DE69506074T2 - Faserverstärkte Turbomaschinenschaufel mit integrierter Bürstendichtung und deren Herstellungsweise - Google Patents

Faserverstärkte Turbomaschinenschaufel mit integrierter Bürstendichtung und deren Herstellungsweise

Info

Publication number
DE69506074T2
DE69506074T2 DE69506074T DE69506074T DE69506074T2 DE 69506074 T2 DE69506074 T2 DE 69506074T2 DE 69506074 T DE69506074 T DE 69506074T DE 69506074 T DE69506074 T DE 69506074T DE 69506074 T2 DE69506074 T2 DE 69506074T2
Authority
DE
Germany
Prior art keywords
reinforced
fiber
manufacture
turbo machine
brush seal
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
DE69506074T
Other languages
English (en)
Other versions
DE69506074D1 (de
Inventor
Monique Andre Thore
Pascal Claude Michel A Vasseur
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
Publication of DE69506074D1 publication Critical patent/DE69506074D1/de
Application granted granted Critical
Publication of DE69506074T2 publication Critical patent/DE69506074T2/de
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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/20—Specially-shaped blade tips to seal space between tips and stator
    • 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
    • F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/08—Sealings
    • F04D29/16—Sealings between pressure and suction sides
    • F04D29/161—Sealings between pressure and suction sides especially adapted for elastic fluid pumps
    • F04D29/164—Sealings between pressure and suction sides especially adapted for elastic fluid pumps of an axial flow wheel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16J—PISTONS; CYLINDERS; SEALINGS
    • F16J15/00—Sealings
    • F16J15/16—Sealings between relatively-moving surfaces
    • F16J15/32—Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings
    • F16J15/3284—Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings characterised by their structure; Selection of materials
    • F16J15/3288—Filamentary structures, e.g. brush seals
    • 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
    • F05D2240/55—Seals
    • F05D2240/56—Brush seals
    • 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)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Composite Materials (AREA)
  • Sealing Devices (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
DE69506074T 1994-09-14 1995-09-13 Faserverstärkte Turbomaschinenschaufel mit integrierter Bürstendichtung und deren Herstellungsweise Expired - Fee Related DE69506074T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9410949A FR2724412B1 (fr) 1994-09-14 1994-09-14 Aube de turbomachine en materiau composite munie d'un joint d'etancheite et son procede de realisation

Publications (2)

Publication Number Publication Date
DE69506074D1 DE69506074D1 (de) 1998-12-24
DE69506074T2 true DE69506074T2 (de) 1999-04-22

Family

ID=9466922

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69506074T Expired - Fee Related DE69506074T2 (de) 1994-09-14 1995-09-13 Faserverstärkte Turbomaschinenschaufel mit integrierter Bürstendichtung und deren Herstellungsweise

Country Status (4)

Country Link
US (1) US5628622A (de)
EP (1) EP0708227B1 (de)
DE (1) DE69506074T2 (de)
FR (1) FR2724412B1 (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102004050739A1 (de) * 2004-10-19 2006-04-20 Mtu Aero Engines Gmbh Turbomaschine, insbesondere Gasturbine

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IT1284468B1 (it) * 1995-07-28 1998-05-21 Mtu Muenchen Gmbh Guarnizione a spazzola per turbomacchine
US5752802A (en) * 1996-12-19 1998-05-19 Solar Turbines Incorporated Sealing apparatus for airfoils of gas turbine engines
US6206642B1 (en) * 1998-12-17 2001-03-27 United Technologies Corporation Compressor blade for a gas turbine engine
EP1167840A1 (de) * 2000-06-21 2002-01-02 Siemens Aktiengesellschaft Bürstendichtung für Turbomaschinenschaufeln
US6488471B1 (en) 2000-10-04 2002-12-03 The United States Of America As Represented By The Secretary Of The Air Force Gas-turbine brush seals with permanent radial gap
US6508624B2 (en) 2001-05-02 2003-01-21 Siemens Automotive, Inc. Turbomachine with double-faced rotor-shroud seal structure
GB2385378B (en) * 2002-02-14 2005-08-31 Rolls Royce Plc Engine casing
US20040180595A1 (en) * 2003-03-11 2004-09-16 Matthew Arold-Gorham Woven brush with base for forming site seal
US7575417B2 (en) * 2003-09-05 2009-08-18 General Electric Company Reinforced fan blade
GB2416192B (en) * 2004-07-14 2006-09-27 Rolls Royce Plc Ducted fan with containment structure
GB0428201D0 (en) * 2004-12-22 2005-01-26 Rolls Royce Plc A composite blade
US7549841B1 (en) * 2005-09-03 2009-06-23 Florida Turbine Technologies, Inc. Pressure balanced centrifugal tip seal
US7972109B2 (en) * 2006-12-28 2011-07-05 General Electric Company Methods and apparatus for fabricating a fan assembly for use with turbine engines
US8262348B2 (en) * 2008-04-08 2012-09-11 Siemens Energy, Inc. Turbine blade tip gap reduction system
GB0807358D0 (en) * 2008-04-23 2008-05-28 Rolls Royce Plc Fan blade
US20100205972A1 (en) * 2009-02-17 2010-08-19 General Electric Company One-piece can combustor with heat transfer surface enhacements
US20110164962A1 (en) * 2010-01-07 2011-07-07 Florida Turbine Technologies, Inc. Turbine blade with tip brush seal
ITCO20110058A1 (it) 2011-12-05 2013-06-06 Nuovo Pignone Spa Turbomacchina
US20140064937A1 (en) * 2012-06-29 2014-03-06 General Electric Company Fan blade brush tip
US9080457B2 (en) 2013-02-23 2015-07-14 Rolls-Royce Corporation Edge seal for gas turbine engine ceramic matrix composite component
US10145301B2 (en) 2014-09-23 2018-12-04 Pratt & Whitney Canada Corp. Gas turbine engine inlet
US10378554B2 (en) 2014-09-23 2019-08-13 Pratt & Whitney Canada Corp. Gas turbine engine with partial inlet vane
FR3027622B1 (fr) 2014-10-28 2018-11-09 Safran Aircraft Engines Aube de rotor a pilotage de jeu actif, ensemble tournant et son procede de fonctionnement
US9938848B2 (en) * 2015-04-23 2018-04-10 Pratt & Whitney Canada Corp. Rotor assembly with wear member
US9957807B2 (en) 2015-04-23 2018-05-01 Pratt & Whitney Canada Corp. Rotor assembly with scoop
US10233764B2 (en) 2015-10-12 2019-03-19 Rolls-Royce North American Technologies Inc. Fabric seal and assembly for gas turbine engine
US10724540B2 (en) 2016-12-06 2020-07-28 Pratt & Whitney Canada Corp. Stator for a gas turbine engine fan
US10690146B2 (en) 2017-01-05 2020-06-23 Pratt & Whitney Canada Corp. Turbofan nacelle assembly with flow disruptor

