发明名称 Helicopter rotor blade flap actuator
摘要 The arrangement has a tilting element (10) pivotably mounted on a counter bearing element (40). A bearing is formed by a convex roller surface (60) on the tilting element or counter bearing element in contact with a concave roller surface (50) on the counter bearing element or tilting element. The radius of the concave roller surface is larger than that of the convex roller surface.
申请公布号 EP1157924(A3) 申请公布日期 2003.11.26
申请号 EP20010111908 申请日期 2001.05.17
申请人 EADS DEUTSCHLAND GMBH 发明人 JAENKER, PETER, DR.
分类号 B64C27/473;B64C27/615;B64C27/68;F16C11/00;(IPC1-7):B64C27/615 主分类号 B64C27/473
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