Gas turbine part and method for manufacturing such gas turbine part
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United States of America
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Feb 25, 2020
Grant Date -
May 18, 2017
app pub date -
Nov 11, 2016
filing date -
Nov 11, 2016
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Abstract
The present disclosure relates to a gas turbine part, which can be exposed to high temperatures and centrifugal forces within a gas turbine. The gas turbine part can include plural sliced parts, wherein at least one of said sliced parts is made from a ternary ceramic called MAX phase, having the formula Mn+1AXn, where n=1, 2, or 3, M is an early transition metal such as Ti, V, Cr, Zr, Nb, Mo, Hf, Sc, Ta, and A is an A-group element such as Al, Si, P, S, Ga, Ge, As, Cd, In, Sn, Tl, Pb, and X is C and/or N.
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