DE69107944D1 - Verfahren und Vorrichtung für die Statoranordnung einer rotierenden Maschine. - Google Patents

Verfahren und Vorrichtung für die Statoranordnung einer rotierenden Maschine.

Info

Publication number
DE69107944D1
DE69107944D1 DE69107944T DE69107944T DE69107944D1 DE 69107944 D1 DE69107944 D1 DE 69107944D1 DE 69107944 T DE69107944 T DE 69107944T DE 69107944 T DE69107944 T DE 69107944T DE 69107944 D1 DE69107944 D1 DE 69107944D1
Authority
DE
Germany
Prior art keywords
rotating machine
stator arrangement
stator
arrangement
rotating
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
DE69107944T
Other languages
English (en)
Other versions
DE69107944T2 (de
Inventor
Allen W Brown
Raymond A Wolf
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Application granted granted Critical
Publication of DE69107944D1 publication Critical patent/DE69107944D1/de
Publication of DE69107944T2 publication Critical patent/DE69107944T2/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
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
    • F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
    • 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
    • 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
    • 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
    • Y10T29/49229—Prime mover or fluid pump making
    • Y10T29/49297—Seal or packing making
    • 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)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE69107944T 1990-09-25 1991-09-19 Verfahren und Vorrichtung für die Statoranordnung einer rotierenden Maschine. Expired - Fee Related DE69107944T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US58771590A 1990-09-25 1990-09-25

Publications (2)

Publication Number Publication Date
DE69107944D1 true DE69107944D1 (de) 1995-04-13
DE69107944T2 DE69107944T2 (de) 1995-07-13

Family

ID=24350905

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69107944T Expired - Fee Related DE69107944T2 (de) 1990-09-25 1991-09-19 Verfahren und Vorrichtung für die Statoranordnung einer rotierenden Maschine.

Country Status (5)

Country Link
US (1) US5281089A (de)
EP (1) EP0478494B1 (de)
JP (1) JP3213623B2 (de)
DE (1) DE69107944T2 (de)
IE (1) IE67360B1 (de)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5702050A (en) * 1995-04-28 1997-12-30 Mitsubishi Jukogyo Kabushiki Kaisha Method of brazing a honeycomb
DE19828065A1 (de) * 1998-06-24 1999-12-30 Bmw Rolls Royce Gmbh Wabenstruktur-Dichtung insbesondere für eine Gasturbine
US6120242A (en) * 1998-11-13 2000-09-19 General Electric Company Blade containing turbine shroud
US6202302B1 (en) * 1999-07-02 2001-03-20 United Technologies Corporation Method of forming a stator assembly for rotary machine
JP4285134B2 (ja) * 2003-07-04 2009-06-24 株式会社Ｉｈｉ シュラウドセグメント
DE102004010236A1 (de) * 2004-03-03 2005-09-15 Mtu Aero Engines Gmbh Ringstruktur in Metallbauweise
US8074998B2 (en) * 2006-05-05 2011-12-13 The Texas A&M University System Annular seals for non-contact sealing of fluids in turbomachinery
US7523552B2 (en) * 2007-05-30 2009-04-28 United Technologies Corporation Milling bleed holes into honeycomb process
US8608424B2 (en) * 2009-10-09 2013-12-17 General Electric Company Contoured honeycomb seal for a turbomachine
US8966756B2 (en) 2011-01-20 2015-03-03 United Technologies Corporation Gas turbine engine stator vane assembly
US9121283B2 (en) 2011-01-20 2015-09-01 United Technologies Corporation Assembly fixture with wedge clamps for stator vane assembly
US8966755B2 (en) 2011-01-20 2015-03-03 United Technologies Corporation Assembly fixture for a stator vane assembly
US9434031B2 (en) 2012-09-26 2016-09-06 United Technologies Corporation Method and fixture for airfoil array assembly
FR3025124B1 (fr) * 2014-08-28 2016-09-30 Snecma Procede de fabrication de supports d'anneaux d'organe de turbomachine
CN109894805A (zh) * 2017-12-11 2019-06-18 南通虹波机械有限公司 一种大型齿轮密封装置的制备方法
DE102018210601A1 (de) * 2018-06-28 2020-01-02 MTU Aero Engines AG Segmentring zur montage in einer strömungsmaschine

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3156041A (en) * 1960-04-18 1964-11-10 Frank M Gault Method of soldering and brazing structural elements
FR1470032A (fr) * 1965-02-24 1967-02-17 Gen Electric Joint rotatif d'étanchéité
US3501089A (en) * 1968-07-17 1970-03-17 Gen Electric Jet pump ejector
FR2452601A1 (fr) * 1979-03-30 1980-10-24 Snecma Support amovible de revetement d'etancheite pour carter de soufflante de turboreacteur
US4522859A (en) * 1979-10-29 1985-06-11 Rohr Industries, Inc. Method of manufacture of honeycomb noise attenuation structure for high temperature applications
US4512712A (en) * 1983-08-01 1985-04-23 United Technologies Corporation Turbine stator assembly
US4525997A (en) * 1983-08-01 1985-07-02 United Technologies Corporation Stator assembly for bounding the flow path of a gas turbine engine
US4652209A (en) * 1985-09-13 1987-03-24 Rockwell International Corporation Knurled turbine tip seal
US4767267A (en) * 1986-12-03 1988-08-30 General Electric Company Seal assembly
US4897021A (en) * 1988-06-02 1990-01-30 United Technologies Corporation Stator vane asssembly for an axial flow rotary machine
FR2635562B1 (fr) * 1988-08-18 1993-12-24 Snecma Anneau de stator de turbine associe a un support de liaison au carter de turbine

Also Published As

Publication number Publication date
EP0478494B1 (de) 1995-03-08
DE69107944T2 (de) 1995-07-13
IE67360B1 (en) 1996-03-20
US5281089A (en) 1994-01-25
JP3213623B2 (ja) 2001-10-02
EP0478494A1 (de) 1992-04-01
JPH04279734A (ja) 1992-10-05
IE913106A1 (en) 1992-02-25

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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