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FR2652383B1 - Perfectionnement aux turbo-moteurs a gaz. - Google Patents

Perfectionnement aux turbo-moteurs a gaz.

Info

Publication number
FR2652383B1
FR2652383B1 FR909011648A FR9011648A FR2652383B1 FR 2652383 B1 FR2652383 B1 FR 2652383B1 FR 909011648 A FR909011648 A FR 909011648A FR 9011648 A FR9011648 A FR 9011648A FR 2652383 B1 FR2652383 B1 FR 2652383B1
Authority
FR
France
Prior art keywords
engines
improvement
gas turbo
turbo
gas
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
FR909011648A
Other languages
English (en)
Other versions
FR2652383A1 (fr
Inventor
Hayton Paul Robert
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of FR2652383A1 publication Critical patent/FR2652383A1/fr
Application granted granted Critical
Publication of FR2652383B1 publication Critical patent/FR2652383B1/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
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/284—Selection of ceramic materials
    • 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/20—Oxide or non-oxide ceramics
    • F05D2300/21—Oxide ceramics
    • 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)
  • Chemical & Material Sciences (AREA)
  • Ceramic Engineering (AREA)
  • Materials Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR909011648A 1989-09-22 1990-09-21 Perfectionnement aux turbo-moteurs a gaz. Expired - Fee Related FR2652383B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8921450A GB2236809B (en) 1989-09-22 1989-09-22 Improvements in or relating to gas turbine engines

Publications (2)

Publication Number Publication Date
FR2652383A1 FR2652383A1 (fr) 1991-03-29
FR2652383B1 true FR2652383B1 (fr) 1992-05-07

Family

ID=10663470

Family Applications (1)

Application Number Title Priority Date Filing Date
FR909011648A Expired - Fee Related FR2652383B1 (fr) 1989-09-22 1990-09-21 Perfectionnement aux turbo-moteurs a gaz.

Country Status (3)

Country Link
US (1) US5129783A (fr)
FR (1) FR2652383B1 (fr)
GB (1) GB2236809B (fr)

