US3445624A - Cobalt alloy and welding electrode based upon this alloy - Google Patents

Cobalt alloy and welding electrode based upon this alloy Download PDF

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Publication number
US3445624A
US3445624A US537716A US3445624DA US3445624A US 3445624 A US3445624 A US 3445624A US 537716 A US537716 A US 537716A US 3445624D A US3445624D A US 3445624DA US 3445624 A US3445624 A US 3445624A
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United States
Prior art keywords
alloy
tungsten
chromium
weight
carbon
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US537716A
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English (en)
Inventor
Jean Albert Francois Sunnen
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.)
La Soudure Electrique Autogene SA
Hoskins Manufacturing Co
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La Soudure Electrique Autogene SA
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Assigned to HOSKINS MANUFACTURING COMPANY reassignment HOSKINS MANUFACTURING COMPANY MERGER (SEE DOCUMENT FOR DETAILS). EFFECTIVE JULY 12,1982 A CORP OF MI Assignors: ARCOS CORPORATION
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/22Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
    • B23K35/24Selection of soldering or welding materials proper
    • B23K35/30Selection of soldering or welding materials proper with the principal constituent melting at less than 1550 degrees C
    • B23K35/3046Co as the principal constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/07Alloys based on nickel or cobalt based on cobalt
    • 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
    • Y10T428/12014All metal or with adjacent metals having metal particles
    • Y10T428/12028Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, etc.]
    • Y10T428/12049Nonmetal 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
    • Y10T428/12014All metal or with adjacent metals having metal particles
    • Y10T428/12028Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, etc.]
    • Y10T428/12063Nonparticulate metal component
    • Y10T428/12097Nonparticulate component encloses particles
    • 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

Definitions

  • the cobalt alloy contains at least 93% by weight of cobalt, 0.5 to 6% by weight of iron, at least one of the metals of the group consisting of manganese, titanium and aluminum and also incidental impurities the amount of which is insufficient to have an effect upon the properties of the alloy, any manganese, titanium and aluminum content being in the ranges from traces to 4.5% by weight for manganese, 0.1 to 2% by weight for titanium and 0.1 to 2% by weight for aluminum, and the sum of the iron content of said alloy, of of its manganese content, of 7 of its titanium content, and of of its aluminum content being below of its total weight.
  • the electrode may include other ingredients in specified ranges such as chromium, tungsten and carbon.
  • the present invention relates to an alloy comprising at least 93% of cobalt and iron, optionally at least one of the metal of the manganese, titanium and aluminum group, and also optionally impurities consisting of nickel, carbon, silicon, sulphur and phosphorus.
  • the present invention relates to a cobalt alloy which 3,445,624 Patented May 20, 1969 is not attended by these disadvantages and which, although consisting of hexagonal crystals or a mixture of hexagonal crystals and face-centered cubic crystals, nevertheless has sufiicient malleability to undergo cold shaping and more particularly to undergo drawing to a diameter of less than two millimeters and rolling into a strip less than 0.3 millimeter thick.
  • the alloy according to the invention is characterised in that its proportions of iron, manganese, titanium and aluminum are such that the sum of its iron content, of of its optional manganese content, of ,1 of its optional titanium content and of 9 of its optional aluminum content is lower than 6% of its total weight, and in that the maximum optional manganese, titanium and aluminum contents are equal to 4.5 2% and 2% respectively.
  • the malleability is ensured in principle in the absence of nickel, which exists only to the extent that it constitutes impurities of the constituents of the alloy and is introduced into the latter essentially as an impurity of the cobalt.
  • the nickel content cannot reach 1%.
  • the malleability of the cobalt alloy may be ensured solely by means of iron provided that its iron content is lower than 6%, in order that the hot hardness may not be greatly reduced when this alloy serves for the deposition of a hard alloy in combination with chromium and tungsten.
  • the iron content is preferably maintained between 3% and 4%.
  • the manganese content is maintained below 4.5% in order to reduce the cracking tendency of the deposit.
  • Titanium and aluminum are advantageous in a proportion not exceeding 2% each, because when the ductile alloy of which they form part is used as a continuous element of a composite welding electrode containing in its coating or in its core hardening elements such as chromium, tungsten and carbon, they create in the welding bath a highly reducing medium which favours the passage of hardening elements into this bath.
  • silicon which is also a reducing agent, must be used in a small proportion because it favours the hexagonal structure. It is advantageous for the cobalt alloy to contain not more than 0.5% thereof.
  • alloys are produced by powder metallurgy, melting in vacuo, under an atmosphere for protection against oxygen and nitrogen, under slag or by any other known means.
  • Alloys of this type may be hot rolled without difiiculty or hot extruded to billets of a diameter of mm. These billets are thereafter drawn in to passes to a diameter of 4 or 3.25 mm. and even less than 2 mm. In drawing from 10 mm. to 4 mm., two intermediate annealing operations are necessary at about 7 mm. and 5 mm.
  • these alloys After annealing at a minimum temperature of 900 C. for one hour, these alloys have a hardness of 45 to 60 kg./mm. and an elongation of 45% to 20%. These alloys are particularly useful for the manufacture of coated electrodes, cored electrodes or bare wires employed under flux or under slag for obtaining hard surfacings of the stellite type comprising, in addition to a high cobalt content, a relatively high chromium, tungsten and carbon content.
  • a wire consisting of the alloy according to the invention may constitute the core of a coated electrode, of which the coating contains the main alloying elements of stellite, such as chromium, tungsten and carbon in the form of powder, alloys or carbides. Part of the alloying elements may be present in the form of chromium oxide and/or tungsten oxide provided that there is introduced into the wire or into the coating a suflicient quantity of reducting metals such as aluminum, manganese or silicon.
  • a wire conforming to the composition of alloy 1 in the table having a diameter of 4 mm. and weighing 50 g., coated with 50 g. of a paste containing 24 g. of metallic chromium, 4 g.
  • the proportions of these three constituents in relation to the total weight of the wire, the metallic chromium, the metallic tungsten and the carbon may vary between the following limits: from 25% to in the case of chromium, from 3% to 15% in the case of tungsten and from 0.5% to 8% in the case of carbon.
  • powdered cobalt may be made to the coating of the electrode in order to bring its output to 200% or 250%.
  • the cobalt alloy in strip form may be used to form a tubular or composite electrode, the strip constituting the sheath, and the chromium, the tungsten and the carbon, as also the other alloying elements and slag, where necessary, being introduced by the powder to the center of the composite electrode.
  • a folded strip conforming to the composition of alloy 5 in the table which has a width of 30 mm. before folding and a thickness of 0.30 mm.
  • this strip of 60 g. of a mixture of powders consisting of 78% of chromium, 19% of tungsten and 3% of carbon, a composite wire 4 mm. in diameter which gave rise to the following deposit: cobalt 61%, chromium 28%, tungsten 6.5%, carbon 1% and iron 3%, the remaining 0.5% consisting of manganese, silicon and traces of nickel.
  • the weight of metallic chromium in the powder mixture is that of the tungsten is and that of the carbon is file- X 3
  • the aforesaid proportion may vary between 25% and 35% in the case of chromium, between 3% and 15% in the case of tungsten and between 0.5 and 8% in the case of carbon.
  • the proportions of chromium, cobalt and carbon in the coating around the continuous metallic portion consisting of the wire or in the powder core maintained by the continuous metallic portion consisting of the strip may be so increased as to bring the output of the electrode to 200% or even to 250%.
  • the tungsten is preferably supplied in the form of a powdered alloy of chromium, tungsten and carbon having a melting point below 2500 C., because it is known that tungsten has a melting point of 3380 C., and tungsten carbide, W C a melting point of 2750 C. These temperatures are generally too high and it is likely that the alloy will not be completely melted during the flame surfacing. Therefore, there are preferably employed in this case an alloy of tungsten, chromium and carbon with or without an addition of boron, having the lowest possible melting point, that is to say, one below 2500" C.
  • a chromium-tungsten-carbon alloy of relatively low melting point is, for example, that comprising 55% of chromium, 38% of tungsten and 3% of carbon, the remainder consisting of aluminum, silicon and iron.
  • the melting point of this alloy is about 1900 C.
  • the composite electrode may be of flattened form, whereby the penetration into the parts to be surfaced, and therefore the dilution, are generally reduced.
  • the strip or wire of cobalt alloy may also be used as an electrode for hard surfacing under a flux.
  • a powder mixture containing chromium, tungsten and carbon is disposed in a manner known per se on the article to be hard-surfaced, where after the hardsurfacing operation is performed.
  • the flux may contain metallic additions of chromium, tungsten and carbon such that the desired alloy is produced in the melting.
  • a flux containing about 6% of tungsten, 20% of chromium carbide, Cr C and 6% of metallic chromium, the remainder consisting of slag-forming elements gave, under a current of 600 amperes at 34 volts, with an electrode wire containing 95% of cobalt and 4% of iron, a deposit of high cobalt content containing about 5% of tungsten, 23% of chromium, 1.5% of carbon and 5% of iron.
  • a cold-shapable cobalt alloy consisting of at least 93% by weight of cobalt, 0.5 to 6% by weight of iron, at least one of the metals of the group consisting of manganese, titanium, and aluminum, and also incidental impurities, the amount of which is insuflicient to have an effect upon the properties of said alloy, any manganese, titanium and aluminum contents being in the ranges from traces to 4.5% by weight for manganese, 0.1 to 2% by weight for titanium, and 0.1 to 2% by weight for aluminum, the sum of the iron content of said alloy, of of its manganese content, of 7 of its titanium content, and of of its aluminum content being below 7 of its total weight.
  • a composite welding electrode comprising on the one hand, a continuous metallic portion, and On the other hand, a mixture including substances forming slag and the principal alloying ingredients of stellite consisting of chromium, tungsten and carbon, in which said continuous metallic portion consists of an alloy of at least 93% by weight of cobalt, 0.5 to 6% by weight of iron, at least one of the metals of the group consisting of manganese, titanium and aluminum, and also incidental impurities, the amount of which is insufficient to have an eflect upon the properties of said alloy, any manganese, titanium and aluminum contents being in the ranges from traces to 4.5 by weight for manganese, 0.1 to 2% by weight for titanium, and 0.1 to 2% by weight for aluminum, and the sum of the iron content of said alloy, of of its manganese content, of 75, of its titanium content and of of its aluminum content, being below 7 of its total weight, and in which said mixture contains 25 to 35% of chromium, 3 to of tungsten, and
  • a composite Welding electrode comprising, on the one hand, a continuous metallic tubular sheath and, on the other hand, a core in said sheath, including substances forming slag and the principal alloying ingredients of stellite consisting of chromium, tungsten and carbon, in which said metallic tubular sheath consists of an alloy of at least 93% by weight of cobalt, 0.5 to 6% by weight of iron, at least one of the metals of the group consist ing of manganese, titanium and aluminum, and also incidental impurities the amount of which is insufiicient to have an effect upon the properties of said alloy, any manganese, titanium and aluminum contents being in the ranges from traces to 4.5% by weight for manganese, 0.1 to 2% by weight for titanium, .and 0.1 to 2% by weight for aluminum, and the sum of the iron content of said alloy of of its manganese content, of of its titanium content, and of of its aluminum content being below 9 of its total weight and'in which such core contains
  • a composite welding electrode comprising, on the one hand, a continuous metalic tubular sheath and on the other hand, a core in said sheath in which said metallic tubular sheath consists of an alloy of at least 93% by weight of cobalt, 0.5 to 6% by weight of iron, at least one of the metals of the group consisting of manganese, titanium and aluminum, and also incidental impurities, the amount of which is insufiicient to have an effect upon the properties of said alloy, any manganese, titanium, and aluminum contents being in the range from traces to 4.5% by weight for manganese, 0.1 to 2% by weight for titanium, and 0.1 to 2% by weight for aluminum, and the sum of the iron content of said alloy, of of its manganese content, of 1 of its titanium content and of %00 of its aluminum content being below 7 of its total weight, and in which said core comprises a mixture of substances forming slag by fusion and of chromium, cobalt and carbon in a proportion suflicient to form
  • a submerged arc welding process comprising depositing upon a joint of parts to be welded, a layer of flux containing, on the one hand, substances which form a slag on the welding bath by melting, and on the other hand, chromium, tungsten, and carbon, and striking an electrode arc in said layer of flux, between the parts to be welded and a metallic electrode which consists of an alloy of at least 93% by weight of cobalt, 0.5 to 6% by weight of iron, at least one of the metals of the group consisting of manganese, titanium, and aluminum, and also incidental impurities the amount of which is insuflicient to have an effect upon the properties of said alloy, any manganese, titanium or aluminum contents being in the range from traces to 4.5 by weight for manganese, 0.1 to 2% by weight for titanium and 0.1 to 2% by weight for aluminum, and the sum of the iron content of said alloy, of of its manganese content, of 5 of its titanium content of of of its aluminum content, being below of its total

