[go: up one dir, main page]

GB1150006A - Improvements in or relating to protection coatings for high temperature alloys - Google Patents

Improvements in or relating to protection coatings for high temperature alloys

Info

Publication number
GB1150006A
GB1150006A GB35965/66A GB3596566A GB1150006A GB 1150006 A GB1150006 A GB 1150006A GB 35965/66 A GB35965/66 A GB 35965/66A GB 3596566 A GB3596566 A GB 3596566A GB 1150006 A GB1150006 A GB 1150006A
Authority
GB
United Kingdom
Prior art keywords
layer
article
mixture
powder
heating
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
Application number
GB35965/66A
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.)
RTX Corp
Original Assignee
United Aircraft 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 Aircraft Corp filed Critical United Aircraft Corp
Publication of GB1150006A publication Critical patent/GB1150006A/en
Expired legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C32/00Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ
    • C22C32/001Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with only oxides
    • C22C32/0015Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with only oxides with only single oxides as main non-metallic constituents
    • C22C32/0026Matrix based on Ni, Co, Cr or alloys thereof
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C10/00Solid state diffusion of only metal elements or silicon into metallic material surfaces
    • C23C10/28Solid state diffusion of only metal elements or silicon into metallic material surfaces using solids, e.g. powders, pastes
    • C23C10/34Embedding in a powder mixture, i.e. pack cementation
    • C23C10/52Embedding in a powder mixture, i.e. pack cementation more than one element being diffused in one step
    • C23C10/54Diffusion of at least chromium
    • C23C10/56Diffusion of at least chromium and at least aluminium
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S428/00Stock material or miscellaneous articles
    • Y10S428/922Static electricity metal bleed-off metallic stock
    • Y10S428/923Physical dimension
    • Y10S428/924Composite
    • Y10S428/926Thickness of individual layer specified
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/1266O, S, or organic compound in metal component
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12736Al-base component
    • Y10T428/12743Next to refractory [Group IVB, VB, or VIB] metal-base component
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12736Al-base component
    • Y10T428/1275Next to Group VIII or IB metal-base component
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12771Transition metal-base component
    • Y10T428/12806Refractory [Group IVB, VB, or VIB] metal-base component
    • Y10T428/12826Group VIB metal-base component
    • Y10T428/12847Cr-base component
    • Y10T428/12854Next to Co-, Fe-, or Ni-base component

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

1,150,006. Diffusion coating; dispersion strengthened nickel alloys. UNITED AIRCRAFT CORP. Aug.11, 1966 [Aug.16, 1965], No.35965/66. Headings C7A and C7F. A Ni-, Co- or Febase heat resistant alloy article, e.g. a gas-turbine blade or vane, is protected against oxidation, corrosion and erosion at operating temperatures above 1200‹C. while subjected to combustion gases by contacting it first with a finely divided mixture comprising Cr powder and a halogen-bearing compound as activator and heating between 982‹ C . and the melting point of the alloy (1454‹C. for Ni-base alloy) to provide an adherent Cr layer, then with a similar mixture, but additionally containing Al powder, and heating between 538‹C. and the melting point of the alloy to provide an adherent Cr-Al (aluminide) layer on the Cr layer. The diffusion heating is conducted in the absence of deleterious gas, e.g. under vacuum or in an atmosphere of He, A and/or H 2 . The mixture may be in powder pack form and the article immersed therein, or the article may be coated with an aqueous slurry of the mixture and dried, prior to diffusion heating. Either mixture may also contain an inert filler powder such as alumina, zirconia, titania, ceria, magnesia, hafnia or rare earth metal oxide. The activator powder may be CrCl 3 , CrBr 3 , CrI 3 , CrF 3 , NaCl, KCl, KF, NH 4 Cl, NH 4 I or NH 4 Br. The article may be of dispersion strengthened Ni-base alloy containing at least 60% Ni, 0À02 to 20% of dispersed ThO 2 , Al 2 O 3 , ZrO 2 , TiO 2 , MgO, HfO 2 or rare earth metal oxide, and balance Fe, Co, Al, Cu, Cr, Mo, W, Ti, Ta and/or Re; e.g. 2% ThO 2 20% Cr and/or 15% Mo, balance Ni. Where a Ni-base alloy article is chromized at a rate in excess of that at which Cr diffuses in the Ni, a discrete body-centered-cubic Cr layer is formed; this layer is absent where the Cr is deposited at the same rate as the diffusion rate. In either case, outer layers comprise a layer of Ni 3 Al + Cr (bonded over the layer of Cr containing Al and/or Ni, or a layer of Al + Ni - Cr) over which is bonded a layer of NiAl + Cr. The chromium layer may have a thickness of 2.54.10<SP>-</SP><SP>3</SP> to 2.54.10 <SP>2</SP> cm.
GB35965/66A 1965-08-16 1966-08-11 Improvements in or relating to protection coatings for high temperature alloys Expired GB1150006A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US48002965A 1965-08-16 1965-08-16