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FR2685033B1 (fr) * 1991-12-11 1994-02-11 Snecma Stator dirigeant l'entree de l'air a l'interieur d'une turbomachine et procede de montage d'une aube de ce stator.
US5704762A (en) * 1993-11-08 1998-01-06 Alliedsignal Inc. Ceramic-to-metal stator vane assembly
US5411368A (en) * 1993-11-08 1995-05-02 Allied-Signal Inc. Ceramic-to-metal stator vane assembly with braze
US5706647A (en) * 1994-11-15 1998-01-13 Solar Turbines Incorporated Airfoil structure
US5653580A (en) * 1995-03-06 1997-08-05 Solar Turbines Incorporated Nozzle and shroud assembly mounting structure
US5839878A (en) * 1996-09-30 1998-11-24 United Technologies Corporation Gas turbine stator vane
US6000906A (en) * 1997-09-12 1999-12-14 Alliedsignal Inc. Ceramic airfoil
US6164903A (en) * 1998-12-22 2000-12-26 United Technologies Corporation Turbine vane mounting arrangement
US6358001B1 (en) * 2000-04-29 2002-03-19 General Electric Company Turbine frame assembly
US6287091B1 (en) * 2000-05-10 2001-09-11 General Motors Corporation Turbocharger with nozzle ring coupling
US6375429B1 (en) * 2001-02-05 2002-04-23 General Electric Company Turbomachine blade-to-rotor sealing arrangement
US6464456B2 (en) * 2001-03-07 2002-10-15 General Electric Company Turbine vane assembly including a low ductility vane
JP4040922B2 (ja) 2001-07-19 2008-01-30 株式会社東芝 組立式ノズルダイアフラムおよびその組立方法
US6884026B2 (en) 2002-09-30 2005-04-26 General Electric Company Turbine engine shroud assembly including axially floating shroud segment
US6821085B2 (en) 2002-09-30 2004-11-23 General Electric Company Turbine engine axially sealing assembly including an axially floating shroud, and assembly method
US6843638B2 (en) 2002-12-10 2005-01-18 Honeywell International Inc. Vane radial mounting apparatus
US6939106B2 (en) * 2002-12-11 2005-09-06 General Electric Company Sealing of steam turbine nozzle hook leakages using a braided rope seal
US6832892B2 (en) * 2002-12-11 2004-12-21 General Electric Company Sealing of steam turbine bucket hook leakages using a braided rope seal
US6808363B2 (en) 2002-12-20 2004-10-26 General Electric Company Shroud segment and assembly with circumferential seal at a planar segment surface
US6893214B2 (en) 2002-12-20 2005-05-17 General Electric Company Shroud segment and assembly with surface recessed seal bridging adjacent members
US6916154B2 (en) * 2003-04-29 2005-07-12 Pratt & Whitney Canada Corp. Diametrically energized piston ring
US7033135B2 (en) 2003-11-10 2006-04-25 General Electric Company Method and apparatus for distributing fluid into a turbomachine
DE102005013794A1 (de) * 2005-03-24 2006-09-28 Alstom Technology Ltd. Leitschaufel für eine Strömungsrotationsmaschine
US8099962B2 (en) * 2008-11-28 2012-01-24 Pratt & Whitney Canada Corp. Mid turbine frame system and radial locator for radially centering a bearing for gas turbine engine
US8047778B2 (en) * 2009-01-06 2011-11-01 General Electric Company Method and apparatus for insuring proper installation of stators in a compressor case
US8360716B2 (en) * 2010-03-23 2013-01-29 United Technologies Corporation Nozzle segment with reduced weight flange
US8668442B2 (en) * 2010-06-30 2014-03-11 Honeywell International Inc. Turbine nozzles and methods of manufacturing the same
US20120195746A1 (en) * 2011-01-27 2012-08-02 General Electric Company Turbomachine service assembly
US9376933B2 (en) * 2011-04-29 2016-06-28 Leonard M. Andersen Apparatus for distributing fluid into a gas turbine
US9951639B2 (en) * 2012-02-10 2018-04-24 Pratt & Whitney Canada Corp. Vane assemblies for gas turbine engines
EP2660429A1 (fr) 2012-05-03 2013-11-06 Siemens Aktiengesellschaft Dispositif d'étanchéité pour aube de guidage de buse et turbine à gaz
US9366149B2 (en) * 2012-09-21 2016-06-14 United Technologies Corporation Multi-stage high pressure compressor case
US9551238B2 (en) 2012-09-28 2017-01-24 United Technologies Corporation Pin connector for ceramic matrix composite turbine frame
US9175573B2 (en) * 2012-11-28 2015-11-03 General Electric Company Dovetail attachment seal for a turbomachine
US9506361B2 (en) 2013-03-08 2016-11-29 Pratt & Whitney Canada Corp. Low profile vane retention
DE102013222980A1 (de) * 2013-11-12 2015-06-11 MTU Aero Engines AG Leitschaufel für eine Strömungsmaschine mit einer Dichtungsvorrichtung, Leitrad sowie Strömungsmaschine
WO2015088656A1 (fr) * 2013-12-12 2015-06-18 United Technologies Corporation Joint d'étanchéité "dog bone" enveloppé
EP2886802B1 (fr) * 2013-12-20 2019-04-10 Safran Aero Boosters SA Joint de virole interne de dernier étage de compresseur de turbomachine axiale
DE102014223975A1 (de) * 2014-11-25 2016-05-25 MTU Aero Engines AG Leitschaufelkranz und Strömungsmaschine
EP3073056B1 (fr) * 2015-03-25 2018-01-03 Ansaldo Energia IP UK Limited Joint de fil
US20170159494A1 (en) * 2015-12-07 2017-06-08 General Electric Company Steam turbine nozzle segment with complete sidewall and integrated hook design
DE102016115610A1 (de) 2016-08-23 2018-03-01 Rolls-Royce Deutschland Ltd & Co Kg Gasturbine und Verfahren zum Aufhängen eines Turbinen-Leitschaufelsegments einer Gasturbine
FR3056637B1 (fr) * 2016-09-27 2018-10-19 Safran Aircraft Engines Ensemble d'anneau de turbine avec calage a froid
CN109209518B (zh) * 2018-10-29 2020-12-22 江苏海事职业技术学院 一种燃气轮机透平静叶定位结构
US10975708B2 (en) * 2019-04-23 2021-04-13 Rolls-Royce Plc Turbine section assembly with ceramic matrix composite vane
US10975709B1 (en) * 2019-11-11 2021-04-13 Rolls-Royce Plc Turbine vane assembly with ceramic matrix composite components and sliding support

