发明名称 Erosion and fatigue resistant blade and blade coating
摘要 A coating is described for an airfoil blade component. The coating comprises a cermet material and has, when applied to the rotor blade, a compressive residual stress greater than about 60 ksi. In another embodiment, the compressive residual stress of the coating is in the range of approximately 90-110 ksi.
申请公布号 EP2631323(B1) 申请公布日期 2015.03.04
申请号 EP20120198621 申请日期 2012.12.20
申请人 SIKORSKY AIRCRAFT CORPORATION 发明人 CLAVETTE, PATRICK LOUIS;SHI, JUN;NARDI, AARON T.
分类号 C23C4/06;B64C11/20;C23C4/12;C23C30/00;F01D5/28 主分类号 C23C4/06
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