Publications (1)

Publication Number Publication Date
GB1150006A true GB1150006A (en) 1969-04-30

Family

ID=23906390

Family Applications (1)

Application Number Title Priority Date Filing Date
GB35965/66A Expired GB1150006A (en) 1965-08-16 1966-08-11 Improvements in or relating to protection coatings for high temperature alloys

Country Status (4)

Country Link
US (1) US3556744A (en)
DE (1) DE1521570C3 (en)
FR (1) FR1511571A (en)
GB (1) GB1150006A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2394960B (en) * 2002-11-04 2007-04-25 Doncasters Ltd High temperature alloys
CN114667365A (en) * 2019-11-05 2022-06-24 赛峰集团 Superalloy aircraft component comprising a cooling channel

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3649883A (en) * 1970-08-17 1972-03-14 Motorola Inc Semiconductor device having a recombination ring
US3779719A (en) * 1970-12-03 1973-12-18 Chromalloy American Corp Diffusion coating of jet engine components and like structures
US4142023A (en) * 1975-12-16 1979-02-27 United Technologies Corporation Method for forming a single-phase nickel aluminide coating on a nickel-base superalloy substrate
US4528043A (en) * 1982-05-14 1985-07-09 Rolls-Royce Limited Surface oxide layer treatment
WO1992016670A2 (en) * 1991-03-14 1992-10-01 The Dow Chemical Company Methods for alloying a metal-containing material into a densified ceramic or cermet body and alloyed bodies produced thereby
US7390535B2 (en) 2003-07-03 2008-06-24 Aeromet Technologies, Inc. Simple chemical vapor deposition system and methods for depositing multiple-metal aluminide coatings
DE102009002868A1 (en) * 2009-05-06 2010-11-18 Inncoa Gmbh Method for applying a multi-layered layer structure to a substrate and substrate having a multi-layered layer structure
DE102012109782A1 (en) * 2012-10-15 2014-04-17 Karlsruher Institut für Technologie layer composite

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2394960B (en) * 2002-11-04 2007-04-25 Doncasters Ltd High temperature alloys
CN114667365A (en) * 2019-11-05 2022-06-24 赛峰集团 Superalloy aircraft component comprising a cooling channel

Also Published As

Publication number Publication date
DE1521570B2 (en) 1973-02-01
US3556744A (en) 1971-01-19
DE1521570C3 (en) 1973-09-13
FR1511571A (en) 1968-02-02
DE1521570A1 (en) 1969-05-29

Similar Documents

Publication Publication Date Title
US3754903A (en) High temperature oxidation resistant coating alloy
US4095003A (en) Duplex coating for thermal and corrosion protection
US3649225A (en) Composite coating for the superalloys
Rhys-Jones Coatings for blade and vane applications in gas turbines
US6332926B1 (en) Apparatus and method for selectively coating internal and external surfaces of an airfoil
US4198442A (en) Method for producing elevated temperature corrosion resistant articles
US3951642A (en) Metallic coating powder containing Al and Hf
US4145481A (en) Process for producing elevated temperature corrosion resistant metal articles
USRE31339E (en) Process for producing elevated temperature corrosion resistant metal articles
US4897315A (en) Yttrium enriched aluminide coating for superalloys
US4070507A (en) Platinum-rhodium-containing high temperature alloy coating method
US6273678B1 (en) Modified diffusion aluminide coating for internal surfaces of gas turbine components
US4086391A (en) Alumina forming coatings containing hafnium for high temperature applications
EP3094758B1 (en) Modified slurry compositions for forming improved chromium diffusion coatings
JPS6013056B2 (en) coated superalloy
WO1985004428A1 (en) Process for preparing high temperature materials
US9689270B2 (en) Duplex-phase CrAl coating for improved corrosion/oxidation protection
GB1466204A (en) Electrophoretic deposition of ductile corrosion resistant metallic coatings
GB1150006A (en) Improvements in or relating to protection coatings for high temperature alloys
Nesbitt et al. Modeling degradation and failure of Ni-Cr-Al overlay coatings
GB1602040A (en) Process for producing protective coatings on metals and metal alloys for use at high temperatures
JPS6039173A (en) High temperature protecting layer
US3996021A (en) Metallic coated article with improved resistance to high temperature environmental conditions
US4071638A (en) Method of applying a metallic coating with improved resistance to high temperature to environmental conditions
US20020023696A1 (en) Formation of an aluminide coating, incorporating a reactive element, on a metal substrate

Legal Events

Date Code Title Description
PS Patent sealed
PLNP Patent lapsed through nonpayment of renewal fees