发明名称 SIMPLIFIED SYSTEM FOR CONTROLLING THE SETTING OF A PROPELLER BLADE FOR AN AIRCRAFT TURBOSHAFT ENGINE
摘要 A system for controlling pitch of a propeller blade of a turboshank engine, including two automatic locking members making it possible, depending on their controlled position, to lock rotation of a blade root in both directions of rotation, or to allow the rotation of the blade root support in either of the two directions.
申请公布号 EP2304191(A1) 申请公布日期 2011.04.06
申请号 EP20090753872 申请日期 2009.05.26
申请人 SNECMA 发明人 GALLET, FRANCOIS
分类号 F01D7/00;F04D29/32 主分类号 F01D7/00
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