IL35730A - A method of producing protective diffusion layers on the surface of cobalt-based alloys - Google Patents

A method of producing protective diffusion layers on the surface of cobalt-based alloys

Info

Publication number
IL35730A
IL35730A IL35730A IL3573070A IL35730A IL 35730 A IL35730 A IL 35730A IL 35730 A IL35730 A IL 35730A IL 3573070 A IL3573070 A IL 3573070A IL 35730 A IL35730 A IL 35730A
Authority
IL
Israel
Prior art keywords
nickel
metals
aluminium
layer
group
Prior art date
Application number
IL35730A
Other languages
Hebrew (he)
Other versions
IL35730A0 (en
Original Assignee
Deutsche Edelstahlwerke Ag
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 Deutsche Edelstahlwerke Ag filed Critical Deutsche Edelstahlwerke Ag
Publication of IL35730A0 publication Critical patent/IL35730A0/en
Publication of IL35730A publication Critical patent/IL35730A/en

Links

Classifications

    • 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
    • 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
    • Y10S428/9335Product by special process
    • Y10S428/941Solid state alloying, e.g. diffusion, to disappearance of an original layer
    • 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
    • Y10T428/12861Group VIII or IB metal-base component
    • Y10T428/12868Group IB metal-base component alternative to platinum group metal-base component [e.g., precious metal, etc.]
    • 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
    • Y10T428/12861Group VIII or IB metal-base component
    • Y10T428/12944Ni-base component

Landscapes

  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Electroplating Methods And Accessories (AREA)
  • Solid-Phase Diffusion Into Metallic Material Surfaces (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Electroplating And Plating Baths Therefor (AREA)

Description

A method of producing protective diffusion layers on the surface of cobalt-based alloys This invention relates to a method of producing on the surface of parts made of cobalt-based alloys protective, diffusion layers that are resistant at high temperatures to oxidation, scaling and corrosion.
It is a known practice to protect objects, for example turbine blades for jet propulsion engines which usually consist of high temperature metal alloys, from oxidation, scaling and corrosion, by diffusing aluminium into their surfaces thereby to provide a protective layer thereon.
The object of the present invention is to provide on parts made of high temperature metals, particularly cobalt-based alloys, a protective layer which imparts improved resistance to oxidation, scaling and corrosion at high temperatures.
For achieving this object the present invention consists in applying to the parts, possibly after they have been previously cleaned and degreased, nickel, one or more metals of the platinum group of metals of the Periodic System of Elements, (preferably platinum), and aluminium, either simultaneously or in succession, and to diffuse the said metals into the surface of the parts .
In a useful embodiment of the method of the invention, layers of nickel, of metal(s) of the platinum group and of aluminium may be consecutively applied to the surface of the part, for example by mechanical or electrolytic means, dipping, spraying formed diffused severally or jointly into the surface of the part by a diffusion heat treatment.
In an alternative method of carrying out the invention a layer of nickel and then a layer of one or more metals of the platinum group may be electro-lytically deposited and the aluminium then deposited from a gas phase on the surface of the part and diffused into the surface of the part together with the nickel and the metal(s) of the platinum group. With advantage the part that has first been provided with a nickel layer and then with a layer of metal (s) of the platinum group, may be embedded in a powder mixture containing metallic aluminium possibly associated with a small proportion of a metal halide and an inert filler (e.g. alumina), the aluminium being then deposited on the part from a gas phase and finally diffused into the surface of the part together with the nickel and the metal(s) of the platinum group. Such a mixture may for example comprise about 5 of aluminium and about 95 of the inert filler.
Cobalt-based alloys that have been provided with a protective diffusion layer according to the invention last about twice as long as similar parts that have been provided with a protective aluminium diffusion layer without nickel and platinum. The graph of the accompanying drawing having time on the abscissa and change in weight on the ordinate shows, as a function of operating been aluminised by a conventional method, and that have been protected by the method according to the invention. It will be seen that the reduction in weight which indicates the rate at which material is lost from the surface of the tested part by oxidation, scaling and corrosion, is less for parts protected according to the invention than parts that have been merely aluminised, and that their useful life of 600 to 700 hours in scaling test when exposed to burnt natural gas at 1100°C with an air factor of I.2, is twice as long. The material of all the tested parts was a cobalt alloy containing 0, 5 carbon, less than 0.5$ silicon, less than 0.5$ manganese, 21.0$ chromium, less than 1.0$ nickel, II.0$ tungsten, 2.0$ niobium tantalum, 1.75$ iron, balance cobalt. The protective treatment of the parts according to the invention was as follows Preliminary surface treatment Wet sand blasting and degreasing in a cyanide, copper-free degreasing bath cathodically for 5 seconds and anodically for 15 seconds, at a temperature of 20°C and current density of 5 amps/sq.dm., followed by pickling in a 10$ sulphuric acid for 10 seconds at 40°C, without the application of current, then washing in warm water at 45°C.
Nickel deposition Electrolytic composition of bath:- 240 g/litre of nickel chloride (NiCl2.H20) 120 g/litre of 36$ hydrochloric acid. 45°C and current density 10 - 11 amps/sq.dm.
Thickness of nickel deposit 20 )i Heat treatment 2 hours at 260°C followed by 3 hours at 450°C.
Preliminary surface treatment of the nickel before Platinisation Degreasing in a cyanide degreasing bath as hereinbefore described cathodically 10 seconds, anodically 20 seconds and cathodically 10 seconds at a temperature of 20°C and a current density of amps/sq.dm., followed by pickling in 10$ by weight caustic soda cathodically 3 seconds and anodically 10 seconds at a temperature of 50°C and a current density of 10 amps/sq.dm., followed by pickling in 4- o hydrochloric acid cathodically 2 seconds and anodically 30 seconds at a temperature of 40°C and a current density of 2.5 amps/sq.dm., followed by washing in warm water at 75°C.
Platinum deposition Electrolytic composition of bath:- 13 g/litre of hexachloroplatinic acid, !^PtClg. 45 g/litre of triammonium phosphate, (NH^)^PO^. 240 g/litre of dis odium phosphate, NagHPO^.
Conditions of electrolysis:- temperature 75°C and current density 5.5 amps/sq.dm.
Thickness of platinum layer 6 - 8 ^um.
Heat treatment as hereinbefore described.
Aluminising from the gas phase ■¾wm the gas-.pka&s.iomposition of powder mixture of aluminium and 95 "by weight of alumina.
Diffusion heat treatment was effected at a temperature of 1100°C for 5 hours.
The result of this treatment was an overall thickness of the protective diffusion layer of Similar results are obtainable with palladium, rhodium and/or ruthenium when used instead of platinum. 35730/2

