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US4161207A Expired / Lapsed US ⏱️ 0.0 years remaining

Production of carbide laden consumables in a graphite mold

Assignee: Eutectic Corp
•
Filing: 1978-01-19
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Granted: 1979-07-17
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Expires: 1998-01-19
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Abstract

Abstract A carbide laden consumable is produced using a mold having at least one U-shaped groove running along the surface thereof, the consumable being produced by charging a first layer of a powdered self-fluxing alloy into the groove, a second layer of a powdered refractory carbide on said first layer and a third layer of said self-fluxing alloy on the carbide layer, and the charged mold then passed through a heating furnace under a reducing atmosphere to produce by melting and cooling a consumable of markedly improved quality.

Inventors

  • 👤 Jean L. Fluckiger
  • 👤 Rene Wasserman

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-02 21:23
CPC Classifications
B; B23; B23K; B23K35/00; B23K35/40; B23K35/22; B23K35/24; B23K35/32; B23K35/327; C; C23; C23C; C23C4/00; C23C4/04; C23C4/06; Y; Y10; Y10T; Y10T428/00; Y10T428/12; Y10T428/12493; Y10T428/12535; Y10T428/12576

Claims Analysis

Total Claims: 9
Claim 1
Independent Claim 347 words
A method of producing a carbide laden consumable in the form of a composite rod which comprises, providing a graphite mold having at least one elongated U-shaped groove therein, said at least one groove containing a charge of fusible ingredients comprising a first layer of powdered self-fluxing matrix metal alloy at the bottom of said groove, a second layer of particulate refractory metal carbide on top of said first layer and a third layer of said matrix metal alloy on top of said second layer, said first layer of said powdered matrix metal constituting about 25% to 50% of the total combined first and third layers, with the third layer making up the balance of the total combined first and third layers. the composition of said matrix metal alloy and said refractory carbide together in said mold ranging by weight from about 80% to 30% of said matrix metal alloy and the balance consisting essentially of about 20% to 70% of said refractory metal carbide, said self-fluxing matrix metal alloy being selected from the group consisting of Ni-base, Ni-Cu-base, Fe-base and Co-base alloys containing by weight at least one element selected from the group consisting of about 0.1% to 6% of silicon and about 0.1% to 5% boron and having a melting point ranging up to about 1370° C., said refractory metal carbide being selected from the group consisting of carbides of W, Mo, Cr, Zr, Ti, Hf, Nb, Ta, V, B and Si and mixtures of at least two of said carbides, passing said graphite mold through a furnace having a heating zone maintained at a temperature above the melting point of said matrix alloy, said furnace having a cooling zone immediately after said heating zone, the atmosphere in said furnace being reducing, causing said matrix alloy to melt and infiltrate the interstices in said carbide layer, and passing said graphite mold into said cooling zone immediately after said heating zone to solidify said matrix alloy and inhibit segregation of said refractory carbide to thereby produce a composite rod characterized by improved quality and improved strength.
Claim 2
Independent Claim 347 words
A method of producing a carbide laden consumable in the form of a composite rod which comprises, providing a graphite mold having at least one elongated U-shaped groove therein, said at least one groove containing a charge of fusible ingredients comprising a first layer of powdered self-fluxing matrix metal alloy at the bottom of said groove, a second layer of particulate refractory metal carbide on top of said first layer and a third layer of said matrix metal alloy on top of said second layer, said first layer of said powdered matrix metal constituting about 25% to 50% of the total combined first and third layers, with the third layer making up the balance of the total combined first and third layers. the composition of said matrix metal alloy and said refractory carbide together in said mold ranging by weight from about 80% to 30% of said matrix metal alloy and the balance consisting essentially of about 20% to 70% of said refractory metal carbide, said self-fluxing matrix metal alloy being selected from the group consisting of Ni-base, Ni-Cu-base, Fe-base and Co-base alloys containing by weight at least one element selected from the group consisting of about 0.1% to 6% of silicon and about 0.1% to 5% boron and having a melting point ranging up to about 1370° C., said refractory metal carbide being selected from the group consisting of carbides of W, Mo, Cr, Zr, Ti, Hf, Nb, Ta, V, B and Si and mixtures of at least two of said carbides, passing said graphite mold through a furnace having a heating zone maintained at a temperature above the melting point of said matrix alloy, said furnace having a cooling zone immediately after said heating zone, the atmosphere in said furnace being reducing, causing said matrix alloy to melt and infiltrate the interstices in said carbide layer, and passing said graphite mold into said cooling zone immediately after said heating zone to solidify said matrix alloy and inhibit segregation of said refractory carbide to thereby produce a composite rod characterized by improved quality and improved strength.
Claim 3
Independent Claim 463 words
