US2014219859A1PendingUtilityA1
Alloys for hardbanding weld overlays
Est. expirySep 17, 2029(~3.2 yrs left)· nominal 20-yr term from priority
C22C 38/24C23C 30/00C22C 38/04B23K 35/3093C22C 38/34C23C 4/073C22C 38/26C22C 38/28B23K 35/3053C22C 45/02C22C 38/58C23C 4/06C22C 33/08C21D 2211/005C22C 38/54C22C 38/02C22C 38/32C21D 2211/004C22C 38/46C22C 38/48B23K 35/308C22C 38/22C22C 38/44C22C 38/50C22C 38/06C22C 38/38
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Claims
Abstract
Disclosed herein are iron-based alloys having a microstructure comprising a fine-grained ferritic matrix and having a 60+ Rockwell C surface, wherein the ferritic matrix comprises <10 μm carbide precipitates. Also disclosed are methods of welding comprising forming a crack free hardbanding weld overlay coating with such an iron-based alloy. Also disclosed are families of alloys capable of forming crack-free weld overlays after multiple welding passes.
Claims
exact text as granted — not AI-modified1 - 23 . (canceled)
24 . A composition of matter comprising:
Fe; between 4-6 wt. % Cr; between 0.8-1.2 wt. % Mn; between 4-5 wt. % Nb; between 0-1 wt. % V; between 0.6-1.1 wt. % C; between 0.1-0.5 wt. % Ti; and between 0.4-0.75 wt. % Si.
25 . The composition of matter of claim 24 , further comprising:
B in an amount of 2.25 wt. % or less; and Mo in an amount of 4 wt. % or less.
26 . The composition of matter of claim 24 , wherein the composition is a welding wire.
27 . The composition of matter of claim 24 , wherein the composition is a weld.
28 . An alloy comprising:
Fe; between 4-6 wt. % Cr; between 0.8-1.2 wt. % Mn; between 4-5 wt. % Nb; between 0-1 wt. % V; between 0.6-1.1 wt. % C; between 0.1-0.5 wt. % Ti; and between 0.4-0.75 wt. % Si.
29 . The alloy of claim 28 , further comprising:
B in an amount of 2.25 wt. % or less; and Mo in an amount of 4 wt. % or less.
30 . The alloy of claim 28 , wherein the alloy has a Rockwell C hardness greater than 50.
31 . The alloy of claim 30 , wherein the alloy has a Rockwell C hardness greater than 55.
32 . The alloy of claim 28 , wherein the alloy has a microstructure comprising a fine-grained matrix, wherein the matrix comprises Nb-carbide precipitates having sizes less than 10 μm and hard precipitates having grain sizes less than 10 μm.
33 . The alloy of claim 28 , wherein the alloy is capable of being deposited as a weld overlay coating.
34 . The alloy of claim 28 , wherein the alloy is capable of being deposited using a MIG welding technique on a tool joint.
35 . The alloy of claim 28 , wherein the alloy is capable of being deposited crack-free when deposited on a substrate that is pre-heated to at least 500° F.
36 . The alloy of claim 28 , wherein the alloy is capable of being welded in two layers onto a 4137 6⅝″ O.D. tool joint to achieve a total weld thickness of at least 8/32″ without cracking.
37 . The alloy of claim 36 , wherein the alloy is capable of being deposited as a 10/32″ thick double pass weld overlay without cracking.
38 . The alloy of claim 36 , wherein the alloy exhibits a mass loss less than 0.3 g lost in ASTM G65 Procedure A.Cited by (0)
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