IT1164320B - Sistema di tenuta abrasiva ed abradibile per il percoroso dei gas in motori a turbina a gas - Google Patents

Sistema di tenuta abrasiva ed abradibile per il percoroso dei gas in motori a turbina a gas

Info

Publication number
IT1164320B
IT1164320B IT22263/83A IT2226383A IT1164320B IT 1164320 B IT1164320 B IT 1164320B IT 22263/83 A IT22263/83 A IT 22263/83A IT 2226383 A IT2226383 A IT 2226383A IT 1164320 B IT1164320 B IT 1164320B
Authority
IT
Italy
Prior art keywords
abradible
abrasive
gases
path
gas turbine
Prior art date
Application number
IT22263/83A
Other languages
English (en)
Other versions
IT8322263A0 (it
IT8322263A1 (it
Inventor
Lawrence Theodore Shiembob
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
Publication of IT8322263A0 publication Critical patent/IT8322263A0/it
Publication of IT8322263A1 publication Critical patent/IT8322263A1/it
Application granted granted Critical
Publication of IT1164320B publication Critical patent/IT1164320B/it

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
    • F01D11/08—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
    • F01D11/122—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 with erodable or abradable material
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • 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
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S277/00—Seal for a joint or juncture
    • Y10S277/922—Bonding or joining for manufacture of seal
    • 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
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S277/00—Seal for a joint or juncture
    • Y10S277/935—Seal made of a particular material
    • Y10S277/939—Containing metal
    • Y10S277/94—Alloy

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
  • Coating By Spraying Or Casting (AREA)
IT22263/83A 1982-08-09 1983-07-27 Sistema di tenuta abrasiva ed abradibile per il percoroso dei gas in motori a turbina a gas IT1164320B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/406,404 US4566700A (en) 1982-08-09 1982-08-09 Abrasive/abradable gas path seal system

Publications (3)

Publication Number Publication Date
IT8322263A0 IT8322263A0 (it) 1983-07-27
IT8322263A1 IT8322263A1 (it) 1985-01-27
IT1164320B true IT1164320B (it) 1987-04-08

Family

ID=23607838

Family Applications (1)

Application Number Title Priority Date Filing Date
IT22263/83A IT1164320B (it) 1982-08-09 1983-07-27 Sistema di tenuta abrasiva ed abradibile per il percoroso dei gas in motori a turbina a gas

Country Status (14)

Country Link
US (1) US4566700A (it)
JP (1) JPS5943265A (it)
BE (1) BE897337A (it)
CA (1) CA1246111A (it)
DE (1) DE3326535A1 (it)
ES (1) ES524398A0 (it)
FR (1) FR2531491A1 (it)
GB (1) GB2125119B (it)
IL (1) IL69236A (it)
IT (1) IT1164320B (it)
MX (1) MX162129A (it)
NL (1) NL190170C (it)
SE (1) SE453848B (it)
SG (1) SG64986G (it)

