FR2431608A1 - Dispositif perfectionne d'alimentation en air de refroidissement d'un support de virole - Google Patents

Dispositif perfectionne d'alimentation en air de refroidissement d'un support de virole

Info

Publication number
FR2431608A1
FR2431608A1 FR7918426A FR7918426A FR2431608A1 FR 2431608 A1 FR2431608 A1 FR 2431608A1 FR 7918426 A FR7918426 A FR 7918426A FR 7918426 A FR7918426 A FR 7918426A FR 2431608 A1 FR2431608 A1 FR 2431608A1
Authority
FR
France
Prior art keywords
cooling air
improved device
rubber support
supplying cooling
rotor
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.)
Granted
Application number
FR7918426A
Other languages
English (en)
Other versions
FR2431608B1 (fr
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of FR2431608A1 publication Critical patent/FR2431608A1/fr
Application granted granted Critical
Publication of FR2431608B1 publication Critical patent/FR2431608B1/fr
Expired 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
    • F01D11/08—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
    • F01D11/20—Actively adjusting tip-clearance
    • F01D11/24—Actively adjusting tip-clearance by selectively cooling-heating stator or rotor components
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Valve-Gear Or Valve Arrangements (AREA)

Abstract

Dispositif permettant de conserver un jeu minimum entre la virole et le rotor en régime permanent et transitoire. Il comprend un élément qui capte la vitesse de fonctionnement du rotor 47; un dispositif 48 qui mesure le temps de fonctionnement du rotor après une accélération; et un organe 55, 60 répondant à ce dispositif qui mesure le temps, qui fait varier la température de l'air. Application aux moteurs d'avion.
FR7918426A 1978-07-17 1979-07-17 Dispositif perfectionne d'alimentation en air de refroidissement d'un support de virole Expired FR2431608B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/925,352 US4230436A (en) 1978-07-17 1978-07-17 Rotor/shroud clearance control system

Publications (2)

Publication Number Publication Date
FR2431608A1 true FR2431608A1 (fr) 1980-02-15
FR2431608B1 FR2431608B1 (fr) 1986-04-11

Family

ID=25451604

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7918426A Expired FR2431608B1 (fr) 1978-07-17 1979-07-17 Dispositif perfectionne d'alimentation en air de refroidissement d'un support de virole

Country Status (7)

Country Link
US (1) US4230436A (fr)
JP (1) JPS5560626A (fr)
CA (1) CA1119525A (fr)
DE (1) DE2927781A1 (fr)
FR (1) FR2431608B1 (fr)
GB (2) GB2025536B (fr)
IT (1) IT1125409B (fr)

