发明名称 |
ACTIVE ROTOR BLADE ASSEMBLY |
摘要 |
The rotor blade actuator is provided with an actuator surface (104), which is designed for applying to a surface of a rotor blade, where a controlled active layer (110) is arranged parallel to the actuator surface. The layer has a controllability, which produces a driving change in length in a direction (101) along the actuator surface. Another controlled active layer is arranged over the former active layer. An independent claim is also included for a rotor blade for helicopter. |
申请公布号 |
EP2228300(B1) |
申请公布日期 |
2017.03.08 |
申请号 |
EP20100155936 |
申请日期 |
2010.03.09 |
申请人 |
Airbus Defence and Space GmbH |
发明人 |
Grohmann, Boris;Storm, Stefan |
分类号 |
B64C27/72 |
主分类号 |
B64C27/72 |
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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