cet agencement

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9503666A FR2732416B1 (fr) 1995-03-29 1995-03-29 Agencement de raccordement de deux secteurs angulaires de turbomachine et joint concu pour servir dans cet agencement

Publications (2)

Publication Number Publication Date
FR2732416A1 FR2732416A1 (fr) 1996-10-04
FR2732416B1 true FR2732416B1 (fr) 1997-04-30

Family

ID=9477529

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9503666A Expired - Fee Related FR2732416B1 (fr) 1995-03-29 1995-03-29 Agencement de raccordement de deux secteurs angulaires de turbomachine et joint concu pour servir dans cet agencement

Country Status (4)

Country Link
US (1) US5707207A (fr)
EP (1) EP0735242B1 (fr)
DE (1) DE69600179T2 (fr)
FR (1) FR2732416B1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112243472A (zh) * 2018-05-23 2021-01-19 赛峰飞机发动机公司 在其之间具有密封件的涡轮机叶片成角度部段

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6042334A (en) * 1998-08-17 2000-03-28 General Electric Company Compressor interstage seal
US6425736B1 (en) * 1999-08-09 2002-07-30 United Technologies Corporation Stator assembly for a rotary machine and method for making the stator assembly
DE10047307A1 (de) * 2000-09-25 2002-08-01 Alstom Switzerland Ltd Dichtungsanordnung
US20040239040A1 (en) * 2003-05-29 2004-12-02 Burdgick Steven Sebastian Nozzle interstage seal for steam turbines
US7438524B2 (en) * 2005-07-20 2008-10-21 United Technologies Corporation Winged structural joint and articles employing the joint
DE102009016803A1 (de) * 2009-04-09 2010-10-14 Rolls-Royce Deutschland Ltd & Co Kg Labyrinth-Anstreifdichtung für eine Strömungsmaschine
JP2012102831A (ja) * 2010-11-12 2012-05-31 Hitachi Ltd ラビリンスシール装置、およびそれを用いたターボ機械
GB2489693B (en) * 2011-04-04 2014-10-01 Rolls Royce Plc Abradable liner
JPWO2014077058A1 (ja) * 2012-11-13 2017-01-05 三菱重工コンプレッサ株式会社 回転機械
US10280779B2 (en) * 2013-09-10 2019-05-07 United Technologies Corporation Plug seal for gas turbine engine
DE102013224199A1 (de) * 2013-11-27 2015-05-28 MTU Aero Engines AG Gasturbinen-Laufschaufel
US10907491B2 (en) * 2017-11-30 2021-02-02 General Electric Company Sealing system for a rotary machine and method of assembling same
FR3085708B1 (fr) * 2018-09-12 2020-11-27 Safran Helicopter Engines Dispositif d'etancheite ameliore pour ensemble rotatif de turbomachine

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3126149A (en) * 1964-03-24 Foamed aluminum honeycomb motor
US3092393A (en) * 1958-01-20 1963-06-04 Rolls Royce Labyrinth seals
US3701536A (en) * 1970-05-19 1972-10-31 Garrett Corp Labyrinth seal
US4537024A (en) * 1979-04-23 1985-08-27 Solar Turbines, Incorporated Turbine engines
DE2931766C2 (de) * 1979-08-04 1982-08-05 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Dichtungseinrichtung für die freien Schaufelenden eines Verstell-Leitapparates einer Gasturbine
US4473337A (en) * 1982-03-12 1984-09-25 United Technologies Corporation Blade damper seal
GB2127104A (en) * 1982-08-11 1984-04-04 Rolls Royce Sealing means for a turbine rotor blade in a gas turbine engine
US4524980A (en) * 1983-12-05 1985-06-25 United Technologies Corporation Intersecting feather seals for interlocking gas turbine vanes
GB2224082A (en) * 1988-10-19 1990-04-25 Rolls Royce Plc Turbine disc having cooling and sealing arrangements
US5141395A (en) * 1991-09-05 1992-08-25 General Electric Company Flow activated flowpath liner seal
US5188507A (en) * 1991-11-27 1993-02-23 General Electric Company Low-pressure turbine shroud
US5249920A (en) * 1992-07-09 1993-10-05 General Electric Company Turbine nozzle seal arrangement
US5388959A (en) * 1993-08-23 1995-02-14 General Electric Company Seal including a non-metallic abradable material

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112243472A (zh) * 2018-05-23 2021-01-19 赛峰飞机发动机公司 在其之间具有密封件的涡轮机叶片成角度部段

Also Published As

Publication number Publication date
EP0735242B1 (fr) 1998-03-11
DE69600179D1 (de) 1998-04-16
US5707207A (en) 1998-01-13
DE69600179T2 (de) 1998-07-30
EP0735242A1 (fr) 1996-10-02
FR2732416A1 (fr) 1996-10-04

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ST Notification of lapse