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.
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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 |
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代理人 |
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主权项 |
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地址 |
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