Foundry core for manufacturing a hollow metal aeronautical part

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United States of America Patent

PATENT NO 12121955
SERIAL NO

18579343

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Abstract

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Casting core for the manufacture of hollow metal aeronautical parts, in particular high-pressure turbine parts by lost-wax casting, including a composite material including on the one hand a first phase of formula Mn+1AlCn, where n=1 to 3 and M being a transition metal selected from the group consisting of titanium and/or niobium and/or molybdenum, the composite material including on the other hand a second phase of formula Al4C3.

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Patent Owner(s)

Patent OwnerAddress
SAFRANPARIS FRANCE PARIS PARIS

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Bechelany, Mirna Moissy-Cramayel, FR 11 7
Sallot, Pierre Jean Moissy-Cramayel, FR 16 0

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