A method of producing a carbide laden consumable in the form of a composite rod which comprises, providing a graphite mold having at least one elongated U-shaped groove therein, said at least one groove containing a charge of fusible ingredients comprising a first layer of powdered self-fluxing matrix metal alloy at the bottom of said groove, a second layer of particulate refractory metal carbide on top of said first layer and a third layer of said matrix metal alloy on top of said second layer, said first layer of said powdered matrix metal constituting about 25% to 50% of the total combined first and third layers, with the third layer making up the balance of the total combined first and third layers, the composition of said matrix metal alloy and said refractory carbide together in said mold ranging by weight from about 80% to 30% of said matrix metal alloy and the balance consisting essentially of about 20% to 70% of said refractory metal carbide, said self-fluxing alloy being selected from the group consisting of: (A) nickel-base matrix alloy containing about 1.5% to 5% Si, about 1.5% to 5% boron, up to about 20% chromium, up to about 7% molybdenum and the balance essentially nickel; (B) cobalt-base matrix alloys containing about 1% to 5% nickel, about 26% to 32% chromium, about 0.5% to 3% silicon, about 1% to 3% boron, about 0.8 to 2% carbon, about 3.5% to 7.5% tungsten, up to about 0.5% molybdenum and the balance essentially cobalt; (C) nickel-copper-base matrix alloys containing about 1% to 5% silicon, about 0.15% to 2.5% boron, about 0.2% to 2% manganese, about 15% to 40% copper and the balance essentially nickel; and (D) nickel silver matrix alloys containing about 2% to 20% nickel, about 28% to 58% zinc, 0.1% to 1% silicon, up to 1% silver and essentially the balance ranging from about 40% to 65% copper, said matrix alloy having a melting point ranging up to about 1370° F., said refractory carbide being selected from the group consisting of W, Mo, Cr, Zr, Ti, Hf, Nb, Ta, V, B and Si and mixtures of at least two of said carbides, passing said graphite mold on a conveyor through a furnace having a heating zone maintained at a temperature above the melting point of said matrix alloy, said furnace having a cooling zone immediately after said heating zone, the atmosphere in said furnace being reducing, causing said matrix alloy to melt and infiltrate the interstices in said carbide layer from said first and third layers, said passing said graphite mold into said cooling zone immediately after said heating zone to solidify said matrix alloy and inhibit segregation of said refractory carbide to thereby produce a composite rod characterized by improved quality and improved strength.
Claim 4
Independent Claim 463 words
A method of producing a carbide laden consumable in the form of a composite rod which comprises, providing a graphite mold having at least one elongated U-shaped groove therein, said at least one groove containing a charge of fusible ingredients comprising a first layer of powdered self-fluxing matrix metal alloy at the bottom of said groove, a second layer of particulate refractory metal carbide on top of said first layer and a third layer of said matrix metal alloy on top of said second layer, said first layer of said powdered matrix metal constituting about 25% to 50% of the total combined first and third layers, with the third layer making up the balance of the total combined first and third layers, the composition of said matrix metal alloy and said refractory carbide together in said mold ranging by weight from about 80% to 30% of said matrix metal alloy and the balance consisting essentially of about 20% to 70% of said refractory metal carbide, said self-fluxing alloy being selected from the group consisting of: (A) nickel-base matrix alloy containing about 1.5% to 5% Si, about 1.5% to 5% boron, up to about 20% chromium, up to about 7% molybdenum and the balance essentially nickel; (B) cobalt-base matrix alloys containing about 1% to 5% nickel, about 26% to 32% chromium, about 0.5% to 3% silicon, about 1% to 3% boron, about 0.8 to 2% carbon, about 3.5% to 7.5% tungsten, up to about 0.5% molybdenum and the balance essentially cobalt; (C) nickel-copper-base matrix alloys containing about 1% to 5% silicon, about 0.15% to 2.5% boron, about 0.2% to 2% manganese, about 15% to 40% copper and the balance essentially nickel; and (D) nickel silver matrix alloys containing about 2% to 20% nickel, about 28% to 58% zinc, 0.1% to 1% silicon, up to 1% silver and essentially the balance ranging from about 40% to 65% copper, said matrix alloy having a melting point ranging up to about 1370° F., said refractory carbide being selected from the group consisting of W, Mo, Cr, Zr, Ti, Hf, Nb, Ta, V, B and Si and mixtures of at least two of said carbides, passing said graphite mold on a conveyor through a furnace having a heating zone maintained at a temperature above the melting point of said matrix alloy, said furnace having a cooling zone immediately after said heating zone, the atmosphere in said furnace being reducing, causing said matrix alloy to melt and infiltrate the interstices in said carbide layer from said first and third layers, said passing said graphite mold into said cooling zone immediately after said heating zone to solidify said matrix alloy and inhibit segregation of said refractory carbide to thereby produce a composite rod characterized by improved quality and improved strength.
Claim 5
Dependent Claim 13 words
The method of claim 2, wherein the reducing atmosphere is a hydrogen-containing atmosphere.
Claim 6
Dependent Claim 23 words
The method of claim 3, wherein the hydrogen-containing atmosphere comprises 10% to 70% by volume of hydrogen and the balance an inert atmosphere.
Claim 7
Dependent Claim 12 words
The method of claim 4, wherein the hydrogen-containing atmosphere is cracked ammonia.
Claim 8
Dependent Claim 49 words
The method of claim 3, wherein the powdered matrix metal alloy has a particle size less than about 200 mesh with up to 50% by weight less than 325 mesh, and wherein the powdered refractory metal carbide has a particle size ranging from about 5 microns to 3/4 inch.
Claim 9
Dependent Claim 24 words
The method of claim 6, wherein the refractory carbide is tungsten carbide of particle size of plus 60 mesh to 3/8 of an inch.

References Cited (Backward Citations)

US2002462A Cited
US1910884A Cited
US1977128A Cited
US2137471A Cited
US3028644A Cited
US3109917A Cited
US3523569A Cited
US3458685A Cited
US3627979A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1982-07-16 1983-01-15 1983-07-17 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1986-07-16 1987-01-15 1987-07-17 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1990-07-16 1991-01-15 1991-07-17 $7700.00 Window Closed / Lapsed

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