High-Temperature Creep and Oxidation Behavior of Mo-Si-B Alloys with High Ti Contents

Overview of attention for article published in Metallurgical and Materials Transactions A, August 2013

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In the top 25% of all research outputs scored by Altmetric
Among the highest-scoring outputs from this source (#42 of 908)
Good Attention Score compared to outputs of the same age (76th percentile)
Above-average Attention Score compared to outputs of the same age and source (57th percentile)

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patent: 5 patents

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So far, Altmetric has seen 5 patents that reference this research output.

Turbine blade and aircraft engine comprising same

Grant US-10577948-B2

United States of America

Method for producing a component from a composite material comprising a metal matrix and…

Application US-10458001-B2

United States of America

TURBINE BLADE AND AIRCRAFT ENGINE COMPRISING SAME

Application US-20170122256-A1

United States of America

BLADE FOR A TURBINE ENGINE MADE FROM DIFFERENT MATERIALS AND METHOD FOR PRODUCING THE SAME

Application EP-3069803-A1

European Patent Office

METHOD FOR PRODUCING A COMPONENT MADE OF A COMPOUND MATERIAL WITH A METAL MATRIX AND…

Application EP-3069802-A1

European Patent Office