<p>A rotary system (103, 203, 301) includes a retention member (305) and a flexible yoke (307) having an opening (309) forming a bridge (311). The rotary system is further provided with two bearing assemblies, a first bearing assembly (317) extending through the opening (309) of the yoke and configured to secure a rotor blade (303) to the retention member (305) and a second bearing assembly (319) extending through the opening (309) of the flexible yoke and configured to secure the rotor blade (303) to the bridge (311). The second bearing element includes a bearing element (521) having a first surface forming a spherical contouring and an opposing integral second surface forming a conical contouring (523).</p>
申请公布号
EP2631177(A1)
申请公布日期
2013.08.28
申请号
EP20120161903
申请日期
2012.05.03
申请人
BELL HELICOPTER TEXTRON INC.
发明人
STAMPS, FRANK B;MARSHALL, BRYAN WADE;THOMPSON, TERRY K;BRAZIEL, ORION;POPELKA, DAVID;TISDALE, PATRICK