DE602004003749D1 - Einrichtung zur passiven Regelung der Wärmedehnung eines Turbomaschinengehäuses - Google Patents

Einrichtung zur passiven Regelung der Wärmedehnung eines Turbomaschinengehäuses

Info

Publication number
DE602004003749D1
DE602004003749D1 DE602004003749T DE602004003749T DE602004003749D1 DE 602004003749 D1 DE602004003749 D1 DE 602004003749D1 DE 602004003749 T DE602004003749 T DE 602004003749T DE 602004003749 T DE602004003749 T DE 602004003749T DE 602004003749 D1 DE602004003749 D1 DE 602004003749D1
Authority
DE
Germany
Prior art keywords
thermal expansion
passive regulation
turbomachinery housing
turbomachinery
housing
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
DE602004003749T
Other languages
English (en)
Other versions
DE602004003749T2 (de
Inventor
Thomas Chereau
Thierry Jean-Maurice Niclot
Alain Raffy
Patrice Suet
Christophe Yvon Gabriel Tourne
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 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 SNECMA SAS filed Critical SNECMA SAS
Publication of DE602004003749D1 publication Critical patent/DE602004003749D1/de
Application granted granted Critical
Publication of DE602004003749T2 publication Critical patent/DE602004003749T2/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
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
DE602004003749T 2003-07-11 2004-06-30 Einrichtung zur passiven Regelung der Wärmedehnung eines Turbomaschinengehäuses Expired - Lifetime DE602004003749T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0308584A FR2857409B1 (fr) 2003-07-11 2003-07-11 Dispositif pour piloter passivement la dilatation thermique du carter d'extension d'un turboreacteur
FR0308584 2003-07-11

Publications (2)

Publication Number Publication Date
DE602004003749D1 true DE602004003749D1 (de) 2007-02-01
DE602004003749T2 DE602004003749T2 (de) 2007-10-11

Family

ID=33443282

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602004003749T Expired - Lifetime DE602004003749T2 (de) 2003-07-11 2004-06-30 Einrichtung zur passiven Regelung der Wärmedehnung eines Turbomaschinengehäuses

Country Status (7)

Country Link
US (1) US7185499B2 (de)
EP (1) EP1496207B1 (de)
JP (1) JP4174039B2 (de)
CA (1) CA2472939C (de)
DE (1) DE602004003749T2 (de)
FR (1) FR2857409B1 (de)
RU (1) RU2343298C2 (de)

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US20090067917A1 (en) * 2007-09-07 2009-03-12 The Boeing Company Bipod Flexure Ring
FR2925122B1 (fr) * 2007-12-14 2015-09-04 Snecma Dispositif de decouplage d'un support de palier
US8875520B2 (en) * 2008-12-31 2014-11-04 Rolls-Royce North American Technologies, Inc. Gas turbine engine device
US8459941B2 (en) * 2009-06-15 2013-06-11 General Electric Company Mechanical joint for a gas turbine engine
ITMI20102195A1 (it) * 2010-11-26 2012-05-26 Alstom Technology Ltd "sistema di collegamento"
CN103492158B (zh) * 2011-04-26 2016-06-15 株式会社Ihi 成形部件
GB201111666D0 (en) * 2011-07-08 2011-08-24 Rolls Royce Plc A joint assembly for an annular structure
FR2978732B1 (fr) * 2011-08-05 2013-09-06 Airbus Operations Sas Dispositif de liaison plus particulierement adapte pour assurer la liaison entre une entree d'air et une motorisation d'une nacelle d'aeronef
US9850780B2 (en) 2012-12-29 2017-12-26 United Technologies Corporation Plate for directing flow and film cooling of components
US9206742B2 (en) * 2012-12-29 2015-12-08 United Technologies Corporation Passages to facilitate a secondary flow between components
US8920109B2 (en) 2013-03-12 2014-12-30 Siemens Aktiengesellschaft Vane carrier thermal management arrangement and method for clearance control
US10451204B2 (en) 2013-03-15 2019-10-22 United Technologies Corporation Low leakage duct segment using expansion joint assembly
ITCO20130044A1 (it) * 2013-10-08 2015-04-09 Nuovo Pignone Srl Cassa per macchina rotativa e macchina rotativa includente tale cassa
DE102013226490A1 (de) 2013-12-18 2015-06-18 Rolls-Royce Deutschland Ltd & Co Kg Gekühlte Flanschverbindung eines Gasturbinentriebwerks
FR3019210B1 (fr) * 2014-04-01 2016-05-13 Snecma Partie de turbomachine comportant une bride avec un dispositif de drainage
US9611760B2 (en) 2014-06-16 2017-04-04 Solar Turbines Incorporated Cutback aft clamp ring
US9879565B2 (en) * 2015-01-20 2018-01-30 United Technologies Corporation Enclosed jacking insert
US10415622B2 (en) * 2016-05-03 2019-09-17 General Electric Company Method and system for hybrid gang channel bolted joint
US10697300B2 (en) * 2017-12-14 2020-06-30 Raytheon Technologies Corporation Rotor balance weight system
US20190368381A1 (en) * 2018-05-30 2019-12-05 General Electric Company Combustion System Deflection Mitigation Structure
US20230003141A1 (en) * 2021-06-30 2023-01-05 Pratt & Whitney Canada Corp. Outside fit flange for aircraft engine
CN114017202B (zh) * 2021-11-12 2023-04-18 中国航发沈阳发动机研究所 一种喷管复材中心锥连接结构
US11814977B1 (en) 2022-08-29 2023-11-14 Rtx Corporation Thermal conditioning of flange with secondary flow

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1058936A (en) * 1912-04-18 1913-04-15 Paul A Bancel Casing for steam-turbines.
US3372542A (en) * 1966-11-25 1968-03-12 United Aircraft Corp Annular burner for a gas turbine
CH488098A (de) * 1968-04-10 1970-03-31 Licentia Gmbh Einrichtung zur Kühlung der Flansche an den Gehäuseteilfugen von Sattdampf- oder Nassdampfturbinen
US4363599A (en) * 1979-10-31 1982-12-14 General Electric Company Clearance control
US5127793A (en) * 1990-05-31 1992-07-07 General Electric Company Turbine shroud clearance control assembly
US5219268A (en) * 1992-03-06 1993-06-15 General Electric Company Gas turbine engine case thermal control flange
US5593277A (en) * 1995-06-06 1997-01-14 General Electric Company Smart turbine shroud
US6352404B1 (en) * 2000-02-18 2002-03-05 General Electric Company Thermal control passages for horizontal split-line flanges of gas turbine engine casings
US6439616B1 (en) * 2001-03-29 2002-08-27 General Electric Company Anti-rotation retainer for a conduit
FR2828908B1 (fr) * 2001-08-23 2004-01-30 Snecma Moteurs Controle des jeux de turbine haute pression

Also Published As

Publication number Publication date
CA2472939A1 (fr) 2005-01-11
JP4174039B2 (ja) 2008-10-29
JP2005030402A (ja) 2005-02-03
RU2004121114A (ru) 2006-01-10
FR2857409A1 (fr) 2005-01-14
DE602004003749T2 (de) 2007-10-11
FR2857409B1 (fr) 2006-07-28
CA2472939C (fr) 2012-03-27
EP1496207B1 (de) 2006-12-20
US20050204746A1 (en) 2005-09-22
RU2343298C2 (ru) 2009-01-10
EP1496207A1 (de) 2005-01-12
US7185499B2 (en) 2007-03-06

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