Deposition welding with prior remelting
US-2015367445-A1 · Dec 24, 2015 · US
US9540714B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9540714-B2 |
| Application number | US-201313834985-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 15, 2013 |
| Priority date | Mar 15, 2013 |
| Publication date | Jan 10, 2017 |
| Grant date | Jan 10, 2017 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
An essentially cobalt-free alloy consists essentially of, in terms of weight percent: 6.3 to 7.2 Cr, 0.5 to 2 Al, 0 to 5 Fe, 0.7 to 0.8 Mn, 9 to 12.5 Mo, 0 to 6 Ta, 0.75 to 3.5 Ti, 0.01 to 0.25 Nb, 0.2 to 0.6 W, 0.02 to 0.04 C, 0 to 0.001 B, 0.0001 to 0.002 N, balance Ni. The alloy is characterized by a γ′ microstructural component in the range of 3 to 17.6 weight percent of the total composition. The alloy is further characterized by, at 850° C., a yield strength of at least 60 Ksi, a tensile strength of at least 70 Ksi, a creep rupture life at 12 Ksi of at least 700 hours, and a corrosion rate, expressed in weight loss [g/(cm 2 sec)]10 −11 during a 1000 hour immersion in liquid FLiNaK at 850° C., in the range of 5.5 to 17.
Opening claim text (preview).
What is claimed is: 1. A cobalt-free Υ′-strengthened alloy consisting essentially of, expressed in weight percent of the total composition: Cr 6.3 to 7.2 Al 0.5 to 2 Fe 0 to 5 Mn 0.7 to 0.8 Mo 9 to 12.5 Ta 0 to 6 Ti 0.99 to 3.5 Nb 0.01 to 0.25 W 0.2 to 0.6 C 0.02 to 0.04 B 0 to 0.0005 N 0.0001 to 0.002 Ni balance said alloy having a Υ′ microstructural component in an amount of calculated weight percent of at least 3 and no more than 17.6; and said alloy being characterized by, at 850° C., a yield strength of at least 60 Ksi, a tensile strength of at least 70 Ksi, and a creep rupture life at 12 Ksi of at least 700 hours, and a corrosion rate, expressed in weight loss [g/(cm 2 sec)]10 −11 during a 1000 hour immersion in liquid FLiNaK at 850° C., in the range of 5.5 to 17, and further characterized by a corrosion susceptibility index of no less than about 0.14 and no more than about 0.2. 2. An alloy in accordance with claim 1 wherein the range of Al is 0.75 to 2weight percent. 3. An alloy in accordance with claim 1 wherein the range of Fe is 0 to 0.05weight percent. 4. An alloy in accordance with claim 1 wherein said Υ′ microstructural component in an amount of a calculated weight percent of at least 3 and no more than 11.8. 5. An alloy in accordance with claim 4 wherein said Υ′ microstructural component in an amount of a calculated weight percent of at least 3 and no more than 9.4. 6. An alloy in accordance with claim 1 wherein said yield strength is at least 65 Ksi. 7. An alloy in accordance with claim 1 wherein said tensile strength is at least 75 Ksi. 8. An alloy in accordance with claim 1 wherein said creep rupture life is at least 750hours. 9. An alloy in accordance with claim 1 wherein said corrosion rate is no more than 8.4.
with the maximum Cr content being less 10% · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.