BR0101314B1 - método para revestir simultaneamente com fase de vapor as superfìcies de aerofólio de trajetória de fluxo e as superfìcies de plataforma superiores de uma pluralidade de aerofólios de turbina, aparelho de receptáculo de seções de prisma e conjunto de revestimento de aerofólio de turbina. - Google Patents

método para revestir simultaneamente com fase de vapor as superfìcies de aerofólio de trajetória de fluxo e as superfìcies de plataforma superiores de uma pluralidade de aerofólios de turbina, aparelho de receptáculo de seções de prisma e conjunto de revestimento de aerofólio de turbina.

Info

Publication number
BR0101314B1
BR0101314B1 BRPI0101314-9A BR0101314A BR0101314B1 BR 0101314 B1 BR0101314 B1 BR 0101314B1 BR 0101314 A BR0101314 A BR 0101314A BR 0101314 B1 BR0101314 B1 BR 0101314B1
Authority
BR
Brazil
Prior art keywords
airfoil
turbine
coating
flow path
vapor phase
Prior art date
Application number
BRPI0101314-9A
Other languages
English (en)
Other versions
BR0101314A (pt
Inventor
Gary Eugene Wheat
Terri Kay Brown
Steve Earl Bauer
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 filed Critical
Publication of BR0101314A publication Critical patent/BR0101314A/pt
Publication of BR0101314B1 publication Critical patent/BR0101314B1/pt

Links

Classifications

    • 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
    • C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/04—Coating on selected surface areas, e.g. using masks
    • C23C14/042—Coating on selected surface areas, e.g. using masks using masks
    • 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
    • C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
    • C23C10/04—Diffusion into selected surface areas, e.g. using masks
    • 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
    • C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
    • C23C14/50—Substrate holders

Landscapes

  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Details Or Accessories Of Spraying Plant Or Apparatus (AREA)
BRPI0101314-9A 2000-04-07 2001-04-04 método para revestir simultaneamente com fase de vapor as superfìcies de aerofólio de trajetória de fluxo e as superfìcies de plataforma superiores de uma pluralidade de aerofólios de turbina, aparelho de receptáculo de seções de prisma e conjunto de revestimento de aerofólio de turbina. BR0101314B1 (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/545,542 US6419753B1 (en) 2000-04-07 2000-04-07 Apparatus and method for masking multiple turbine components

Publications (2)

Publication Number Publication Date
BR0101314A BR0101314A (pt) 2001-11-06
BR0101314B1 true BR0101314B1 (pt) 2009-08-11

Family

ID=24176646

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0101314-9A BR0101314B1 (pt) 2000-04-07 2001-04-04 método para revestir simultaneamente com fase de vapor as superfìcies de aerofólio de trajetória de fluxo e as superfìcies de plataforma superiores de uma pluralidade de aerofólios de turbina, aparelho de receptáculo de seções de prisma e conjunto de revestimento de aerofólio de turbina.

Country Status (5)

Country Link
US (2) US6419753B1 (pt)
EP (1) EP1143032B1 (pt)
BR (1) BR0101314B1 (pt)
DE (1) DE60130703T2 (pt)
SG (1) SG91909A1 (pt)

