<p>A yoke for a rotary wing aircraft rotor system has a plurality of arms, each arm having a root. Each root has a notched portion configured to allow passage of a portion of a blade-pitch control system through the notched portion.</p>
申请公布号
MX2008014460(A)
申请公布日期
2009.04.30
申请号
MX20080014460
申请日期
2007.05.14
申请人
TEXTRON INNOVATIONS INC.
发明人
STAMPS, FRANK B.;RAUBER, RICHARD E.;TISDALE, PATRICK R.;CAMPBELL, THOMAS C.;DONOVAN, TOM;BRASWELL, JAMES LEE, JR.