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FR2467292A1 (fr) * 1979-10-09 1981-04-17 Snecma Dispositif de reglage du jeu entre les aubes mobiles et l'anneau de turbine
US4338061A (en) * 1980-06-26 1982-07-06 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Control means for a gas turbine engine
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US4513567A (en) * 1981-11-02 1985-04-30 United Technologies Corporation Gas turbine engine active clearance control
US4525998A (en) * 1982-08-02 1985-07-02 United Technologies Corporation Clearance control for gas turbine engine
FR2540939A1 (fr) * 1983-02-10 1984-08-17 Snecma Anneau d'etancheite pour un rotor de turbine d'une turbomachine et installation de turbomachine munie de tels anneaux
GB2136508B (en) * 1983-03-11 1987-12-31 United Technologies Corp Coolable stator assembly for a gas turbine engine
DE3309812C2 (de) 1983-03-18 1994-04-14 United Technologies Corp Äußeres Gehäuse für ein Gasturbinentriebwerk
US4525997A (en) * 1983-08-01 1985-07-02 United Technologies Corporation Stator assembly for bounding the flow path of a gas turbine engine
US4648241A (en) * 1983-11-03 1987-03-10 United Technologies Corporation Active clearance control
US4576547A (en) * 1983-11-03 1986-03-18 United Technologies Corporation Active clearance control
US4643638A (en) * 1983-12-21 1987-02-17 United Technologies Corporation Stator structure for supporting an outer air seal in a gas turbine engine
US4553901A (en) * 1983-12-21 1985-11-19 United Technologies Corporation Stator structure for a gas turbine engine
US4645416A (en) * 1984-11-01 1987-02-24 United Technologies Corporation Valve and manifold for compressor bore heating
US4632635A (en) * 1984-12-24 1986-12-30 Allied Corporation Turbine blade clearance controller
US4752184A (en) * 1986-05-12 1988-06-21 The United States Of America As Represented By The Secretary Of The Air Force Self-locking outer air seal with full backside cooling
US4824327A (en) * 1987-12-15 1989-04-25 United Technologies Corporation Gas turbine engine oil drain slot
US4928240A (en) * 1988-02-24 1990-05-22 General Electric Company Active clearance control
US5012420A (en) * 1988-03-31 1991-04-30 General Electric Company Active clearance control for gas turbine engine
US4893983A (en) * 1988-04-07 1990-01-16 General Electric Company Clearance control system
US4893984A (en) * 1988-04-07 1990-01-16 General Electric Company Clearance control system
US4826397A (en) * 1988-06-29 1989-05-02 United Technologies Corporation Stator assembly for a gas turbine engine
US5039278A (en) * 1989-04-11 1991-08-13 General Electric Company Power turbine ventilation system
US5090193A (en) * 1989-06-23 1992-02-25 United Technologies Corporation Active clearance control with cruise mode
US5104287A (en) * 1989-09-08 1992-04-14 General Electric Company Blade tip clearance control apparatus for a gas turbine engine
US5018942A (en) * 1989-09-08 1991-05-28 General Electric Company Mechanical blade tip clearance control apparatus for a gas turbine engine
US5096375A (en) * 1989-09-08 1992-03-17 General Electric Company Radial adjustment mechanism for blade tip clearance control apparatus
US5054997A (en) * 1989-11-22 1991-10-08 General Electric Company Blade tip clearance control apparatus using bellcrank mechanism
US5098133A (en) * 1990-01-31 1992-03-24 General Electric Company Tube coupling with swivelable piston
US5056988A (en) * 1990-02-12 1991-10-15 General Electric Company Blade tip clearance control apparatus using shroud segment position modulation
US5049033A (en) * 1990-02-20 1991-09-17 General Electric Company Blade tip clearance control apparatus using cam-actuated shroud segment positioning mechanism
US5100291A (en) * 1990-03-28 1992-03-31 General Electric Company Impingement manifold
US5127793A (en) * 1990-05-31 1992-07-07 General Electric Company Turbine shroud clearance control assembly
GB2245316B (en) * 1990-06-21 1993-12-15 Rolls Royce Plc Improvements in shroud assemblies for turbine rotors
DE69017685T2 (de) * 1990-10-17 1995-07-06 United Technologies Corp Aktive Rotor-Statorspielregelung für Gasturbine.
US5228828A (en) * 1991-02-15 1993-07-20 General Electric Company Gas turbine engine clearance control apparatus
US5152666A (en) * 1991-05-03 1992-10-06 United Technologies Corporation Stator assembly for a rotary machine
