Development of two rhenium- containing superalloys for single- crystal blade and directionally solidified vane applications in advanced turbine engines

Overview of attention for article published in Journal of Materials Engineering and Performance, August 1993

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In the top 25% of all research outputs scored by Altmetric
Among the highest-scoring outputs from this source (#19 of 370)
Good Attention Score compared to outputs of the same age (73rd percentile)

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patent: 8 patents

Citations

dimensions_citation: 41 Dimensions

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mendeley: 58 Mendeley

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So far, Altmetric has seen 8 patents that reference this research output.

Turbine airfoil component and method for making

Grant US-8770944-B2

United States of America

Heat treatment method for bodies that comprise a nickel based superalloy

Grant US-7074284-B2

United States of America

Nickel-base superalloy

Grant US-6419763-B1

United States of America

Nickel base superalloy

Application EP-1054072-A1

European Patent Office

Nickel-base superalloy

Grant US-5888451-A

United States of America

Monocrystalline nickel-base superalloy with Ti, Ta, and Hf carbides

Grant US-5759301-A

United States of America

Blade for gas turbine

Grant US-5611670-A

United States of America

Low yttrium, high temperature alloy

Grant US-5443789-A

United States of America