US3839024A - Wear and corrosion resistant alloy - Google Patents

Wear and corrosion resistant alloy Download PDF

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Publication number
US3839024A
US3839024A US00332581A US33258173A US3839024A US 3839024 A US3839024 A US 3839024A US 00332581 A US00332581 A US 00332581A US 33258173 A US33258173 A US 33258173A US 3839024 A US3839024 A US 3839024A
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United States
Prior art keywords
percent
alloy
chromium
nickel
molybdenum
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US00332581A
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English (en)
Inventor
J Demo
D Ferriss
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Stoody Co
EIDP Inc
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EI Du Pont de Nemours and Co
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Filing date
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Application filed by EI Du Pont de Nemours and Co filed Critical EI Du Pont de Nemours and Co
Priority to US00332581A priority Critical patent/US3839024A/en
Priority to DE19732348702 priority patent/DE2348702C3/de
Priority to DE19732348703 priority patent/DE2348703A1/de
Priority to HUDU000213 priority patent/HU169042B/hu
Priority to HUDU212A priority patent/HU166691B/hu
Priority to AR25053673A priority patent/AR201840A1/es
Priority to SE7314167A priority patent/SE390643B/xx
Priority to JP11640573A priority patent/JPS5641688B2/ja
Priority to IN2323/CAL/73A priority patent/IN140338B/en
Priority to DD174147*A priority patent/DD107076A5/xx
Priority to DK566373AA priority patent/DK141173B/da
Priority to JP48116404A priority patent/JPS5238807B2/ja
Priority to NO404473A priority patent/NO134705B/no
Priority to FR7337191A priority patent/FR2204250A5/fr
Priority to AU61546/73A priority patent/AU483816B2/en
Priority to GB4859573A priority patent/GB1439049A/en
Priority to CA183,671A priority patent/CA1001864A/en
Priority to CH1474273A priority patent/CH580764A5/xx
Priority to DD17415073A priority patent/DD107075A5/xx
Priority to BR8134/73A priority patent/BR7308134D0/pt
Priority to IT30377/73A priority patent/IT998816B/it
Priority to NL7314446A priority patent/NL7314446A/xx
Priority to AT889273A priority patent/AT333519B/de
Priority to ZA00738120A priority patent/ZA738120B/xx
Priority to AT889473A priority patent/AT333520B/de
Priority to LU68651A priority patent/LU68651A1/xx
Priority to IL43461A priority patent/IL43461A0/xx
Application granted granted Critical
Publication of US3839024A publication Critical patent/US3839024A/en
Priority to AR25608074A priority patent/AR202667A1/es
Priority to NO760902A priority patent/NO760902L/no
Priority to JP4160977A priority patent/JPS52125412A/ja
Assigned to STOODY COMPANY, A CORP. OF DE reassignment STOODY COMPANY, A CORP. OF DE ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: CABOT CORPORATION, A CORP. OF DE
Assigned to WELLS FARGO BANK, N.A. reassignment WELLS FARGO BANK, N.A. SECURITY INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: STOODY DELORO STELLITE, INC.