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GB0026549D0 (en) * 2000-10-31 2000-12-13 Fotolec Technologies Plc Apparatus and methods for use in coating articles
US6769877B2 (en) 2002-10-18 2004-08-03 General Electric Company Undercut leading edge for compressor blades and related method
US7121803B2 (en) * 2002-12-26 2006-10-17 General Electric Company Compressor blade with dovetail slotted to reduce stress on the airfoil leading edge
US6902376B2 (en) 2002-12-26 2005-06-07 General Electric Company Compressor blade with dovetail slotted to reduce stress on the airfoil leading edge
US7122224B2 (en) * 2003-06-11 2006-10-17 General Electric Company Methods and apparatus for turbine engine component coating
FR2863191B1 (fr) * 2003-12-04 2007-04-20 Snecma Moteurs Masque de protection pour le traitement de surface d'aubes de turbomachines
US7104759B2 (en) * 2004-04-01 2006-09-12 General Electric Company Compressor blade platform extension and methods of retrofitting blades of different blade angles
JP4384109B2 (ja) 2005-01-05 2009-12-16 三星モバイルディスプレイ株式會社 蒸着システム用蒸着源の駆動軸及びこれを具備した蒸着システム
US20060193981A1 (en) * 2005-02-25 2006-08-31 General Electric Company Apparatus and method for masking vapor phase aluminide coating to achieve internal coating of cooling passages
US7371428B2 (en) * 2005-11-28 2008-05-13 Howmet Corporation Duplex gas phase coating
US7632541B2 (en) * 2006-03-13 2009-12-15 General Electric Company Method and device to prevent coating a dovetail of a turbine airfoil
DE102006033047A1 (de) * 2006-07-14 2008-01-24 Viktor Georgiev Abdeckbauteil zum Maskieren von Oberflächen zu behandelnden Werkstücken
US8353259B2 (en) * 2007-08-24 2013-01-15 United Technologies Corporation Masking fixture for a coating process
US8173218B2 (en) * 2007-10-24 2012-05-08 United Technologies Corporation Method of spraying a turbine engine component
DE102008011242A1 (de) * 2008-02-14 2009-08-20 Mtu Aero Engines Gmbh Vorrichtung und Verfahren zur partiellen Beschichtung von Bauteilen
DE102008053394A1 (de) * 2008-10-27 2010-04-29 Mtu Aero Engines Gmbh Vorrichtung zum partiellen Abdecken einer Bauteilzone
GB0902633D0 (en) 2009-02-18 2009-04-01 Rolls Royce Plc A method and an arrangement for vapour phase coating of an internal surface of at least one hollow article
US8967078B2 (en) * 2009-08-27 2015-03-03 United Technologies Corporation Abrasive finish mask and method of polishing a component
EP2359940A1 (en) * 2010-02-12 2011-08-24 Siemens Aktiengesellschaft Overspray shielding device and method
FR2959528B1 (fr) * 2010-04-29 2012-06-08 Snecma Masque amovible pour une plate-forme d'aube ou de secteur de distributeur de turbomachine
US9121091B2 (en) 2012-01-19 2015-09-01 United Technologies Corporation Turbine airfoil mask
FR3047255B1 (fr) * 2016-01-28 2018-01-12 Snecma Mexico, S.A. De C.V. Outillage pour la mise en oeuvre d'un procede de depot d'un revetement metallique en phase vapeur sur des pieces de turbomachine
DE102016110799A1 (de) * 2016-06-13 2017-12-14 Cavonic GmbH Verfahren und Vorrichtung zum Beschichten von Kunststoffausgießern
US10570753B2 (en) 2017-01-23 2020-02-25 United Technologies Corporation Apparatus and method for masking under platform areas of airfoil components
US11566529B2 (en) 2017-08-22 2023-01-31 General Electric Company Turbine component with bounded wear coat
US20190194799A1 (en) 2017-12-22 2019-06-27 United Technologies Corporation Line-of-sight coating fixture and apparatus
CN109382769A (zh) * 2018-12-25 2019-02-26 深圳仕上电子科技有限公司 喷砂保护治具
CN113215523B (zh) * 2021-04-12 2022-04-12 龚雅斌 一种新型人民防空战时通风设备合金共渗工艺

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US4271005A (en) 1979-12-03 1981-06-02 United Technologies Corporation Workpiece support apparatus for use with cathode sputtering devices
US5128179A (en) * 1981-07-08 1992-07-07 Alloy Surfaces Company, Inc. Metal diffusion and after-treatment
US4485759A (en) 1983-01-19 1984-12-04 Multi-Arc Vacuum Systems Inc. Planetary substrate support apparatus for vapor vacuum deposition coating
US4671968A (en) 1985-04-01 1987-06-09 Macdermid, Incorporated Method for electroless deposition of copper on conductive surfaces and on substrates containing conductive surfaces
GB2210387B (en) 1987-09-30 1992-03-11 Rolls Royce Plc Chemical vapour deposition
DE4425991C1 (de) 1994-07-22 1995-12-07 Mtu Muenchen Gmbh Vorrichtung und Verfahren zur partiellen Beschichtung von Bauteilgruppen
US5792267A (en) * 1997-05-16 1998-08-11 United Technologies Corporation Coating fixture for a turbine engine blade
US6037004A (en) * 1997-12-19 2000-03-14 United Technologies Corporation Shield and method for protecting an airfoil surface
US6039810A (en) * 1998-11-13 2000-03-21 General Electric Company High temperature vapor coating container
US6224673B1 (en) 1999-08-11 2001-05-01 General Electric Company Apparatus for masking turbine components during vapor phase diffusion coating

Also Published As

Publication number Publication date
EP1143032B1 (en) 2007-10-03
BR0101314A (pt) 2001-11-06
US6706323B2 (en) 2004-03-16
SG91909A1 (en) 2002-10-15
DE60130703T2 (de) 2008-07-24
EP1143032A1 (en) 2001-10-10
DE60130703D1 (de) 2007-11-15
US20020098284A1 (en) 2002-07-25
US6419753B1 (en) 2002-07-16

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Legal Events

Date Code Title Description
B06A Notification to applicant to reply to the report for non-patentability or inadequacy of the application [chapter 6.1 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 04/04/2001, OBSERVADAS AS CONDICOES LEGAIS.

B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time
B24J Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12)