Method for manufacturing gas turbine part

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United States of America Patent

PATENT NO 10612382
SERIAL NO

15349394

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Abstract

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The present disclosure relates to building very large gas turbines without changing rotor materials. The gas turbine part can include a structure composed of a metal and a ternary ceramic called MAX phase, having a 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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Patent Owner(s)

Patent OwnerAddress
ANSALDO ENERGIA IP UK LIMITED5TH FLOOR NORTH SIDE 7/10 CHANDOS STREET CAVENDISH SQUARE LONDON W1G9DQ

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Bahraini, Hasani Maryam Lupfig, CH 3 10
Bossmann, Hans-Peter Lauchringen, DE 32 601

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