DE3561231D1 - Process for the production of a ceramic turbine ring integrated into a metalic support - Google Patents

Process for the production of a ceramic turbine ring integrated into a metalic support

Info

Publication number
DE3561231D1
DE3561231D1 DE8585402051T DE3561231T DE3561231D1 DE 3561231 D1 DE3561231 D1 DE 3561231D1 DE 8585402051 T DE8585402051 T DE 8585402051T DE 3561231 T DE3561231 T DE 3561231T DE 3561231 D1 DE3561231 D1 DE 3561231D1
Authority
DE
Germany
Prior art keywords
metalic
production
support
turbine ring
ring integrated
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
Application number
DE8585402051T
Other languages
English (en)
Inventor
Alain Marie Lardellier
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
Application granted granted Critical
Publication of DE3561231D1 publication Critical patent/DE3561231D1/de
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D25/00—Special casting characterised by the nature of the product
    • 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
    • F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Ceramic Products (AREA)
  • Devices For Post-Treatments, Processing, Supply, Discharge, And Other Processes (AREA)
DE8585402051T 1984-10-30 1985-10-23 Process for the production of a ceramic turbine ring integrated into a metalic support Expired DE3561231D1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8416535A FR2572394B1 (fr) 1984-10-30 1984-10-30 Procede de fabrication d'un anneau de turbine en ceramique integre a un support metallique annulaire

Publications (1)

Publication Number Publication Date
DE3561231D1 true DE3561231D1 (en) 1988-02-04

Family

ID=9309108

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8585402051T Expired DE3561231D1 (en) 1984-10-30 1985-10-23 Process for the production of a ceramic turbine ring integrated into a metalic support

Country Status (5)

Country Link
US (1) US4646810A (de)
EP (1) EP0181255B1 (de)
JP (1) JPS61119370A (de)
DE (1) DE3561231D1 (de)
FR (1) FR2572394B1 (de)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4914794A (en) * 1986-08-07 1990-04-10 Allied-Signal Inc. Method of making an abradable strain-tolerant ceramic coated turbine shroud
JPH0791352B2 (ja) * 1987-11-20 1995-10-04 住友デュレズ株式会社 シェルモールド用ノボラック型フェノール樹脂の製造方法
FR2646473B1 (fr) * 1989-04-26 1991-07-05 Snecma Moteur a soufflantes contrarotatives tractrices
US5062767A (en) * 1990-04-27 1991-11-05 The United States Of America As Represented By The Secretary Of The Air Force Segmented composite inner shrouds
US5413647A (en) * 1992-03-26 1995-05-09 General Electric Company Method for forming a thin-walled combustion liner for use in a gas turbine engine
US5447411A (en) * 1993-06-10 1995-09-05 Martin Marietta Corporation Light weight fan blade containment system
US6000906A (en) * 1997-09-12 1999-12-14 Alliedsignal Inc. Ceramic airfoil
US6758653B2 (en) 2002-09-09 2004-07-06 Siemens Westinghouse Power Corporation Ceramic matrix composite component for a gas turbine engine
WO2007064605A2 (en) 2005-11-30 2007-06-07 Dresser-Rand Company End closure device for a turbomachine casing
EP1865258A1 (de) * 2006-06-06 2007-12-12 Siemens Aktiengesellschaft Gepanzerte Maschinenkomponente und Gasturbine
US8528339B2 (en) 2007-04-05 2013-09-10 Siemens Energy, Inc. Stacked laminate gas turbine component
EP2951399B1 (de) * 2013-01-29 2020-02-19 Rolls-Royce Corporation Turbinendeckband und zugehöriges montageverfahren
EP2769969B1 (de) * 2013-02-25 2018-10-17 Ansaldo Energia IP UK Limited Verfahren zur Herstellung einer Metall-Keramik-Verbundstruktur sowie Metall-Keramik-Verbundstruktur
EP2971577B1 (de) 2013-03-13 2018-08-29 Rolls-Royce Corporation Turbinendeckband
DE102013213834A1 (de) * 2013-07-15 2015-02-19 MTU Aero Engines AG Verfahren zum Herstellen eines Isolationselements und Isolationselement für ein Gehäuse eines Flugtriebwerks
US10190434B2 (en) 2014-10-29 2019-01-29 Rolls-Royce North American Technologies Inc. Turbine shroud with locating inserts
CA2915370A1 (en) 2014-12-23 2016-06-23 Rolls-Royce Corporation Full hoop blade track with axially keyed features
CA2915246A1 (en) 2014-12-23 2016-06-23 Rolls-Royce Corporation Turbine shroud
EP3045674B1 (de) 2015-01-15 2018-11-21 Rolls-Royce Corporation Turbinenummantelung mit rohrförmigen laufradpositionierungseinsätzen
CA2925588A1 (en) 2015-04-29 2016-10-29 Rolls-Royce Corporation Brazed blade track for a gas turbine engine
CA2924855A1 (en) 2015-04-29 2016-10-29 Rolls-Royce Corporation Keystoned blade track
US10125788B2 (en) 2016-01-08 2018-11-13 General Electric Company Ceramic tile fan blade containment
US10240476B2 (en) 2016-01-19 2019-03-26 Rolls-Royce North American Technologies Inc. Full hoop blade track with interstage cooling air
US10415415B2 (en) 2016-07-22 2019-09-17 Rolls-Royce North American Technologies Inc. Turbine shroud with forward case and full hoop blade track
US10287906B2 (en) 2016-05-24 2019-05-14 Rolls-Royce North American Technologies Inc. Turbine shroud with full hoop ceramic matrix composite blade track and seal system
CN110723966B (zh) * 2019-11-13 2022-04-01 中国航发南方工业有限公司 扇形片状陶瓷型芯的制备方法
CN112723899A (zh) * 2020-12-31 2021-04-30 淮安市浩远机械制造有限公司 一种氧化铝陶瓷钎焊合金钢复合耐磨板及其制备工艺

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3401026A (en) * 1966-01-19 1968-09-10 Gen Motors Corp Method of forming a bimetallic article
US3511306A (en) * 1969-03-17 1970-05-12 Certain Teed St Gobain Method and apparatus for centrifugally casting perforated rings
BE792224A (fr) * 1971-12-01 1973-03-30 Penny Robert N Element composite long ayant un coefficient de dilatation lineaire effectif predetermine
US4112574A (en) * 1976-11-02 1978-09-12 International Harvester Company Torsielastic thrust bushing for track chains
US4087199A (en) * 1976-11-22 1978-05-02 General Electric Company Ceramic turbine shroud assembly
US4135851A (en) * 1977-05-27 1979-01-23 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Composite seal for turbomachinery
US4377196A (en) * 1980-07-14 1983-03-22 Abex Corporation Method of centrifugally casting a metal tube
US4426193A (en) * 1981-01-22 1984-01-17 The United States Of America As Represented By The Secretary Of The Air Force Impact composite blade
FR2540938B1 (fr) * 1983-02-10 1987-06-05 Snecma Anneau de turbine d'une turbomachine
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

Also Published As

Publication number Publication date
FR2572394B1 (fr) 1986-12-19
JPS61119370A (ja) 1986-06-06
FR2572394A1 (fr) 1986-05-02
US4646810A (en) 1987-03-03
EP0181255A1 (de) 1986-05-14
EP0181255B1 (de) 1987-12-23
JPH0247309B2 (de) 1990-10-19

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee