发明名称 |
Configuration of a turbomachine rotor blade |
摘要 |
<p>The device has a blade that is provided with a base (30). An axial locking unit of the base engages and retains the base radially in a cavity (31). The axis of blade (24) is inclined with respect to a line perpendicular to the axis of rotation of a rotor. The axis is inclined to partially compensate the displacement of the axis caused by mechanical and thermal constraints applied to the rotor during operation of a turbomachine.</p> |
申请公布号 |
EP1524406(A1) |
申请公布日期 |
2005.04.20 |
申请号 |
EP20040292380 |
申请日期 |
2004.10.06 |
申请人 |
SNECMA |
发明人 |
RODRIGUES, PAUL;SOUPIZON, JEAN-LUC |
分类号 |
F01D5/14;F01D5/30;(IPC1-7):F01D5/14 |
主分类号 |
F01D5/14 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|