Nickel-base precipitation hardenable alloys with improved hydrogen embrittlement resistance
Abstract
Nickel-base precipitation hardenable alloys with enhanced hydrogen embrittlement resistance and desired yield strength have critical ranges of titanium and iron, among other elements. One of the nickel-base precipitation hardenable alloys has a composition, in wt.%, of Cr from about 18.0% to about 23.0%, Fe from about 7.0% to about 12.0%, Mo from about 6.5% to about 9.5%, Nb from about 3.2% to about 5.2%, Ti from about 0.3% to about 1.3%, Al up to about 0.4%, with a balance of Ni and incidental impurities. This alloy has a yield strength (0.2% offset) greater than or equal to 120 ksi (827 MPa), a plastic strain ratio greater than or equal to 0.35, and a plastic strain to failure greater than or equal to 9.0%.
Claims
exact text as granted — not AI-modifiedWhat is claimed is:
1 . A nickel-based precipitation hardenable alloy comprising:
a composition, in weight percent, comprising:
chromium from about 18.0% to about 23.0%;
iron from about 7.0% to about 12.0%;
molybdenum from about 6.5% to about 9.5%;
niobium from about 3.2% to about 5.2%;
titanium from about 0.3% to about 1.3%;
aluminum up to about 0.4%; and
balance nickel and incidental impurities;
wherein the nickel-based precipitation hardenable alloy has:
a yield strength (0.2% offset) greater than or equal to about 120 ksi (827 MPa);
a plastic strain ratio greater than or equal to 0.35; and
a plastic strain to failure greater than or equal to 9.0%.
2 . The nickel-based precipitation hardenable alloy according to claim 1 , wherein the titanium is between about 0.8% to about 1.1% and the iron is between about 9.0% to about 12.0%.
3 . The nickel-based precipitation hardenable alloy according to claim 1 , wherein the titanium is between about 0.8% to about 1.0% and the iron is between about 10.0% to about 12.0%.
4 . The nickel-based precipitation hardenable alloy according to claim 1 , wherein the titanium is between about 0.4% to about 0.8% and the iron is between about 10.0% to about 12.0%.
5 . The nickel-based precipitation hardenable alloy according to claim 1 , wherein the yield strength (0.2% offset) is between about 120 ksi (827 MPa) and 150 ksi (1034 MPa).
6 . The nickel-based precipitation hardenable alloy according to claim 1 , wherein the plastic strain ratio is greater than or equal to 0.40, and the plastic strain to failure is greater than or equal to 10.0%.
7 . The nickel-based precipitation hardenable alloy according to claim 1 , wherein the plastic strain ratio is greater than or equal to 0.50, and the plastic strain to failure is greater than or equal to 12.0%.
8 . A nickel-based precipitation hardenable alloy comprising:
a composition, in weight percent, comprising:
chromium from about 18.0% to about 23.0%;
iron from about 9.0% to about 16.0%;
molybdenum from about 4.5% to about 7.5%;
niobium from about 3.2% to about 5.2%;
titanium from about 0.4% to about 1.3%;
aluminum up to about 0.4%; and
balance nickel and incidental impurities;
wherein the nickel-based precipitation hardenable alloy has:
a yield strength (0.2% offset) greater than or equal to about 120 ksi (827 MPa);
a plastic strain ratio greater than or equal to 0.30; and
a plastic strain to failure greater than or equal to 8.5%.
9 . The nickel-based precipitation hardenable alloy according to claim 8 , wherein the titanium is between about 0.8% to about 1.1% and the iron is between about 11.0% to about 16.0%.
10 . The nickel-based precipitation hardenable alloy according to claim 8 , wherein the titanium is between about 0.8% to about 1.0% and the iron is between about 12.0% to about 16.0%.
11 . The nickel-based precipitation hardenable alloy according to claim 8 , wherein the titanium is between about 0.5% to about 0.8% and the iron is between about 12.0% to about 16.0%.
12 . The nickel-based precipitation hardenable alloy according to claim 8 , wherein the yield strength (0.2% offset) is between about 120 ksi (827 MPa) and 150 ksi (1034 MPa).
13 . The nickel-based precipitation hardenable alloy according to claim 8 , wherein the plastic strain ratio is greater than or equal to 0.35, and the plastic strain to failure is greater than or equal to 9.0%.
14 . The nickel-based precipitation hardenable alloy according to claim 8 , wherein the plastic strain ratio is greater than or equal to 0.45, and the plastic strain to failure is greater than or equal to 10.0%.
15 . A nickel-based precipitation hardenable alloy comprising:
a composition, in weight percent, comprising:
chromium from about 18.0% to about 23.0%;
iron from about 15.0% to about 21.0%;
molybdenum from about 3.0% to about 4.5%;
niobium from about 3.2% to about 5.2%;
titanium from about 0.5% to about 1.3%;
aluminum up to about 0.4%;
copper from about 0.5% to about 3.0%; and
balance nickel and incidental impurities;
wherein the nickel-based precipitation hardenable alloy has:
a yield strength (0.2% offset) greater than or equal to about 140 ksi (965 MPa);
a plastic strain ratio greater than or equal to 0.30; and
a plastic strain to failure greater than or equal to 8.0%.
16 . The nickel-based precipitation hardenable alloy according to claim 15 , wherein the titanium between about 0.8% to about 1.1% and the iron is between about 16.0% to about 21.0%.
17 . The nickel-based precipitation hardenable alloy according to claim 15 , wherein the titanium between about 0.8% to about 1.0% and the iron is between about 17.0% to 20.0%.
18 . The nickel-based precipitation hardenable alloy according to claim 15 , wherein the titanium between about 0.5% to about 0.8% and the iron is between about 18% to about 21.0%.
19 . The nickel-based precipitation hardenable alloy according to claim 15 , wherein the yield strength (0.2% offset) is between about 140 ksi (965 MPa) and 170 ksi (1172 MPa).
20 . The nickel-based precipitation hardenable alloy according to claim 15 , wherein the plastic strain ratio is greater than or equal to 0.35, and the plastic strain to failure is greater than or equal to 9.0%.
21 . The nickel-based precipitation hardenable alloy according to claim 15 , wherein the plastic strain ratio is greater than or equal to 0.45, and the plastic strain to failure is greater than or equal to 10.0%.Join the waitlist — get patent alerts
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