发明名称 Manufacture of monocrystalline aerodynamic blades
摘要 A monocrystalline aerodynamic blade constituted by two platforms (13,14) enframing an aerofoil (12) is manufactured by disposing the shells of the mould in such a manner that the platforms (13,14) are parallel to the plane of a baffle (18,19,20,21) for grain selection which discharges into a junction (22) leading the grain to the two platforms, and in supplying the mould through a filler (23,24) at the upper ends (13 a ,14 a ) of the platforms. The platforms (13,14) are parallel to the direction [001] of the selected monocrystal, and the generating lines of the aerofoil (12) are parallel to one of the horizontal directions [101] and [100].
申请公布号 GB2301303(A) 申请公布日期 1996.12.04
申请号 GB19810036625 申请日期 1981.12.04
申请人 * SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION 发明人 MARTIAL GERARD * ALESSANDRI;JEAN-MARC * THERET
分类号 C30B11/00;C30B11/14 主分类号 C30B11/00
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