发明名称 Device for locking the blades of a turbomachine disk
摘要 <p>The blade lock (5), shaped to fix a turbine blade (13) in a disc groove (6), has a first side face (19) with a thrust surface that engages with the groove between the upper edge of a first lip (9) and the base of the groove as it is pivoted by a thrust element (3) between free and locked positions. The thrust element is in the form of a screw inserted in a threaded hole that made through the lock. The second side face (11) of the lock has a lug (15) that prevents any circumferential movement of the lock once it is in its locked position.</p>
申请公布号 EP1801355(A1) 申请公布日期 2007.06.27
申请号 EP20050292779 申请日期 2005.12.23
申请人 TECHSPACE AERO 发明人 ERNST, PHILIPPE
分类号 F04D29/34;F01D5/30 主分类号 F04D29/34
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