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C19/00—Alloys based on nickel or cobalt
    • C22C19/03—Alloys based on nickel or cobalt based on nickel
    • C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/055—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 20% but less than 30%
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
    • B23K35/24—Selection of soldering or welding materials proper
    • B23K35/30—Selection of soldering or welding materials proper with the principal constituent melting at less than 1550 degrees C
    • B23K35/3033—Ni as the principal constituent
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
    • B23K35/24—Selection of soldering or welding materials proper
    • B23K35/30—Selection of soldering or welding materials proper with the principal constituent melting at less than 1550 degrees C
    • B23K35/3046—Co as the principal constituent
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C19/00—Alloys based on nickel or cobalt
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C19/00—Alloys based on nickel or cobalt
    • C22C19/07—Alloys based on nickel or cobalt based on cobalt
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C28/00—Alloys based on a metal not provided for in groups C22C5/00 - C22C27/00
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C29/00—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C29/00—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
    • C22C29/18—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on silicides
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C32/00—Non-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
    • C22C32/0047—Non-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 carbides, nitrides, borides or silicides as the main non-metallic constituents
    • C22C32/0078—Non-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 carbides, nitrides, borides or silicides as the main non-metallic constituents only silicides
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02—Parts of sliding-contact bearings
    • F16C33/04—Brasses; Bushes; Linings
    • F16C33/06—Sliding surface mainly made of metal
    • F16C33/12—Structural composition; Use of special materials or surface treatments, e.g. for rust-proofing
    • F16C33/121—Use of special materials
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16J—PISTONS; CYLINDERS; SEALINGS
    • F16J15/00—Sealings
    • F16J15/16—Sealings between relatively-moving surfaces
    • F16J15/34—Sealings between relatively-moving surfaces with slip-ring pressed against a more or less radial face on one member
    • F16J15/3496—Sealings between relatively-moving surfaces with slip-ring pressed against a more or less radial face on one member use of special materials
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16J—PISTONS; CYLINDERS; SEALINGS
    • F16J9/00—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction
    • F16J9/26—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction characterised by the use of particular materials

Definitions

  • the alloy microstructure consists of 10-100 volume percent of a hard phase which is predominantly Laves phase and 0-90 volume percent of a relatively soft matrix phase, and 2. the alloy microstructure consists of at least 10 volume percent of a Laves phase.
  • Laves phases are known to be wear resistant. Alloys having hard Laves phases dispersed in softer matrices are known to have low friction properties. Such alloys which are both wear and corrosion resistant are not readily available.
  • U.S. Pat. No. 3,410,732 discloses that certain cobaltbased alloys containing chromium exhibit improved corrosion resistance in certain acidic media; however,
  • the alloy of this invention consists essentially of, by weight:
  • the alloy microstructure consists of 10-100 volume percent of a hard phase which is predominantly Laves phase and -90 volume percent of a relatively soft matrix phase, and
  • the alloy microstructure consists of at least volume percent of a Laves phase.
  • a preferred embodiment of this invention includes the aforesaid alloy wherein the hard phase is at least 10 volume percent (preferably -75 volume percent), the molybdenum content is 22-36 percent, the silicon content is at least 1.5 percent (usually not above 5 percent and, preferably, 2-3 percent) and, alternatively, the cobalt content is 45-59 percent and the chromium content is 17-25 percent or the nickel content is 48-63 percent and the chromium content is 8-22 percent.
  • Other preferred embodiments include the above and consist essentially of 50-55 percent cobalt, 22-29 percent molybdenum, 17-22 percent chromium and 1.5-4 percent silicon; 48-63 percent nickel, 24-36 percent molybdenum, 8-16 percent chromium and 2-5 percent silicon; 53 percent cobalt, 28 percent molybdenum, 17 percent chromium and 2 percent silicon; 51 percent cobalt, 25 percent molybdenum, 22 percent chromium and 2 percent silicon; 62 percent nickel, 28 percent molybdenum, 8 percent chromium and 2 percent silicon; 50 percent nickel, 32 percent molybdenum, 15 percent chromium and 3 percent silicon; and 53 percent nickel, 35 percent molybdenum, 9 percent chr0- mium and 3 percent silicon.
  • Still other preferred embodiments include the alloy in rod or powder form; articles obtained by bonding alloy particles to each other at elevated pressures and temperatures, followed by cooling; coated articles obtained by applying the fused alloy to a metal substrate, followed by cooling of the alloy; and coated articles obtained by applying partly fused particles of the alloy to a substrate at elevated temperature, followed by cooling of the alloy.
  • the alloy of this invention is based on the discovery of an alloy composition having the high wear resistance of known wear resistant alloys, which have low corrosion resistance, and having the high corrosion resistance of known corrosion resistant alloys, which have low wear resistance. It also has been discovered that the nickel-based alloy of this invention is resistant to stress corrosion cracking.
  • the defined alloy can be produced by melting a mixture of the elemental components or subcombinations of the elements at a temperature sufficient (for example, l,250-1,850C.) to provide a molten composition, and thereafter solidifying the melt by cooling.