Claims (1)

1. A method of producing protective diffusion layers that are resistant to scaling and corrosion at high temperatures on the surface of objects consisting of alloys into which aluminium is characterized in that in addition to nickel and one or metals of the group of rhodium platinum are diffused into the surface of the A method according to Claim in which successive of one or several metals the group of rhodium and and finall of aluminium are applied to the surface of the objects electrolytically or by dipping or and from the layers the metals are diffused singly or in common into the surface of the objects by a diffusion heat A method according Claim in which first a layer of nickel and on the latter a layer of one or more metals of the group platinum are deposited and aluminium then deposited from the gas phase and diffused into the surface of the object together with the nickel and the platinum metal or A method according to 1 or in which the object plated first with a nickel layer on the with a of one or more metals of the group rhodium or embedded in a powder mixture containing of metallic email with aluminium oxide the balance up to 100 and the object thus plated and embedded is sub to the diffusion For the Applicants PARTNERS insufficientOCRQuality
IL35730A 1969-12-05 1970-11-26 A method of producing protective diffusion layers on the surface of cobalt-based alloys IL35730A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19691961047 DE1961047B2 (en) 1969-12-05 1969-12-05 PROCESS FOR THE PRODUCTION OF DIFFUSION PROTECTIVE COATINGS ON OBJECTS FROM COBALT-BASED ALLOYS

Publications (2)

Publication Number Publication Date
IL35730A0 IL35730A0 (en) 1971-01-28
IL35730A true IL35730A (en) 1973-11-28

Family

ID=5753074

Family Applications (1)

Application Number Title Priority Date Filing Date
IL35730A IL35730A (en) 1969-12-05 1970-11-26 A method of producing protective diffusion layers on the surface of cobalt-based alloys

Country Status (13)

