发明名称 PROP ROTOR HUB
摘要 A prop rotor hub includes a constant velocity joint in the same plane as a prop blade yoke. Torque is transmitted from a shaft to the blades through the CV joint, hub plates attached to the CV joint, and the yoke, which is attached to the hub plates. Providing all elements in a substantially planar arrangement results in a hub assembly which has significantly less height than a traditional design. The hub itself is in-plane with the yoke, resulting in a more efficient torque transmission from the mast to the rotor.
申请公布号 CA2320629(A1) 申请公布日期 2001.04.01
申请号 CA20002320629 申请日期 2000.09.26
申请人 BELL HELICOPTER TEXTRON INC. 发明人 BROEKHUIZEN, WILLEM;SCHELLHASE, ERNST C.
分类号 B64C27/48;B64C11/02;B64C27/22;B64C27/32;B64C27/473;(IPC1-7):B64C27/32 主分类号 B64C27/48
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