  • the resulting product is an alloy of nickel or cobalt, molybdenum, chromium and silicon in the proportions specified above and consists essentially of a cobaltor nickelbased matrix which is strengthened by the formation of intermetallic compounds and by the alloying of the matrix.
  • the alloy is characterized by having two major phases which are detectable by metallographic, chemical and X-ray diffraction techniques. Specifically, the alloy contains at least 10 volume percent of a hard phase which provides at least 10 volume percent of a Laves phase and up to volume percent of a relatively soft matrix phase.
  • the matrix phase in the alloy is formed from the same alloy components as the hard phase.
  • the matrix can be substantially the base metal, a solid solution, an intermetallic compound other than Laves phase or a mixture of solid solution and intermetallic compound. Silicides of the alloy metal components also can be present in the matrix.
  • Laves phase contains one or more metallographical constituents that have the C, (hexagonal), C (cubic) or C (I-Iexagonal) crystal structure as described in International Tables for X-Ray Crystallography," Symmetry Groups, N. F. M. Henry and K. Lonsdale, International Union of Crystallography, Kynoch Press, Birmingham, England (1952).
  • Prototypes of the Laves phase crystal structures are, respectively, MgZn MgCuand MgNi
  • Such phase structures are unique crystal structures that permit the most complete occupation of space by assemblages of two sizes of spheres.
  • the Laves phase can be represented by the formula AB- the large atom A occupying certain sets of crystallographic sites and the small atoms B occupying other sites, in which the ratio of atomic radii AB is in the range 1.05-1.68.
  • Laves phases occur as intermediate phases in numerous alloy systems. Laves phases generally have a homogeneity range, that is, they can have any of a range of elemental compositions while maintaining their characteristic crystal structure.
  • the atom ratio B:A can vary from slightly lsss to slightly more than 2, possibly the result of some vacant sites in the crystal structure. Also, more than one kind of atom can occupy the large atom sites, the small atom sites, or both.
  • Such Laves phases can be represented stoichiometrically by the formula (A ,C,)(B u) where C represents the atoms of one or more kinds that substitute for the large atoms, D represents the atoms of one or more kinds that substitute for the small atoms, of the binary Laves formula AB And x and y have values in the range -1.
  • An alloy is a substance having metallic properties and containing in its elemental composition two or more chemical elements of which at least two are metals.
  • the alloy of this invention has at least three metallic elements.
  • Other elements (which are non-essential) can be present in the alloy of the invention provided they do not have a substantially adverse effect on the wear and corrosion resistance of the alloys.
  • typical non-essential elements Manganese is sometimes present up to about 0.6 percent and iron is tolerable up to about 2 percent.
  • cobalt-based alloys typically contain about 0.5 percent nickel, and nickelbased alloys typically contain about 0.5 percent cobalt. Up to about 3 percent of all such non-essential elements can be present in the alloy of this invention. It is to be understood that the previously-disclosed weight percentages of the essential elements are based only on the weights of the four essential elements in the alloy.
  • the hard phase is almost exclusively Laves phase at about an 8 percent chromium content. At 12-25 percent chromium contents an additional phase may appear. This additional phase may surround Laves phase particles and may constitute a significant, though minor, part of the hard phase. This additional hard phase component is normally harder than the dispersing matrix phase and may constitute up to volume per cent of the alloy.
  • the Laves phase constitutes at least 50 volume percent and, usually, greater than 75 volume percent of the hard phase. The alloy in all cases has at least 10 volume percent Laves phase.
  • Table I contains metallographic data on representative compositions of the alloy of this invention.
  • the table shows the volume per cent of phases present, the bulk Rockwell C hardness and the microhardness values of the hard and matrix phases.
  • Articles can be formed from the alloy of this invention by melting and casting the alloy using conventional furnaces, molds and techniques.
  • the alloy can be pre formed or, as already disclosed, it can be formed from unalloyed mixtures of the necessary components. In the latter case, conventional prior art alloy conditions and techniques are chosen so as to form the alloy in situ.