GB2263946A (en) * 1992-02-04 1993-08-11 Bmw Rolls Royce Gmbh An arrangement for supplying cooling air to a gas turbine casing.
FR2688539A1 (fr) * 1992-03-11 1993-09-17 Snecma Stator de turbomachine comprenant des dispositifs de reglage de jeu entre le stator et les aubes du rotor.
DE4327376A1 (de) * 1993-08-14 1995-02-16 Abb Management Ag Verdichter sowie Verfahren zu dessen Betrieb
US5399066A (en) * 1993-09-30 1995-03-21 General Electric Company Integral clearance control impingement manifold and environmental shield
US5685693A (en) * 1995-03-31 1997-11-11 General Electric Co. Removable inner turbine shell with bucket tip clearance control
DE19643716A1 (de) * 1996-10-23 1998-04-30 Asea Brown Boveri Schaufelträger für einen Verdichter
GB9709086D0 (en) * 1997-05-07 1997-06-25 Rolls Royce Plc Gas turbine engine cooling apparatus
DE19756734A1 (de) * 1997-12-19 1999-06-24 Bmw Rolls Royce Gmbh Passives Spalthaltungssystem einer Gasturbine
US5993150A (en) * 1998-01-16 1999-11-30 General Electric Company Dual cooled shroud
US6224329B1 (en) * 1999-01-07 2001-05-01 Siemens Westinghouse Power Corporation Method of cooling a combustion turbine
DE19961528C1 (de) * 1999-12-20 2001-06-13 Siemens Ag Verfahren zur Überwachung des radialen Spalts zwischen dem Rotor und dem Stator eines elektrischen Generators und Vorrichtung zur Durchführung des Verfahrens
US6327844B1 (en) * 2000-03-03 2001-12-11 General Electric Company Methods and apparatus for retaining flow restrictors within turbine engines
US7554324B2 (en) * 2003-10-28 2009-06-30 Honeywell International Inc. Turbine blade proximity sensor and control system
FR2890685B1 (fr) * 2005-09-14 2007-12-14 Snecma Pilotage de jeu au sommet d'aubes de rotor de turbine haute pression dans une turbomachine
US7491029B2 (en) 2005-10-14 2009-02-17 United Technologies Corporation Active clearance control system for gas turbine engines
US8126628B2 (en) * 2007-08-03 2012-02-28 General Electric Company Aircraft gas turbine engine blade tip clearance control
US8616827B2 (en) * 2008-02-20 2013-12-31 Rolls-Royce Corporation Turbine blade tip clearance system
US8256228B2 (en) * 2008-04-29 2012-09-04 Rolls Royce Corporation Turbine blade tip clearance apparatus and method
US8296037B2 (en) * 2008-06-20 2012-10-23 General Electric Company Method, system, and apparatus for reducing a turbine clearance
JP5220509B2 (ja) * 2008-08-01 2013-06-26 ゼネラル・エレクトリック・カンパニイ 航空機用ガスタービンエンジンのブレード先端間隙制御
GB201105103D0 (en) * 2011-03-28 2011-05-11 Rolls Royce Plc Securing system
US8708554B2 (en) * 2011-05-12 2014-04-29 Arrowhead Products Corporation Leak detection apparatus for aircraft bleed air systems
US9157331B2 (en) * 2011-12-08 2015-10-13 Siemens Aktiengesellschaft Radial active clearance control for a gas turbine engine
US8967951B2 (en) 2012-01-10 2015-03-03 General Electric Company Turbine assembly and method for supporting turbine components
US9677421B2 (en) 2012-10-24 2017-06-13 United Technologies Corporation Gas turbine engine rotor drain feature
US9587507B2 (en) 2013-02-23 2017-03-07 Rolls-Royce North American Technologies, Inc. Blade clearance control for gas turbine engine
JP5460902B2 (ja) * 2013-03-07 2014-04-02 ゼネラル・エレクトリック・カンパニイ 航空機用ガスタービンエンジンのブレード先端間隙制御
WO2014143934A1 (fr) * 2013-03-15 2014-09-18 United Technologies Corporation Ensemble joint étanche à l'air externe d'aube flottant pour moteur à turbine à gaz
EP2984297B1 (fr) * 2013-04-12 2020-04-01 United Technologies Corporation Système de commande de jeu à réponse rapide de carter de turbine à volume variable
FR3024751B1 (fr) * 2014-08-05 2019-07-19 Safran Aircraft Engines Unite de commande pour le pilotage d'un jeu entre des sommets d'aubes et un anneau de turbine
US10316698B2 (en) * 2016-05-23 2019-06-11 United Technologies Corporation Dirt shield
US10794214B2 (en) * 2017-05-08 2020-10-06 United Technologies Corporation Tip clearance control for gas turbine engine
US10815814B2 (en) * 2017-05-08 2020-10-27 Raytheon Technologies Corporation Re-use and modulated cooling from tip clearance control system for gas turbine engine
EP3540182A1 (fr) * 2018-03-14 2019-09-18 Siemens Aktiengesellschaft Procédé de commande d'une minimisation d'ouverture d'une turbine à gaz
CN110454238A (zh) * 2019-07-31 2019-11-15 中国航发沈阳发动机研究所 一种用于涡轮间隙主动控制的热气分配器、平台及方法
US20230228202A1 (en) * 2022-01-20 2023-07-20 General Electric Company Stator plenum with collet seal

