发明授权
US08926281B2 Compact rotorcraft dual-element spherical elastomeric centrifugal-force bearing assembly 有权
紧凑型旋翼飞机双元件球形弹性离心力轴承总成

Compact rotorcraft dual-element spherical elastomeric centrifugal-force bearing assembly
摘要:
A rotary system includes a retention member and a flexible yoke having an opening forming a bridge. The rotary system is further provided with two bearing assemblies, a first bearing assembly extending through the opening of the yoke and configured to secure a rotor blade to the retention member and a second bearing assembly extending through the opening of the flexible yoke and configured to secure the rotor blade to the bridge. The second bearing element includes a bearing element having a first surface forming a spherical contouring and an opposing integral second surface forming a conical contouring.
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