  • the preformed alloy can be physically reduced to particle sizes adapted to make articles by powder metallurgy procedures. In such procedures, powder particles of the preformed alloy are positioned in a mold and subsequently compressed at elevated pressures and temperatures to partly fuse them until a complete body of the alloy is produced (a powder metallurgy part) and thereafter cooled. Such parts are wear and corrosion resistant.
  • Coatings of the alloy on various substrates can be made by known procedures, for example, as disclosed in US. Pat. No. 3,331,700; by overlaying metal substrates with melts of the alloy provided in rodform; or by plasma spraying coatings of partly fused particles of the alloy on metal substrates and thereafter cooling the coatings.
  • the aforesaid rod can consist of solid preformed alloy which is a continuous structure or it can consist of a combination of a continuous metal sheath which is filled with the necessary components so that the alloy is formed in situ during fusion. It is to be understood that the coatings may need dimensional finishing to prepare them for use. Such coatings are wear and corrosion resistant.
  • the alloy of this invention is especially useful for providing one or, preferably, both of two surfaces which are in sliding contact with each other and exposed to corrosive liquids.
  • Typical sliding surface applications include rotating and axially movable shafts sliding inside cylindrical bushings and against end restraining surfaces such as thrust bearings.
  • Bearings and seals provided with surfaces of the alloy of this invention resist corrosion by oxidizing liquids, such as ferric chloride and nitric acid solutions, and reducing liquids, such as aqueous hydrochloric, formic and sulfuric acids.
  • oxidizing liquids such as ferric chloride and nitric acid solutions
  • reducing liquids such as aqueous hydrochloric, formic and sulfuric acids.
  • the alloy may resist a few corrodants less than some known alloys, it exhibits superiority in its overall resistance to both wear and corrosion.
  • acidic media including dilute and concentrated mineral and organic acids and solutions of acidic salts, such as aqueous hydrochloric acid, nitric acid, sulfuric acid, phosphoric acid, formic acid, acetic acid and ferric chlo- Metallographic Data on Representative Compositions of the Alloy of this Invention Rc Rockwell C Hardness VHN Vickers Hardness No. greater than ride.
  • acidic media are especially corrosive at elevated temperatures, for example, 50100C.
  • alloys tested had compositions as given below, including phase volumes.
  • the number preceding each element of an alloy composition is percent by weight.
  • Hard phase volumes are expressed as alloy percent and are determined by relative areas under intensity graphs generated by X-ray diffraction analyses of characteristic alloy phases, as is well known in the metallurgical art.
  • Alloys A through H were prepared by mixing the elements in the specified weight proportions, heating each mixture in air until completely molten, pouring off scum which formed on the surface and allowing the melt to cool to room temperature.
  • Alloys C through H are alloys of the invention; alloys A, B and I through Q are commercially available prior art alloys.
  • G 50 Ni/32 Mo/3 Si/l5 Cr, having 50 percent hard hase.
  • the hard phase in each alloy above contains at least 75 percent Laves phase.
  • Hastelloy C another nickel superalloy of composition 54 Ni/16 Mo/16 Cr/l Si/5 Fe/4 W, having no LP and known as corrosion resistant.
  • Hastelloy B another nickel superalloy of composition 6 Fe/28 Mo/l Si/balance Ni, having no LP and known as corrosion resistant.
  • O Stellite 68 a well known alloy of composition 29 Cr/1.5 (max.) Mo/2 Si/3 Fc/4.5 W/0.9-l .4 C/balance Co, having no LP and known as wear rcsistant.
  • Table I1 shows the weight losses of the riders and drums and the surface ratings of the worn riders and Fe, having no LP and known as corrosion resistant. drums of alloys which were rubbed together.
  • M Monel 400 a nickel-based alloy of composition 1.4 Fe/32 Cu/balance Ni, having no LP and generally known as corrosion resistant.
  • Hastelloy N A nickel-based superalloy, Hastelloy N, of com- It can be seen that the alloys of the invention (Exs. 3-7) in sliding contact against themselves are superior to Stellite 68 against itself (Ex. 8) chromium plated steel (Ex. 9), stainless steel 316 (Ex. 11) and l-lastelloy C (Ex. 10) with the coba1t-based alloys (Exs. 3-4) being somewhat superior to the nickel-based alloys (Exs. 5-7) under these conditions.