Citations (6)

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US3584458A (en) * 1969-11-25 1971-06-15 Gen Motors Corp Turbine cooling
GB1248198A (en) * 1970-02-06 1971-09-29 Rolls Royce Sealing device
FR2280791A1 (fr) * 1974-07-31 1976-02-27 Snecma Perfectionnements au reglage du jeu entre les aubes et le stator d'une turbine
US4005946A (en) * 1975-06-20 1977-02-01 United Technologies Corporation Method and apparatus for controlling stator thermal growth
FR2333953A1 (fr) * 1975-12-05 1977-07-01 United Technologies Corp Dispositif de reglage de jeu pour un moteur a turbine a gaz
FR2360750A1 (fr) * 1976-08-02 1978-03-03 Gen Electric Procede pour reduire le jeu fonctionnel entre un rotor de turbine et la frette qui l'entoure

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GB1090173A (en) * 1966-05-04 1967-11-08 Rolls Royce Gas turbine engine
US3391904A (en) * 1966-11-02 1968-07-09 United Aircraft Corp Optimum response tip seal
BE756582A (fr) * 1969-10-02 1971-03-01 Gen Electric Ecran circulaire et support d'ecran avec dispositif de reglage de la temperature pour turbomachine
US3966354A (en) * 1974-12-19 1976-06-29 General Electric Company Thermal actuated valve for clearance control
GB1581566A (en) * 1976-08-02 1980-12-17 Gen Electric Minimum clearance turbomachine shroud apparatus
US4102595A (en) * 1976-10-19 1978-07-25 General Electric Company Bleed valve control system
US4117669A (en) * 1977-03-04 1978-10-03 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Apparatus and method for reducing thermal stress in a turbine rotor

Patent Citations (6)

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Publication number Priority date Publication date Assignee Title
US3584458A (en) * 1969-11-25 1971-06-15 Gen Motors Corp Turbine cooling
GB1248198A (en) * 1970-02-06 1971-09-29 Rolls Royce Sealing device
FR2280791A1 (fr) * 1974-07-31 1976-02-27 Snecma Perfectionnements au reglage du jeu entre les aubes et le stator d'une turbine
US4005946A (en) * 1975-06-20 1977-02-01 United Technologies Corporation Method and apparatus for controlling stator thermal growth
FR2333953A1 (fr) * 1975-12-05 1977-07-01 United Technologies Corp Dispositif de reglage de jeu pour un moteur a turbine a gaz
FR2360750A1 (fr) * 1976-08-02 1978-03-03 Gen Electric Procede pour reduire le jeu fonctionnel entre un rotor de turbine et la frette qui l'entoure

Also Published As

Publication number Publication date
DE2927781C2 (fr) 1987-05-27
JPS5560626A (en) 1980-05-07
US4230436A (en) 1980-10-28
CA1119525A (fr) 1982-03-09
JPH0135162B2 (fr) 1989-07-24
GB2025536A (en) 1980-01-23
GB2089439A (en) 1982-06-23
DE2927781A1 (de) 1980-01-31
GB2089439B (en) 1983-04-20
GB2025536B (en) 1983-04-27
IT7923983A0 (it) 1979-06-29
FR2431608B1 (fr) 1986-04-11
IT1125409B (it) 1986-05-14

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