FR2724973B1 - Dispositif d'etancheite d'aubages mobiles de turbomachine avec controle actif des jeux en temps reel et methode de determination dudit dispositif - Google Patents

Dispositif d'etancheite d'aubages mobiles de turbomachine avec controle actif des jeux en temps reel et methode de determination dudit dispositif

Info

Publication number
FR2724973B1
FR2724973B1 FR8222166A FR8222166A FR2724973B1 FR 2724973 B1 FR2724973 B1 FR 2724973B1 FR 8222166 A FR8222166 A FR 8222166A FR 8222166 A FR8222166 A FR 8222166A FR 2724973 B1 FR2724973 B1 FR 2724973B1
Authority
FR
France
Prior art keywords
turbomachine
real
determining
game control
time active
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
FR8222166A
Other languages
English (en)
Other versions
FR2724973A1 (fr
Inventor
Gerard Ernest Andre Jourdain
Jean Paul Lagrange
Jean Philippe Emile Richard
Marcel Robert Soligny
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 FR8222166A priority Critical patent/FR2724973B1/fr
Priority to FR8311583A priority patent/FR2716496B1/fr
Priority to FR8311584A priority patent/FR2740829B2/fr
Priority to DE3347380A priority patent/DE3347380C2/de
Priority to GB8334526A priority patent/GB2305977B/en
Priority to US06/568,223 priority patent/US5593278A/en
Publication of FR2724973A1 publication Critical patent/FR2724973A1/fr
Application granted granted Critical
Publication of FR2724973B1 publication Critical patent/FR2724973B1/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
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/16Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means
    • F01D11/18Adjusting 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
    • 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
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005Sealing means between non relatively rotating elements
    • F01D11/006Sealing the gap between rotor blades or blades and rotor
    • F01D11/008Sealing the gap between rotor blades or blades and rotor by spacer elements between the blades, e.g. independent interblade platforms
    • 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
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3053Fixing blades to rotors; Blade roots ; Blade spacers by means of pins
    • 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
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3007Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/36Application in turbines specially adapted for the fan of turbofan engines
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR8222166A 1982-12-31 1982-12-31 Dispositif d'etancheite d'aubages mobiles de turbomachine avec controle actif des jeux en temps reel et methode de determination dudit dispositif Expired - Fee Related FR2724973B1 (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
FR8222166A FR2724973B1 (fr) 1982-12-31 1982-12-31 Dispositif d'etancheite d'aubages mobiles de turbomachine avec controle actif des jeux en temps reel et methode de determination dudit dispositif
FR8311583A FR2716496B1 (fr) 1982-12-31 1983-07-12 Dispositif d'étanchéité d'aubages mobiles de turbomachine avec contrôle des jeux en temps réel et méthode de détermination dudit dispositif.
FR8311584A FR2740829B2 (fr) 1982-12-31 1983-07-12 Dispositif d'etancheite d'aubages mobiles de turbomachine avec controle des jeux en temps reel
DE3347380A DE3347380C2 (de) 1982-12-31 1983-12-29 Dichtungsvorrichtung für rotierende Schaufeln von Turbomaschinen mit Echtzeitsteuerung des Schaufelspitzenspiels
GB8334526A GB2305977B (en) 1982-12-31 1983-12-29 Turbo machine rotor blade sealing device with clearance control in real time and method for designing the said device
US06/568,223 US5593278A (en) 1982-12-31 1983-12-30 Gas turbine engine rotor blading sealing device

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR8222166A FR2724973B1 (fr) 1982-12-31 1982-12-31 Dispositif d'etancheite d'aubages mobiles de turbomachine avec controle actif des jeux en temps reel et methode de determination dudit dispositif
FR8311583A FR2716496B1 (fr) 1982-12-31 1983-07-12 Dispositif d'étanchéité d'aubages mobiles de turbomachine avec contrôle des jeux en temps réel et méthode de détermination dudit dispositif.
FR8311584A FR2740829B2 (fr) 1982-12-31 1983-07-12 Dispositif d'etancheite d'aubages mobiles de turbomachine avec controle des jeux en temps reel

