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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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