  • Examples 12-28 The superiority of the alloy of the invention over similarly constituted alloys of the prior art (Examples 1 and 2) under a wider variety of corrosive conditions is indicated by the results of the following examples.
  • the following test was used to compare the corrosion resistance of the alloy of the invention and known corrosion nd wear resistance alloys in contact with a variety of corrosive liquids. It consisted of a. immersing a weighed Vs inch X 1 inch X 1 /2 inch coupon of metal wet belt ground to an 80 grit finish in a liter of a testing liquid for 24 hour intervals at the indicated temperature,
  • Table 111 shows the corrosion performance as mils/year of metal thickness loss in the alloys tested in the aqueous liquids at the exposure temperatures shown in column headings.
  • the cobalt-based alloys of the invention (Exs. 14-15) have corrosion resistance superior to stainless steels (Exs. 20-21) and Stellite B (Ex. 28) and generally equivalent to Monel (Ex. 24), the Hastelloys (Exs. 25-27) and Carpenter 20Cb3 (Ex. 22).
  • the nickelbased alloys of the invention (Exs. 16-18) can be seen to perform in similar comparative relation to the known alloys cited. It can further be seen that alloys of the invention (Exs. 14, 15, l7, l8 and 19) show corrosion resistance against the oxidizing ferric chloride and- /or nitric acid media superior to Monel 400 (Ex. 24), Hastelloy N (Ex.
  • nickel-based alloys with 8 percent Cr (Ex. 30) and with percent Cr (Ex. 31 are superior to the prior art cobalt-based alloy with 8 percent Cr (Ex. 29).
  • the attainment of 100 hours without failure indicates that attainability of at least 1,000 hours without failure is possible under these conditions.
  • Alloy consisting essentially of, by weight: a. at least 45 percent cobalt or nickel; b. -42 percent molybdenum; c. 17-25 percent chromium if (a) is cobalt and 8-22 percent chromium if (a) is nickel; and d. sufficient silicon, within the range 15-12 percent,
  • the alloy microstructure consists of 20-100 volume percent of a hard phase which is at least 75 volume percent Laves phase and 0-80 volume percent of a relatively soft matrix phase, said alloy containing no more than 3 percent nonessential elements.
  • the alloy of claim 1 wherein the hard phase is 20-75 volume percent and which consists essentially of 20-75 volume percent and which consists essentially of 48-63 percent nickel, 22-36 percent molybdenum, 8-22 percent chromium and 15-5 percent silicon.
  • the alloy of claim 6 which consists essentially of 48-63 percent nickel, 24-36 percent molybdenum, 8-16 percent chromium and 2-5 percent silicon.
  • the alloy of claim 7 which consists essentially of 62 percent nickel, 28 percent molybdenum, 8 percent chromium and 2 percent silicon.
  • the alloy of claim 7 which consist essentially of 50 percent nickel, 32 percent molybdenum, 15 percent chromium and 3 percent silicon.
  • the alloy of claim 7 which consists essentially of 53 percent nickel, 35 percent molybdenum, 9 percent chromium and 3 percent silicon.
  • the alloy of claim 1 in the form of a powder.
  • the alloy of claim 1 in the form of a rod.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Powder Metallurgy (AREA)
US00332581A 1972-10-19 1973-02-15 Wear and corrosion resistant alloy Expired - Lifetime US3839024A (en)

Priority Applications (30)

Application Number Priority Date Filing Date Title
US00332581A US3839024A (en) 1973-02-15 1973-02-15 Wear and corrosion resistant alloy
DE19732348702 DE2348702C3 (de) 1972-10-19 1973-09-27 Verwendung einer Kobalt- oder Nickellegierung als Werkstoff für Gleitpaare
DE19732348703 DE2348703A1 (de) 1973-02-15 1973-09-27 Abriebfeste und korrosionsfeste legierung
HUDU000213 HU169042B (hu) 1972-10-19 1973-10-09
HUDU212A HU166691B (hu) 1973-02-15 1973-10-09
AR25053673A AR201840A1 (es) 1972-10-19 1973-10-16 Nueva aleacion mejorada resistente al desgaste y la corrosion y articulos producidos con dicha aleacion y recubiertos con la misma
CH1474273A CH580764A5 (hu) 1972-10-19 1973-10-18
IN2323/CAL/73A IN140338B (hu) 1972-10-19 1973-10-18
DD174147*A DD107076A5 (hu) 1973-02-15 1973-10-18
DK566373AA DK141173B (da) 1973-02-15 1973-10-18 Slid- og korrosionsbestandig cobalt- eller nikkellegering.
