US2016201166A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016201166-A1 |
| Application number | US-201615079601-A |
| Country | US |
| Kind code | A1 |
| Filing date | Mar 24, 2016 |
| Priority date | Nov 19, 2009 |
| Publication date | Jul 14, 2016 |
| Grant date | — |
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.
A heat-resistant superalloy having chromium, aluminum, cobalt, titanium, and ruthenium added thereto as main components, and having a subcomponent(s) optionally added thereto, the remainder, excluding the main components and the subcomponent(s), comprising nickel and an impurity inevitably contained, wherein the amount of the chromium added is 2 to 25% by mass, the amount of the aluminum added is 0.2 to 7% by mass, the amount of the cobalt added is 19.5 to 55% by mass, the amount of the titanium added is [0.17×(% by mass for cobalt-23)+3] to [0.17×(% by mass for cobalt-20)+7]% by mass (with the proviso that the amount of the titanium added is 5.1% by mass or more), and the amount of the ruthenium added is 0.1 to 10% by mass.
Opening claim text (preview).
1 - 12 . (canceled) 13 . A method for forging a heat-resistant superalloy comprising forging the heat-resistant superalloy at about 1100° C., wherein the heat-resistant superalloy comprises chromium, aluminum, cobalt, titanium, and ruthenium as main components, optionally a subcomponent(s), and a remainder, excluding the main components and the subcomponent(s), of nickel and an inevitable impurity, wherein an amount of the chromium is 2 to 25% by mass, an amount of the aluminum is 0.2 to 7% by mass, an amount of the cobalt is 19.5 to 55% by mass, an amount of the titanium is [0.17×(% by mass for cobalt-23)+3] to [0.17×(% by mass for cobalt-20)+7]% by mass, with the proviso that the amount of the titanium is 5.1% by mass or more, and an amount of the ruthenium is 0.1 to 10% by mass. 14 . The method according to claim 13 , wherein a turbine disk is formed by forging the heat-resistant superalloy at about 1100° C. 15 . A heat-resistant superalloy comprising chromium, aluminum, cobalt, titanium, and ruthenium as main components, optionally a subcomponent(s), and a remainder, excluding the main components and the subcomponent(s), of nickel and an inevitable impurity, wherein an amount of the chromium is 2 to 25% by mass, an amount of the aluminum is 0.2 to 7% by mass, an amount of the cobalt is 19.5 to 55% by mass, an amount of the titanium is [0.17×(% by mass for cobalt-23)+3] to [0.17×(% by mass for cobalt-20)+7]% by mass, with the proviso that the amount of the titanium is 5.1% by mass or more, and an amount of the ruthenium is 0.1 to 10% by mass, and wherein a turbine disk is produced by high-temperature forging the heat-resistant superalloy at about 1100° C.
Nickel- or cobalt-based alloys · CPC title
Ruthenium · CPC title
discs, e.g. disc wheels · CPC title
Blade-carrying members, e.g. rotors (rotors of non-bladed type F01D1/34; stators F01D9/00 {; selecting particular materials F01D5/28}) · CPC title
with the maximum Cr content being at least 20% but less than 30% · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.