发明名称 ROTOR BLADE SPACING FOR VIBRATION ATTENUATION
摘要 <p>A rotor system for a rotorcraft, the rotor system is a rotor hub having six rotor blades attached to a rotor mast via a rotor yoke assembly. Each rotor blade is angularly spaced in 30 ° and 90 ° alternating angular increment about a mast axis of rotation. Such rotor blades spacing reduces the vibration that is translated into the rotorcraft through the rotor mast.</p>
申请公布号 CA2762246(C) 申请公布日期 2015.07.21
申请号 CA20092762246 申请日期 2009.05.22
申请人 BELL HELICOPTER TEXTRON INC. 发明人 BRUNKEN, JOHN E., JR.
分类号 B64C27/51;B64C27/10;B64C29/00 主分类号 B64C27/51
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