发明名称 Pinion shaft flange for power transmission in helicopter, has rigid body with cylindrical axial passage to receive conical rings, which are radially deformable to clamp shaft end to flange during axial movement of rings
摘要 <p>The flange has a rigid body (7) with a cylindrical axial passage to coaxially receive conical rings (8, 9) and to define an annular space (10) between the passage inner surface and an external surface of any ring. An end (2A) of a hollow power transmission shaft is engaged at the space. The rings are radially deformable to clamp the shaft end to the flange by tightening the shaft end during the axial movement of the rings.</p>
申请公布号 FR2852369(A1) 申请公布日期 2004.09.17
申请号 FR20030003102 申请日期 2003.03.13
申请人 EUROCOPTER 发明人 MERMOZ EMMANUEL
分类号 F16D1/09;F16D1/091;(IPC1-7):F16D1/05;B64C27/14 主分类号 F16D1/09
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