发明名称 Compact rotorcraft dual-element spherical elastomeric centrifugal-force bearing assembly
摘要 <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
分类号 B64C27/35 主分类号 B64C27/35
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