发明名称 LINED CENTRIFUGAL MOLD WITH CONTROLLED THERMAL INERTIA
摘要 The invention concerns a unit comprising a mould (4) adapted to receive a molten metal alloy and the said metal alloy poured therein. The alloy is TiAl. The mould is rotational and comprises receiving recesses (135) made of steel, metal alloy and/or ceramic, and, at the location of a plurality of section planes each passing through the mould and the poured metal alloy, the mould has a surface heat capacity less than that of the poured metal alloy,
申请公布号 EP3119544(A1) 申请公布日期 2017.01.25
申请号 EP20150706869 申请日期 2015.01.28
申请人 Safran Aircraft Engines 发明人 MARTIN, Guillaume;FARGEAS, Serge;SOISSON, Marc;PIATON, Valéry
分类号 B22D13/10;B22D27/20 主分类号 B22D13/10
代理机构 代理人
主权项
地址