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Nonmetallic Welding Materials (AREA)
US537716A 1965-04-12 1966-03-28 Cobalt alloy and welding electrode based upon this alloy Expired - Lifetime US3445624A (en)

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BE662408 1965-04-12
BE11393 1965-04-12

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JP (1) JPS4827584B1 (enrdf_load_html_response)
BE (1) BE662408A (enrdf_load_html_response)
DE (1) DE1783126C3 (enrdf_load_html_response)
GB (1) GB1148321A (enrdf_load_html_response)
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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3501277A (en) * 1966-03-11 1970-03-17 Coast Metals Inc Ductile cobalt strip
US3932204A (en) * 1969-10-31 1976-01-13 Elect & Magn Alloys Res Inst Cobalt-aluminum magnetic materials with high coercive force
US5844153A (en) * 1995-07-12 1998-12-01 Emtec Magnetics Gmbh Cobalt binder metal alloy
US6060181A (en) * 1998-08-17 2000-05-09 Mcdonnell Douglas Corporation Low loss magnetic alloy
US6063445A (en) * 1998-08-17 2000-05-16 Mcdonnell Douglas Corporation Method of preparation of polymer substrates for metal plating
US6376063B1 (en) 1998-06-15 2002-04-23 The Boeing Company Making particulates of controlled dimensions by electroplating
US20120110848A1 (en) * 2010-11-08 2012-05-10 United Technologies Corporation Low and extra low sulfur alloys for repair
CN112643245A (zh) * 2021-01-11 2021-04-13 中国科学院金属研究所 一种高温合金焊接用钴基合金焊丝及其制备方法和应用

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2440995A1 (de) * 1974-08-27 1976-03-11 Castolin Gmbh Schweissmaterial fuer das pulverschweissen
CN107335940A (zh) * 2017-08-26 2017-11-10 芜湖鼎瀚再制造技术有限公司 气门喷焊用钴铬钨合金粉及其焊接工艺

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3091022A (en) * 1959-03-25 1963-05-28 Union Carbide Corp Cold-formable predominantly cobalt alloys
US3286075A (en) * 1964-08-04 1966-11-15 Boehler & Co Ag Geb Process of welding a precipitation-hardenable austenitic steel

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3091022A (en) * 1959-03-25 1963-05-28 Union Carbide Corp Cold-formable predominantly cobalt alloys
US3286075A (en) * 1964-08-04 1966-11-15 Boehler & Co Ag Geb Process of welding a precipitation-hardenable austenitic steel

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3501277A (en) * 1966-03-11 1970-03-17 Coast Metals Inc Ductile cobalt strip
US3932204A (en) * 1969-10-31 1976-01-13 Elect & Magn Alloys Res Inst Cobalt-aluminum magnetic materials with high coercive force
US5844153A (en) * 1995-07-12 1998-12-01 Emtec Magnetics Gmbh Cobalt binder metal alloy
US6376063B1 (en) 1998-06-15 2002-04-23 The Boeing Company Making particulates of controlled dimensions by electroplating
US6699579B2 (en) 1998-06-15 2004-03-02 The Boeing Company Particulates of controlled dimension
US6060181A (en) * 1998-08-17 2000-05-09 Mcdonnell Douglas Corporation Low loss magnetic alloy
US6063445A (en) * 1998-08-17 2000-05-16 Mcdonnell Douglas Corporation Method of preparation of polymer substrates for metal plating
US20120110848A1 (en) * 2010-11-08 2012-05-10 United Technologies Corporation Low and extra low sulfur alloys for repair
US10173291B2 (en) 2010-11-08 2019-01-08 United Technologies Corporation Low and extra low sulfur alloys for repair
CN112643245A (zh) * 2021-01-11 2021-04-13 中国科学院金属研究所 一种高温合金焊接用钴基合金焊丝及其制备方法和应用
CN112643245B (zh) * 2021-01-11 2022-02-22 中国科学院金属研究所 一种高温合金焊接用钴基合金焊丝及其制备方法和应用

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JPS4827584B1 (enrdf_load_html_response) 1973-08-23
GB1148321A (en) 1969-04-10
BE662408A (enrdf_load_html_response)
DE1783126A1 (de) 1972-03-02
DE1783126B2 (de) 1973-06-07
DE1783126C3 (de) 1974-01-03
SE326089B (enrdf_load_html_response) 1970-07-13

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