JP48116404A JPS5238807B2 (hu) 1973-02-15 1973-10-18
NO404473A NO134705B (hu) 1972-10-19 1973-10-18
FR7337191A FR2204250A5 (en) 1972-10-19 1973-10-18 Abrasion-resistant alloy surfaces - comprise transition metals and are self-lubricating or used with lubricants
AU61546/73A AU483816B2 (en) 1973-10-18 Improved wear and corrosion resistant alloys and wear resistant frictionally contacting surfaces
GB4859573A GB1439049A (en) 1973-02-15 1973-10-18 Wear-and corrosion-resistant alloy
CA183,671A CA1001864A (en) 1973-02-15 1973-10-18 Wear and corrosion resistant alloy
SE7314167A SE390643B (sv) 1973-02-15 1973-10-18 Legering innehallande laves-fas
DD17415073A DD107075A5 (hu) 1972-10-19 1973-10-18
BR8134/73A BR7308134D0 (pt) 1973-02-15 1973-10-18 Liga aperfeicoada resistente a desgaste e corrosao
JP11640573A JPS5641688B2 (hu) 1972-10-19 1973-10-18
IT30377/73A IT998816B (it) 1973-02-15 1973-10-19 Lega resistente all usura ed alla corrosione
AT889273A AT333519B (de) 1972-10-19 1973-10-19 Gleitpaar
ZA00738120A ZA738120B (en) 1973-02-15 1973-10-19 Wear and corrosion resistant alloy
AT889473A AT333520B (de) 1973-02-15 1973-10-19 Abriebfeste und korrosionsfeste legierung
LU68651A LU68651A1 (hu) 1972-10-19 1973-10-19
NL7314446A NL7314446A (hu) 1973-02-15 1973-10-19
IL43461A IL43461A0 (en) 1973-02-15 1973-10-22 Wear and corrosion resistant alloy
AR25608074A AR202667A1 (es) 1972-10-19 1974-10-14 Dispositivos mecanicos metalicos que comprenden dos superficies opuestas mantenidas en contacto de friccion entre si
NO760902A NO760902L (hu) 1972-10-19 1976-03-15
JP4160977A JPS52125412A (en) 1973-02-15 1977-04-13 Wear and corrosion resistant alloy

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JP (2) JPS5238807B2 (hu)
AT (1) AT333520B (hu)
BR (1) BR7308134D0 (hu)
CA (1) CA1001864A (hu)
DD (1) DD107076A5 (hu)
DE (1) DE2348703A1 (hu)
DK (1) DK141173B (hu)
GB (1) GB1439049A (hu)
HU (1) HU166691B (hu)
IL (1) IL43461A0 (hu)
IT (1) IT998816B (hu)
NL (1) NL7314446A (hu)
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Cited By (14)

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US5312697A (en) * 1992-04-24 1994-05-17 Inco Alloys International, Inc. Alloy overlay having thermal characteristics similar to those of a substrate
EP0882806A1 (en) * 1997-05-21 1998-12-09 Kabushiki Kaisha Toyota Chuo Kenkyusho Hard molybdenum alloy, wear resistant alloy and method for manufacturing the same
EP1074698A2 (en) * 1999-08-03 2001-02-07 General Electric Company A lubricating coating for tubes in gas turbines
WO2004009860A1 (en) * 2002-07-17 2004-01-29 Deloro Stellite Company, Inc. Wear-resistant, corrosion-resistant cobalt-based alloys
US20050142026A1 (en) * 2003-12-29 2005-06-30 Wu James B.C. Ductile cobalt-based Laves phase alloys
US20060134455A1 (en) * 2004-12-15 2006-06-22 Deloro Stellite Holdings Corporation Imparting high-temperature degradation resistance to components for internal combustion engine systems
US20070169585A1 (en) * 2003-11-21 2007-07-26 Hitachi Powdered Metals Co., Ltd. Alloy powder for forming hard phase and ferriferous mixed powder using the same, and manufacturing method for wear resistant sintered alloy and wear resistant sintered alloy
