发明名称 ANISOTROPIC ACTUATION OF A HELICOPTER ROTOR BLADE TIP
摘要 <p>The blade (10) has a leading edge (33) turned towards a direction of rotation (23) and a diverting edge (34) turned away from the direction of rotation within a rotor blade tip (12). The leading edge has an inclination at a longitudinal extending direction (21) of the blade relative to the direction of rotation within the tip. An actuator (200) e.g. D33 type piezoactuator, is arranged in a region at the diverting edge in the tip, and geometrically deforms the tip within the region of the diverting edge. The inclination of the leading edge represents a swept projection of the tip.</p>
申请公布号 EP2228299(A2) 申请公布日期 2010.09.15
申请号 EP20100155932 申请日期 2010.03.09
申请人 EADS DEUTSCHLAND GMBH 发明人 GROHMANN, BORIS;STORM, STEFAN
分类号 B64C27/46;B64C27/72 主分类号 B64C27/46
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