An alloy comprising rhodium, aluminum, and chromium, wherein a microstructure of the alloy comprises a face-centered-cubic phase and a B2-structured phase and is essentially free of an L12-structured phase at temperatures greater than about 1000.degree. C., and a gas turbine engine component comprising the alloy.

Uma liga que compreende o rhodium, o alumínio, e o cromo, wherein um microstructure da liga compreende uma fase cara-centr-cúbica e uma fase de B2-structured e está essencialmente livre de uma fase de L12-structured nas temperaturas mais grandes do que sobre 1000.degree. C., e um componente de motor da turbina do gás que compreende a liga.

 
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