Publications (2)

Publication Number Publication Date
FR2724973A1 FR2724973A1 (fr) 1996-03-29
FR2724973B1 true FR2724973B1 (fr) 1996-12-13

Family

ID=27251136

Family Applications (3)

Application Number Title Priority Date Filing Date
FR8222166A Expired - Fee Related FR2724973B1 (fr) 1982-12-31 1982-12-31 Dispositif d'etancheite d'aubages mobiles de turbomachine avec controle actif des jeux en temps reel et methode de determination dudit dispositif
FR8311584A Expired - Lifetime FR2740829B2 (fr) 1982-12-31 1983-07-12 Dispositif d'etancheite d'aubages mobiles de turbomachine avec controle des jeux en temps reel
FR8311583A Expired - Fee Related FR2716496B1 (fr) 1982-12-31 1983-07-12 Dispositif d'étanchéité d'aubages mobiles de turbomachine avec contrôle des jeux en temps réel et méthode de détermination dudit dispositif.

Family Applications After (2)

Application Number Title Priority Date Filing Date
FR8311584A Expired - Lifetime FR2740829B2 (fr) 1982-12-31 1983-07-12 Dispositif d'etancheite d'aubages mobiles de turbomachine avec controle des jeux en temps reel
FR8311583A Expired - Fee Related FR2716496B1 (fr) 1982-12-31 1983-07-12 Dispositif d'étanchéité d'aubages mobiles de turbomachine avec contrôle des jeux en temps réel et méthode de détermination dudit dispositif.

Country Status (4)

Country Link
US (1) US5593278A (fr)
DE (1) DE3347380C2 (fr)
FR (3) FR2724973B1 (fr)
GB (1) GB2305977B (fr)

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US10316683B2 (en) * 2014-04-16 2019-06-11 United Technologies Corporation Gas turbine engine blade outer air seal thermal control system
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US9976435B2 (en) * 2014-12-19 2018-05-22 United Technologies Corporation Blade tip clearance systems
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US10221715B2 (en) * 2015-03-03 2019-03-05 Rolls-Royce North American Technologies Inc. Turbine shroud with axially separated pressure compartments
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US10392944B2 (en) 2016-07-12 2019-08-27 General Electric Company Turbomachine component having impingement heat transfer feature, related turbomachine and storage medium
DE102016117345A1 (de) * 2016-09-15 2018-03-15 Man Diesel & Turbo Se Radialturbine eines Turboladers und Turbolader
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EP3324003B1 (fr) 2016-11-18 2020-03-18 Ansaldo Energia Switzerland AG Aube pour interface de bouclier thermique de stator dans une turbine à gaz
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
US10612466B2 (en) * 2017-09-11 2020-04-07 United Technologies Corporation Gas turbine engine active clearance control system using inlet particle separator
CN109356660B (zh) * 2018-12-14 2021-11-19 中国航发沈阳发动机研究所 双级高压涡轮转静子组件
IT201900001173A1 (it) * 2019-01-25 2020-07-25 Nuovo Pignone Tecnologie Srl Turbina con un anello avvolgente attorno a pale rotoriche e metodo per limitare la perdita di fluido di lavoro in una turbina
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Also Published As

Publication number Publication date
FR2740829B2 (fr) 1999-09-17
GB8334526D0 (en) 1996-06-19
DE3347380A1 (de) 1996-05-09
GB2305977A (en) 1997-04-23
FR2716496B1 (fr) 1998-12-04
FR2716496A1 (fr) 1995-08-25
DE3347380C2 (de) 1997-08-14
GB2305977B (en) 1998-01-07
FR2724973A1 (fr) 1996-03-29
US5593278A (en) 1997-01-14
FR2740829A2 (fr) 1997-05-09

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