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
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