Country Link
US (1) US3692554A (en)
JP (1) JPS4931609B1 (en)
AT (1) AT296715B (en)
BE (1) BE759275A (en)
CA (1) CA924970A (en)
CH (1) CH552682A (en)
DE (1) DE1961047B2 (en)
FR (1) FR2072284A5 (en)
GB (1) GB1282530A (en)
IL (1) IL35730A (en)
NL (1) NL7017774A (en)
SE (1) SE358420B (en)
ZA (1) ZA708014B (en)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3819338A (en) * 1968-09-14 1974-06-25 Deutsche Edelstahlwerke Ag Protective diffusion layer on nickel and/or cobalt-based alloys
US3961910A (en) * 1973-05-25 1976-06-08 Chromalloy American Corporation Rhodium-containing superalloy coatings and methods of making same
US3999956A (en) * 1975-02-21 1976-12-28 Chromalloy American Corporation Platinum-rhodium-containing high temperature alloy coating
US3979273A (en) * 1975-05-27 1976-09-07 United Technologies Corporation Method of forming aluminide coatings on nickel-, cobalt-, and iron-base alloys
JPS5310704U (en) * 1976-07-09 1978-01-28
JPS5345908U (en) * 1976-09-22 1978-04-19
US4439470A (en) * 1980-11-17 1984-03-27 George Kelly Sievers Method for forming ternary alloys using precious metals and interdispersed phase
US4501776A (en) * 1982-11-01 1985-02-26 Turbine Components Corporation Methods of forming a protective diffusion layer on nickel, cobalt and iron base alloys
FR2638174B1 (en) * 1988-10-26 1991-01-18 Onera (Off Nat Aerospatiale) METHOD FOR PROTECTING THE SURFACE OF METAL WORKPIECES AGAINST CORROSION AT HIGH TEMPERATURE, AND WORKPIECE TREATED BY THIS PROCESS
US5759380A (en) * 1989-04-04 1998-06-02 General Electric Company Method of preparing oxidation resistant coatings
US5057196A (en) * 1990-12-17 1991-10-15 General Motors Corporation Method of forming platinum-silicon-enriched diffused aluminide coating on a superalloy substrate
KR940001346B1 (en) * 1991-12-30 1994-02-19 포항종합제철 주식회사 Aluminum diffusion coating layer of heat resisting stainless steel and method for forming the same
GB9204791D0 (en) * 1992-03-05 1992-04-22 Rolls Royce Plc A coated article
US5650235A (en) * 1994-02-28 1997-07-22 Sermatech International, Inc. Platinum enriched, silicon-modified corrosion resistant aluminide coating
US5427866A (en) * 1994-03-28 1995-06-27 General Electric Company Platinum, rhodium, or palladium protective coatings in thermal barrier coating systems
US5658614A (en) * 1994-10-28 1997-08-19 Howmet Research Corporation Platinum aluminide CVD coating method
CA2165641C (en) * 1994-12-24 2007-02-06 David Stafford Rickerby A method of applying a thermal barrier coating to a superalloy article and a thermal barrier coating
GB9426257D0 (en) * 1994-12-24 1995-03-01 Rolls Royce Plc Thermal barrier coating for a superalloy article and method of application
WO1996041068A1 (en) * 1995-06-07 1996-12-19 National Research Council Of Canada Anti-fretting barrier
US6066405A (en) * 1995-12-22 2000-05-23 General Electric Company Nickel-base superalloy having an optimized platinum-aluminide coating
US5897966A (en) * 1996-02-26 1999-04-27 General Electric Company High temperature alloy article with a discrete protective coating and method for making
FR2745590B1 (en) * 1996-02-29 1998-05-15 Snecma THERMAL BARRIER COATING WITH IMPROVED UNDERLAYER AND PARTS COATED WITH SUCH A THERMAL BARRIER
US6228510B1 (en) * 1998-12-22 2001-05-08 General Electric Company Coating and method for minimizing consumption of base material during high temperature service
US6207297B1 (en) 1999-09-29 2001-03-27 Siemens Westinghouse Power Corporation Barrier layer for a MCrAlY basecoat superalloy combination
SG98436A1 (en) * 1999-12-21 2003-09-19 United Technologies Corp Method of forming an active-element containing aluminide as stand alone coating and as bond coat and coated article
EP1123987A1 (en) * 2000-02-11 2001-08-16 General Electric Company Repairable diffusion aluminide coatings
US8123872B2 (en) 2006-02-22 2012-02-28 General Electric Company Carburization process for stabilizing nickel-based superalloys
US10030298B2 (en) 2015-08-21 2018-07-24 General Electric Company Method for altering metal surfaces

Also Published As

Publication number Publication date
CA924970A (en) 1973-04-24
AT296715B (en) 1972-02-25
SE358420B (en) 1973-07-30
IL35730A0 (en) 1971-01-28
NL7017774A (en) 1971-06-08
BE759275A (en) 1971-04-30
ZA708014B (en) 1971-08-25
DE1961047B2 (en) 1971-12-09
US3692554A (en) 1972-09-19
CH552682A (en) 1974-08-15
GB1282530A (en) 1972-07-19
DE1961047A1 (en) 1971-07-15
FR2072284A5 (en) 1971-09-24
JPS4931609B1 (en) 1974-08-23

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