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
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