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US2819871A (en) * 1954-09-07 1958-01-14 John R Mcveigh Vane structure
GB858891A (en) * 1958-12-12 1961-01-18 John Ryan Mckee Jr Composite sealing washer
US3326523A (en) * 1965-12-06 1967-06-20 Gen Electric Stator vane assembly having composite sectors
GB1386949A (en) * 1971-06-18 1975-03-12 Rolls Royce Combustion chamber for a gas turbine engine
US3881844A (en) * 1974-05-28 1975-05-06 Gen Electric Blade platform vibration dampers
FR2275651A1 (fr) * 1974-06-21 1976-01-16 Snecma Perfectionnements aux stators de turbomachines axiales
US3966353A (en) * 1975-02-21 1976-06-29 Westinghouse Electric Corporation Ceramic-to-metal (or ceramic) cushion/seal for use with three piece ceramic stationary vane assembly
GB2129503B (en) * 1977-08-03 1984-09-19 Rolls Royce A nozzle guide vane for a gas turbine engine
US4245954A (en) * 1978-12-01 1981-01-20 Westinghouse Electric Corp. Ceramic turbine stator vane and shroud support
US4218067A (en) * 1979-02-02 1980-08-19 Pressure Science Incorporated Multi-ply sealing rings
GB2043798B (en) * 1979-03-14 1983-01-12 Rolls Royce Gas turbine stator vane assembly
GB2084261A (en) * 1980-09-30 1982-04-07 Rolls Royce Mounting compressor stator blades
US4477086A (en) * 1982-11-01 1984-10-16 United Technologies Corporation Seal ring with slidable inner element bridging circumferential gap
FR2535795B1 (fr) * 1982-11-08 1987-04-10 Snecma Dispositif de suspension d'aubes statoriques de compresseur axial pour le controle actif des jeux entre rotor et stator
US4445694A (en) * 1982-12-17 1984-05-01 Westinghouse Electric Corp. All-metal expandable ultra high vacuum seal
US4500098A (en) * 1983-12-22 1985-02-19 United Technologies Corporation Gas seal for rotating components
FR2557662B1 (fr) * 1983-12-29 1987-12-31 Commissariat Energie Atomique Joint d'etancheite metallique flexible comportant des parties saillantes consommables
GB2172347B (en) * 1985-03-12 1988-03-16 Gen Connector Corp Sealing rings
DE3509192A1 (de) * 1985-03-14 1986-09-25 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Stroemungsmaschine mit mitteln zur kontrolle des radialspaltes
FR2600379B1 (fr) * 1986-06-18 1988-09-02 Snecma Redresseur de soufflante de turboreacteur multiflux
US4834613A (en) * 1988-02-26 1989-05-30 United Technologies Corporation Radially constrained variable vane shroud
US4990056A (en) * 1989-11-16 1991-02-05 General Motors Corporation Stator vane stage in axial flow compressor

Also Published As

Publication number Publication date
GB2236809B (en) 1994-03-16
US5129783A (en) 1992-07-14
FR2652383A1 (fr) 1991-03-29
GB2236809A (en) 1991-04-17
GB8921450D0 (en) 1989-11-08

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Legal Events

Date Code Title Description
ST Notification of lapse