发明名称 Rotor blade for a rotor airplane
摘要 A rotor blade comprises an inner rotor blade root area, a rotor blade main area disposed adjacent to the inner rotor blade root area along a length of the rotor blade and having an aerodynamically effective rotor blade profile, the profile including a nose area and a rear edge area, and a rotor blade tip disposed adjacent to the rotor blade main area along the length of the rotor blade. The rotor blade tip is configured to be deformable relative to the rotor blade main area and is operatively connected to a first actuator device. The first actuator device is configured to initiate a vertical movement of the rotor blade tip upwards or downwards relative to the lift direction. The vertical movement starts from a neutral position relative to the rotor blade main area.
申请公布号 US8152465(B2) 申请公布日期 2012.04.10
申请号 US20080339679 申请日期 2008.12.19
申请人 JAENKER PETER;KLOEPPEL VALENTIN;EUROCOPTER DEUTSCHLAND GMBH 发明人 JAENKER PETER;KLOEPPEL VALENTIN
分类号 B64C9/00;B64C11/28 主分类号 B64C9/00
代理机构 代理人
主权项
地址