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US4713300A (en) * 1985-12-13 1987-12-15 Minnesota Mining And Manufacturing Company Graded refractory cermet article
US4784569A (en) * 1986-01-10 1988-11-15 General Electric Company Shroud means for turbine rotor blade tip clearance control
US4764089A (en) * 1986-08-07 1988-08-16 Allied-Signal Inc. Abradable strain-tolerant ceramic coated turbine shroud
FR2615254A1 (fr) * 1987-05-13 1988-11-18 Snecma Aube mobile de soufflante comportant une depouille en extremite
JPS6460701A (en) * 1987-08-31 1989-03-07 Toyota Motor Corp Flame coating film for controlling clearance gap
US4936745A (en) * 1988-12-16 1990-06-26 United Technologies Corporation Thin abradable ceramic air seal
JPH02143433U (it) * 1989-04-28 1990-12-05
JPH03156103A (ja) * 1989-11-10 1991-07-04 Toyota Motor Corp 相対移動装置
JPH0396601A (ja) * 1989-09-08 1991-04-22 Toyota Motor Corp 相対移動装置
IT216861Z2 (it) * 1989-09-18 1991-10-05 Sacchi Gian Galeazzo Dispositivo per il fissaggio di pannelli decorativi su parete o su intelaiatura metallica per la costituzione di facciate ornamentali ventilate.
US5143511A (en) * 1990-09-28 1992-09-01 Lamson Corporation Regenerative centrifugal compressor
JP2785087B2 (ja) * 1991-07-12 1998-08-13 プラクセア・エス・ティー・テクノロジー・インコーポレイテッド 炭化クロム−時効硬化性ニッケル基合金を被覆した回転シール部材
US5304032A (en) * 1991-07-22 1994-04-19 Bosna Alexander A Abradable non-metallic seal for rotating turbine engines
US5275531A (en) * 1993-04-30 1994-01-04 Teleflex, Incorporated Area ruled fan blade ends for turbofan jet engine
US5524846A (en) * 1993-12-21 1996-06-11 The Boeing Company Fire protection system for airplanes
US5607284A (en) * 1994-12-29 1997-03-04 United Technologies Corporation Baffled passage casing treatment for compressor blades
US5932356A (en) * 1996-03-21 1999-08-03 United Technologies Corporation Abrasive/abradable gas path seal system
US5976695A (en) * 1996-10-02 1999-11-02 Westaim Technologies, Inc. Thermally sprayable powder materials having an alloyed metal phase and a solid lubricant ceramic phase and abradable seal assemblies manufactured therefrom
DE19640979A1 (de) * 1996-10-04 1998-04-16 Asea Brown Boveri Bürstendichtung
US6186508B1 (en) * 1996-11-27 2001-02-13 United Technologies Corporation Wear resistant coating for brush seal applications
US5951892A (en) 1996-12-10 1999-09-14 Chromalloy Gas Turbine Corporation Method of making an abradable seal by laser cutting
US6057047A (en) * 1997-11-18 2000-05-02 United Technologies Corporation Ceramic coatings containing layered porosity
SG72959A1 (en) * 1998-06-18 2000-05-23 United Technologies Corp Article having durable ceramic coating with localized abradable portion
US6120242A (en) * 1998-11-13 2000-09-19 General Electric Company Blade containing turbine shroud
US20040124231A1 (en) * 1999-06-29 2004-07-01 Hasz Wayne Charles Method for coating a substrate
US6451454B1 (en) * 1999-06-29 2002-09-17 General Electric Company Turbine engine component having wear coating and method for coating a turbine engine component
EP1152124A1 (de) * 2000-05-04 2001-11-07 Siemens Aktiengesellschaft Dichtungsanordnung
US6365222B1 (en) 2000-10-27 2002-04-02 Siemens Westinghouse Power Corporation Abradable coating applied with cold spray technique
GB2399777A (en) * 2002-11-01 2004-09-29 Rolls Royce Plc Abradable seals for gas turbine engines
DE102004034312A1 (de) * 2004-07-15 2006-02-02 Mtu Aero Engines Gmbh Dichtungsanordnung und Verfahren zur Herstellung eines Dichtkörpers für eine Dichtungsanordnung
US20060249911A1 (en) * 2005-05-04 2006-11-09 General Electric Company Abradable and/or abrasive coating and brush seal configuration
JP4886271B2 (ja) * 2005-10-31 2012-02-29 株式会社東芝 蒸気タービンおよびその親水性コーティング材料
JP4718991B2 (ja) 2005-12-22 2011-07-06 株式会社東芝 シール装置
US8100640B2 (en) 2007-10-25 2012-01-24 United Technologies Corporation Blade outer air seal with improved thermomechanical fatigue life
DE102007056452A1 (de) * 2007-11-23 2009-05-28 Mtu Aero Engines Gmbh Dichtsystem einer Turbomaschine
US7998604B2 (en) * 2007-11-28 2011-08-16 United Technologies Corporation Article having composite layer
GB0911500D0 (en) 2009-07-03 2009-08-12 Rolls Royce Plc Rotor blade over-tip leakage control
US20110086163A1 (en) * 2009-10-13 2011-04-14 Walbar Inc. Method for producing a crack-free abradable coating with enhanced adhesion
US20130140774A1 (en) * 2010-01-13 2013-06-06 Dresser-Rand Company Annular seal apparatus and method
US9598972B2 (en) 2010-03-30 2017-03-21 United Technologies Corporation Abradable turbine air seal
US8562290B2 (en) * 2010-04-01 2013-10-22 United Technologies Corporation Blade outer air seal with improved efficiency
US9199227B2 (en) 2011-08-23 2015-12-01 Advanced Ceramic Fibers, Llc Methods of producing continuous boron carbide fibers
US8940391B2 (en) 2010-10-08 2015-01-27 Advanced Ceramic Fibers, Llc Silicon carbide fibers and articles including same
US10954167B1 (en) 2010-10-08 2021-03-23 Advanced Ceramic Fibers, Llc Methods for producing metal carbide materials
US10208238B2 (en) 2010-10-08 2019-02-19 Advanced Ceramic Fibers, Llc Boron carbide fiber reinforced articles
US9803296B2 (en) 2014-02-18 2017-10-31 Advanced Ceramic Fibers, Llc Metal carbide fibers and methods for their manufacture
US9275762B2 (en) 2010-10-08 2016-03-01 Advanced Ceramic Fibers, Llc Cladding material, tube including such cladding material and methods of forming the same
US20130216798A1 (en) * 2012-02-17 2013-08-22 General Electric Company Coated article and process of coating an article
US9528008B2 (en) 2013-03-07 2016-12-27 United Technologies Corporation Lightweight and corrosion resistant abradable coating
GB201405704D0 (en) 2014-03-31 2014-05-14 Rolls Royce Plc Gas turbine engine
US10174481B2 (en) * 2014-08-26 2019-01-08 Cnh Industrial America Llc Shroud wear ring for a work vehicle
GB201415201D0 (en) * 2014-08-28 2014-10-15 Rolls Royce Plc A wear monitor for a gas turbine engine fan
EP3015715A1 (de) * 2014-10-27 2016-05-04 MTU Aero Engines GmbH Leitschaufelkranz für eine strömungsmaschine und strömungsmaschine
US10450876B2 (en) * 2015-04-15 2019-10-22 United Technologies Corporation Abrasive tip blade manufacture methods
US10030532B2 (en) * 2015-04-22 2018-07-24 United Technologies Corporation Abradable seal with thermally conductive microspheres
US10793478B2 (en) 2017-09-11 2020-10-06 Advanced Ceramic Fibers, Llc. Single phase fiber reinforced ceramic matrix composites
US11149744B2 (en) * 2017-09-19 2021-10-19 Raytheon Technologies Corporation Turbine engine seal for high erosion environment
FR3099187B1 (fr) * 2019-07-26 2023-05-26 Safran Aircraft Engines Revêtement abradable
DE102021211656A1 (de) 2021-10-15 2023-04-20 Siemens Energy Global GmbH & Co. KG Dichtungsbereich zwischen rotierenden und stehenden Komponenten, Verfahren zur Herstellung und Maschine