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FR379209A (fr) * 1906-07-03 1907-10-29 Sebastian Ziani De Ferranti Perfectionnements aux turbines à fluide élastique
US885032A (en) * 1907-06-24 1908-04-21 Sebastian Ziani De Ferranti Fluid packing.
DE593417C (de) * 1931-07-18 1934-02-26 I G Farbenindustrie Akt Ges Verfahren zur Darstellung von 1-Amino-10-anthronen
US2859936A (en) * 1954-03-03 1958-11-11 Cincinnati Testing & Res Lab Compressor blade and method of forming same
US3117716A (en) * 1963-04-10 1964-01-14 Bell Aerospace Corp Ducted rotor
GB1237532A (en) * 1967-06-24 1971-06-30 Rolls Royce Improvements in turbines and compresser rotors
GB1303245A (de) * 1969-06-28 1973-01-17
GB1450553A (en) * 1973-11-23 1976-09-22 Rolls Royce Seals and a method of manufacture thereof
SU628323A2 (ru) * 1975-03-24 1978-10-15 Каунасский Политехнический Институт Имени Антанаса Снечкуса Устройство дл снижени аэродинамического шума
JPS5277908A (en) * 1975-12-24 1977-06-30 Mitsubishi Heavy Ind Ltd Vane for rotary machine
JPS5439207A (en) * 1977-09-02 1979-03-26 Hitachi Ltd A propeller fan and process for making the same
US4227703A (en) * 1978-11-27 1980-10-14 General Electric Company Gas seal with tip of abrasive particles
US4354804A (en) * 1979-11-30 1982-10-19 Williams Research Corporation Composite turbine wheel, method of manufacture and fixture therefor
GB2070700B (en) * 1980-03-01 1983-10-05 Rolls Royce Gas turbine seals
US4390320A (en) * 1980-05-01 1983-06-28 General Electric Company Tip cap for a rotor blade and method of replacement
US4589823A (en) * 1984-04-27 1986-05-20 General Electric Company Rotor blade tip
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DE3425162A1 (de) * 1984-07-07 1986-01-16 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Dichtung zwischen zwei maschinenteilen
SU1260554A1 (ru) * 1985-01-07 1986-09-30 Предприятие П/Я А-3513 Поворотно-лопастна гидромашина
SU1592522A1 (ru) * 1988-05-04 1990-09-15 Vladislav T Tomashevskij Лoпatka boздушhoгo haгhetateля
US5197281A (en) * 1990-04-03 1993-03-30 General Electric Company Interstage seal arrangement for airfoil stages of turbine engine counterrotating rotors
US5114159A (en) * 1991-08-05 1992-05-19 United Technologies Corporation Brush seal and damper
FR2682992B1 (fr) 1991-10-23 1995-04-21 Snecma Aubage de turbomachine en materiau composite a matrice a base d'un elastomere.
FR2684719B1 (fr) 1991-12-04 1994-02-11 Snecma Aube de turbomachine comprenant des nappes de materiau composite.
FR2691749B1 (fr) * 1992-05-27 1994-07-22 Snecma Dispositif d'etancheite entre des etages d'aubes et un tambour tournant notamment pour eviter les fuites autour des etages d'aubes de redresseur .

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102004050739A1 (de) * 2004-10-19 2006-04-20 Mtu Aero Engines Gmbh Turbomaschine, insbesondere Gasturbine
DE102004050739B4 (de) * 2004-10-19 2006-06-14 Mtu Aero Engines Gmbh Turbomaschine, insbesondere Gasturbine

Also Published As

Publication number Publication date
US5628622A (en) 1997-05-13
FR2724412B1 (fr) 1996-10-25
DE69506074D1 (de) 1998-12-24
EP0708227B1 (de) 1998-11-18
EP0708227A1 (de) 1996-04-24
FR2724412A1 (fr) 1996-03-15

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: SNECMA MOTEURS, PARIS, FR

8339 Ceased/non-payment of the annual fee