US7520947B2 (en) 2003-05-23 2009-04-21 Ati Properties, Inc. Cobalt alloys, methods of making cobalt alloys, and implants and articles of manufacture made therefrom
EP2130933A1 (en) * 2007-03-29 2009-12-09 Mitsubishi Heavy Industries, Ltd. Coating material, method for production thereof, coating method, rotor blade equipped with shroud
US20100008812A1 (en) * 2008-07-03 2010-01-14 Hitachi Powdered Metals Co., Ltd. Hard phase forming alloy powder, wear resistant sintered alloy, and production method for wear resistant sintered alloy
CN101463439B (zh) * 2007-12-18 2010-09-01 中国科学院兰州化学物理研究所 镍铝金属间化合物基高温自润滑复合材料的制备方法
CN104328351A (zh) * 2014-10-23 2015-02-04 苏州莱特复合材料有限公司 一种用于轴承的粉末冶金材料及其制备方法
US10760686B2 (en) * 2017-10-11 2020-09-01 Raytheon Technologies Corporation Wear resistant piston seal
US11155904B2 (en) 2019-07-11 2021-10-26 L.E. Jones Company Cobalt-rich wear resistant alloy and method of making and use thereof

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CN105562959B (zh) * 2016-03-02 2017-10-24 长春三友汽车部件制造有限公司 一种提高高强度钢激光焊接接头力学性能的方法

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US3331700A (en) * 1963-04-01 1967-07-18 Du Pont Method of coating metals
US3410732A (en) * 1965-04-30 1968-11-12 Du Pont Cobalt-base alloys
US3482967A (en) * 1965-10-22 1969-12-09 Gen Electric Brazing alloy
US3592632A (en) * 1966-07-14 1971-07-13 Int Nickel Co High temperature nickel-chromium-iron alloys particularly suitable for steam power applications
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Cited By (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5312697A (en) * 1992-04-24 1994-05-17 Inco Alloys International, Inc. Alloy overlay having thermal characteristics similar to those of a substrate
EP0882806A1 (en) * 1997-05-21 1998-12-09 Kabushiki Kaisha Toyota Chuo Kenkyusho Hard molybdenum alloy, wear resistant alloy and method for manufacturing the same
US6066191A (en) * 1997-05-21 2000-05-23 Kabushiki Kaisha Toyota Chuo Kenkyusho Hard molybdenum alloy, wear resistant alloy and method for manufacturing the same
EP1074698A2 (en) * 1999-08-03 2001-02-07 General Electric Company A lubricating coating for tubes in gas turbines
EP1074698A3 (en) * 1999-08-03 2001-11-14 General Electric Company A lubricating coating for tubes in gas turbines
WO2004009860A1 (en) * 2002-07-17 2004-01-29 Deloro Stellite Company, Inc. Wear-resistant, corrosion-resistant cobalt-based alloys
US20040057863A1 (en) * 2002-07-17 2004-03-25 Wu James B. C. Wear-Resistant, Corrosion-Resistant Cobalt-Based Alloys
US6852176B2 (en) 2002-07-17 2005-02-08 Deloro Stellite Holdings Corporation Wear-resistant, corrosion-resistant cobalt-based alloys
US7520947B2 (en) 2003-05-23 2009-04-21 Ati Properties, Inc. Cobalt alloys, methods of making cobalt alloys, and implants and articles of manufacture made therefrom
US7601196B2 (en) 2003-11-21 2009-10-13 Hitachi Powdered Metals Co., Ltd. Alloy powder for forming hard phase and ferriferous mixed powder using the same, and manufacturing method for wear resistant sintered alloy and wear resistant sintered alloy
