发明名称 Laminated thrust bearing, rotor provided with such a bearing and aircraft
摘要 The abutment (10) has a stack comprising a pair of main layers (20, 30), where one of the layers presents thickness (e1) in a lead-lag plane (PTRA). The thickness varies between a minimum thickness (e1min) on pitch-variation axis (AXPAS) and a maximum thickness (e1max) on a flapping axis (AXBAT). The other layer presents, in the lead-lag plane, another thickness (e2) that varies between another minimum thickness (e2min) on the flapping axis and another maximum thickness (e2max) on the pitch-variation axis. The thicknesses are constant in a flapping plane and a pitch-angle variation plane.
申请公布号 EP2610175(A1) 申请公布日期 2013.07.03
申请号 EP20120007713 申请日期 2012.11.14
申请人 EUROCOPTER 发明人 FERRANT, MATTHIEU;LEGRAND, MATHIEU
分类号 B64C27/35;F16F1/387 主分类号 B64C27/35
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