Nickel Based Alloy with High Fatigue Resistance and Methods of Forming the Same

US2019241995A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2019241995-A1
Application numberUS-201815890681-A
CountryUS
Kind codeA1
Filing dateFeb 7, 2018
Priority dateFeb 7, 2018
Publication dateAug 8, 2019
Grant date

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  1. Title

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  2. Abstract

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  5. First independent claim

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Abstract

Official abstract text for this publication.

A nickel based alloy, along with methods of its use and manufacture, is provided that may include about 20 wt. % to about 26 wt. % cobalt; about 9 wt. % to about 13 wt. % chromium; about 2 wt. % to about 6 wt. % iron; about 3.5 wt. % to about 6 wt. % aluminum; about 9 wt. % to about 13 wt. % tungsten; about 6 wt. % to about 9 wt. % tantalum; about 0.06 wt. % to about 0.20 wt. % boron; and the balance nickel. The nickel based alloy may have gamma prime precipitates in a plurality of grain interiors and a gamma prime solvus temperature of about 1038° C. or greater. Additionally or alternatively, the nickel based alloy may comprise about 30% by volume or more gamma prime precipitates in the plurality of grain interiors.

First claim

Opening claim text (preview).

What is claimed is: 1 . A nickel based alloy, comprising: about 20 wt. % to about 26 wt. % cobalt; about 9 wt. % to about 13 wt. % chromium; about 2 wt. % to about 6 wt. % iron; about 3.5 wt. % to about 6 wt. % aluminum; about 9 wt. % to about 13 wt. % tungsten; about 6 wt. % to about 9 wt. % tantalum; about 0.06 wt. % to about 0.20 wt. % boron; and the balance nickel. 2 . The nickel based alloy according to claim 1 , wherein the nickel based alloy comprises gamma prime precipitates in a plurality of grain interiors and has a gamma prime solvus temperature of about 1038° C. or greater. 3 . The nickel based alloy according to claim 2 , wherein the nickel based alloy comprises about 30% by volume or more gamma prime precipitates in the plurality of grain interiors. 4 . The nickel based alloy according to claim 3 , wherein the nickel based alloy has a grain boundary phase fraction of about 20% by volume or more. 5 . The nickel based alloy according to claim 4 , wherein the nickel based alloy has a grain boundary phase lineal density of about 310 precipitates per mm or greater. 6 . The nickel based alloy according to claim 2 , wherein the nickel based alloy comprises precipitates of W-bearing phases along one or more grain boundaries. 7 . The nickel based alloy according to claim 6 , wherein the W-bearing phase comprises Laves phase, mu phase, beta phase, sigma phase, borides, or carbides. 8 . The nickel based alloy according to claim 1 , wherein the nickel based alloy comprises about 0.065 wt. % to about 0.155 wt. % boron. 9 . The nickel based alloy according to claim 1 , wherein the nickel based alloy comprises about 22% by weight to about 24% by weight cobalt, about 10% by weight to about 12% by weight chromium, about 3% by weight to about 5% by weight iron, about 4% by weight to about 5.5% by weight aluminum, about 10% by weight to about 12% by weight tungsten, about 7% by weight to about 8% by weight tantalum, and about 0.07% by weight to about 0.15% by weight boron. 10 . The nickel based alloy according to claim 1 , wherein the nickel based alloy further comprises greater than 0% by weight to about 0.1% by weight carbon. 11 . The nickel based alloy according to claim 1 , wherein the nickel based alloy further comprises about 0.02% by weight to about 0.08% by weight carbon. 12 . The nickel based alloy according to claim 1 , wherein the nickel based alloy further comprises greater than 0% by weight to about 0.5% by weight hafnium. 13 . The nickel based alloy according to claim 1 , wherein the nickel based alloy further comprises greater than 0% by weight to about 0.1% by weight zirconium. 14 . A component for a gas turbine assembly comprising the nickel alloy of claim 1 . 15 . A nickel based alloy consisting of: about 20 wt. % to about 26 wt. % cobalt; about 9 wt. % to about 13 wt. % chromium; about 2 wt. % to about 6 wt. % iron; about 3.5 wt. % to about 6 wt. % aluminum; about 9 wt. % to about 13 wt. % tungsten; about 6 wt. % to about 9 wt. % tantalum; about 0.06 wt. % to about 0.20 wt. % boron; and the balance nickel. 16 . The nickel based alloy according to claim 15 , wherein boron is included in an amount of about 0.065 wt. % to about 0.155 wt. % boron. 17 . The nickel based alloy according to claim 15 , consisting of about 22% by weight to about 24% by weight cobalt, about 10% by weight to about 12% by weight chromium, about 3% by weight to about 5% by weight iron, about 4% by weight to about 5.5% by weight aluminum, about 10% by weight to about 12% by weight tungsten, about 7% by weight to about 8% by weight tantalum, and about 0.07% by weight to about 0.15% by weight boron.

Assignees

Inventors

Classifications

  • with the maximum Cr content being at least 10% but less than 20% · CPC title

  • of nickel or cobalt or alloys based thereon · CPC title

  • with the maximum Cr content being less 10% · CPC title

  • with chromium · CPC title

  • and Mo or W · CPC title

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What does patent US2019241995A1 cover?
A nickel based alloy, along with methods of its use and manufacture, is provided that may include about 20 wt. % to about 26 wt. % cobalt; about 9 wt. % to about 13 wt. % chromium; about 2 wt. % to about 6 wt. % iron; about 3.5 wt. % to about 6 wt. % aluminum; about 9 wt. % to about 13 wt. % tungsten; about 6 wt. % to about 9 wt. % tantalum; about 0.06 wt. % to about 0.20 wt. % boron; and the b…
Who is the assignee on this patent?
Gen Electric
What technology area does this patent fall under?
Primary CPC classification C22C30/00. Mapped technology areas include Chemistry & Metallurgy.
When was this patent published?
Publication date Thu Aug 08 2019 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 3 related publications on this page (citations in our corpus or others sharing the same primary CPC).