公开(公告)号：US20160131081A1

公开(公告)日：2016-05-12

申请号：US14996822

申请日：2016-01-15

申请人： AIRCELLE

发明人： Hakim MAALIOUNE ,  Alexandre DESCAMPS ,  Pierre MORADELL-CASELLAS

IPC分类号： F02K1/76

CPC分类号： F02K1/763 ,  B64D29/06 ,  F02K1/766 ,  F05D2260/57 ,  F16H25/2454

摘要： The present disclosure provides an electric thrust reverser system for an aircraft engine nacelle, including a mechanism for actuating a thrust reverser mechanism. The actuating mechanism includes a first drive cylinder and a second drive cylinder. Each cylinder includes a mechanical connection casing, a primary lock (8) and a movable rod secured to a point connected to the associated thrust reverser mechanism. A motor-actuated drive unit is mechanically connected, via flexible shafts, to the mechanical connection casings of each drive cylinder and set in motion by the command of a control unit via an electrical connection. A tertiary lock is disposed for securing the associated thrust reverser mechanism, to a fixed structure of the nacelle.

摘要翻译： 本公开提供了一种用于飞机发动机机舱的电推力反向器系统，其包括用于致动推力反向器机构的机构。 致动机构包括第一驱动气缸和第二驱动气缸。 每个气缸包括机械连接壳体，主锁（8）和固定到连接到相关联的推力反向器机构的点的可动杆。 电机驱动的驱动单元通过柔性轴机械地连接到每个驱动气缸的机械连接壳体，并且通过电连接通过控制单元的命令而设置运动。 三级锁被设置用于将相关联的推力反向器机构固定到机舱的固定结构。