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US2886352A (en) * 1956-10-16 1959-05-12 Stackpole Carbon Co Shaft seal
US3147087A (en) * 1959-02-19 1964-09-01 Gen Electric Controlled density heterogeneous material and article
US3339933A (en) * 1965-02-24 1967-09-05 Gen Electric Rotary seal
US3519282A (en) * 1966-03-11 1970-07-07 Gen Electric Abradable material seal
US3575427A (en) * 1969-11-03 1971-04-20 United Aircraft Corp Composite abradable seal
US3625634A (en) * 1969-12-10 1971-12-07 Gen Motors Corp Turbomachine rotor
US3844011A (en) * 1970-12-21 1974-10-29 Gould Inc Powder metal honeycomb
US3880550A (en) * 1974-02-22 1975-04-29 Us Air Force Outer seal for first stage turbine
US4422648A (en) * 1982-06-17 1983-12-27 United Technologies Corporation Ceramic faced outer air seal for gas turbine engines

Also Published As

Publication number Publication date
CA1246111A (en) 1988-12-06
SE8303868D0 (sv) 1983-07-06
SE8303868L (sv) 1984-02-10
DE3326535A1 (de) 1984-03-01
ES8405910A1 (es) 1984-07-01
ES524398A0 (es) 1984-07-01
SG64986G (en) 1987-03-27
IL69236A (en) 1990-12-23
GB8317918D0 (en) 1983-08-03
BE897337A (fr) 1983-11-14
GB2125119B (en) 1986-03-05
US4566700A (en) 1986-01-28
NL8302477A (nl) 1984-03-01
SE453848B (sv) 1988-03-07
JPS5943265A (ja) 1984-03-10
DE3326535C2 (it) 1988-04-07
MX162129A (es) 1991-04-01
IL69236A0 (en) 1983-11-30
IT8322263A0 (it) 1983-07-27
FR2531491A1 (fr) 1984-02-10
NL190170C (nl) 1993-11-16
NL190170B (nl) 1993-06-16
JPS6323428B2 (it) 1988-05-16
IT8322263A1 (it) 1985-01-27
FR2531491B1 (it) 1985-04-19
GB2125119A (en) 1984-02-29

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