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 WO2010134923(A1) 申请公布日期 2010.11.25
申请号 WO2009US44955 申请日期 2009.05.22
申请人 BELL HELICOPTER TEXTRON INC.;BRUNKEN, JOHN, E. 发明人 BRUNKEN, JOHN, E.
分类号 B64C27/00 主分类号 B64C27/00
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