发明名称 Adjustable blade profile for helicopter rotor blade has variable spring force acting between blade body and profile edge adjusted relative to blade longitudinal direction
摘要 The adjustable blade profile is provided by a blade body and a pair of profile edges, at least one profile edge (VPk) adjusted relative to an axis extending in the direction of the blade longitudinal axis. A spring (1) acting between the blade body and the adjustable profile edge has a spring characteristic that alters in dependence on the centrifugal force. The spring (1) acting between the blade body (5) and the profile edge (VPk) may be provided by a spring blade (2) with a piezo actuator at one end.
申请公布号 DE19859041(C1) 申请公布日期 2000.03.09
申请号 DE19981059041 申请日期 1998.12.21
申请人 DAIMLERCHRYSLER AG 发明人 MUELLER, GUENTHER
分类号 B64C3/48;B64C27/467;B64C27/473;B64C27/615;(IPC1-7):B64C27/54;B64C27/46 主分类号 B64C3/48
代理机构 代理人
主权项
地址