US20070169585A1 (en) * 2003-11-21 2007-07-26 Hitachi Powdered Metals Co., Ltd. Alloy powder for forming hard phase and ferriferous mixed powder using the same, and manufacturing method for wear resistant sintered alloy and wear resistant sintered alloy
US7294167B2 (en) * 2003-11-21 2007-11-13 Hitachi Powdered Metals Co., Ltd. Alloy powder for forming hard phase and ferriferous mixed powder using the same, and manufacturing method for wear resistant sintered alloy and wear resistant sintered alloy
US20050142026A1 (en) * 2003-12-29 2005-06-30 Wu James B.C. Ductile cobalt-based Laves phase alloys
US7572408B2 (en) * 2003-12-29 2009-08-11 Deloro Stellite Holdings Corporation Ductile cobalt-based Laves phase alloys
US8668959B2 (en) 2004-12-15 2014-03-11 Kennametal Inc. Imparting high-temperature degradation resistance to metallic components
US8383203B2 (en) 2004-12-15 2013-02-26 Kennametal Inc. Imparting high-temperature degradation resistance to components for internal combustion engine systems
US20060134455A1 (en) * 2004-12-15 2006-06-22 Deloro Stellite Holdings Corporation Imparting high-temperature degradation resistance to components for internal combustion engine systems
EP2130933A1 (en) * 2007-03-29 2009-12-09 Mitsubishi Heavy Industries, Ltd. Coating material, method for production thereof, coating method, rotor blade equipped with shroud
US20100104440A1 (en) * 2007-03-29 2010-04-29 Mitsubishi Heavy Industries, Ltd. Coating material and method of manufacturing same, coating method, and moving blade with shroud
EP2130933A4 (en) * 2007-03-29 2010-10-06 Mitsubishi Heavy Ind Ltd COATING MATERIAL, MANUFACTURING METHOD THEREOF, COATING METHOD, ROTOR BLADE EQUIPPED WITH PROTECTIVE COATING
CN101463439B (zh) * 2007-12-18 2010-09-01 中国科学院兰州化学物理研究所 镍铝金属间化合物基高温自润滑复合材料的制备方法
US20100008812A1 (en) * 2008-07-03 2010-01-14 Hitachi Powdered Metals Co., Ltd. Hard phase forming alloy powder, wear resistant sintered alloy, and production method for wear resistant sintered alloy
US9260772B2 (en) 2008-07-03 2016-02-16 Hitachi Powdered Metals Co., Ltd. Hard phase forming alloy powder, wear resistant sintered alloy, and production method for wear resistant sintered alloy
CN104328351A (zh) * 2014-10-23 2015-02-04 苏州莱特复合材料有限公司 一种用于轴承的粉末冶金材料及其制备方法
CN104328351B (zh) * 2014-10-23 2016-05-18 宁夏鸿裕机械科技有限公司 一种用于轴承的粉末冶金材料及其制备方法
US10760686B2 (en) * 2017-10-11 2020-09-01 Raytheon Technologies Corporation Wear resistant piston seal
US11155904B2 (en) 2019-07-11 2021-10-26 L.E. Jones Company Cobalt-rich wear resistant alloy and method of making and use thereof

Also Published As

Publication number Publication date
NL7314446A (hu) 1974-08-19
IL43461A0 (en) 1974-01-14
ATA889473A (de) 1976-03-15
AT333520B (de) 1976-11-25
HU166691B (hu) 1975-05-28
DD107076A5 (hu) 1974-07-12
JPS52125412A (en) 1977-10-21
JPS501026A (hu) 1975-01-08
JPS5238807B2 (hu) 1977-10-01
IT998816B (it) 1976-02-20
BR7308134D0 (pt) 1974-09-24
CA1001864A (en) 1976-12-21
ZA738120B (en) 1975-05-28
DK141173C (hu) 1980-06-30
JPS5728734B2 (hu) 1982-06-18
SE390643B (sv) 1977-01-03
GB1439049A (en) 1976-06-09
DK141173B (da) 1980-01-28
DE2348703A1 (de) 1974-08-22

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