发明名称 PROPELLER BLADES HAVING ICEPHOBIC COATING
摘要 A propeller blade (1) for rotation about a hub assembly has disposed thereon at least along a leading edge (7) a coating (6) comprising an icephobic material, the coating (6) extending along the blade (1) from a radially inner region (9) to a radially outer region (10), wherein the radially outer region (10) is disposed between the blade root and the blade tip at a position where rotational forces on the blade (1) are sufficient, in use, to cause removal of ice from an uncoated blade (1).
申请公布号 CA2751861(A1) 申请公布日期 2012.03.15
申请号 CA20112751861 申请日期 2011.09.08
申请人 GE AVIATION SYSTEMS LIMITED 发明人 TOWKAN, MICHAEL FEDOR
分类号 B64D15/18;B32B7/10;B64C11/16;C09K3/18 主分类号 B64D15/18
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