公开(公告)号：US20140061389A1

公开(公告)日：2014-03-06

申请号：US14042471

申请日：2013-09-30

申请人： SAGEM DEFENSE SECURITE

发明人： Hafid ELABELLAOUI ,  Jean-Eric BESOLD ,  Sebastien PAUTARD ,  Thierry CARTRY ,  David ENGLER ,  Etienne MERLET

IPC分类号： B64D31/04

CPC分类号： B64D31/04

摘要： An aeroengine control device including a mount and having pivotally mounted thereon a code wheel together with a main lever and a secondary lever, both for turning the code wheel. Each lever is movable between a rest position and a maximum actuation position. The secondary lever is mounted to pivot on the main lever. Cam paths are mounted on the code wheel and on the mount in such a manner that the main lever can move the code wheel when the main lever is moved while the secondary lever is in the rest position. The secondary lever can move the code wheel when the secondary lever is moved while the main lever is in the rest position, with movement of either lever being prevented when the other lever is clearly away from its rest position.

摘要翻译： 一种航空发动机控制装置，包括安装件，并且与主杠杆和副杠杆一起枢转地安装有代码轮，两者用于转动代码轮。 每个杠杆可在静止位置和最大致动位置之间移动。 辅助杠杆安装成在主杠杆上枢转。 凸轮路径以这样的方式安装在代码轮和安装座上，使得当主杆处于静止位置时主杆能够移动代码轮。 当主杆处于静止位置时，辅助杆可以移动代码轮，同时当另一个杆明显远离其静止位置时，两个杆的移动被阻止。

公开(公告)号：US20160308422A1

公开(公告)日：2016-10-20

申请号：US15101105

申请日：2014-09-19

申请人： SAGEM DEFENSE SECURITE

发明人： Severi VIENNOT ,  Thierry CARTRY ,  Mickael WERQUIN ,  Louis CHAVIGNIER

IPC分类号： H02K7/14 ,  H02K7/108 ,  H02K7/116

CPC分类号： H02K7/145 ,  B64C13/42 ,  B64C13/44 ,  B64C13/50 ,  H02K5/225 ,  H02K7/00 ,  H02K7/10 ,  H02K7/108 ,  H02K7/116 ,  H02K7/14 ,  H02K2213/06 ,  H02K2213/09

摘要： An actuator including a frame, an electric motor fastened to the frame and to a rotor that is constrained to rotate with an outlet shaft, and a connector electrically connected to the motor and secured to the frame to be connected to a complementary connector. The actuator includes a secondary drive device having a secondary shaft having a first end that extends outside the frame and is arranged to be coupled to rotate with a rotary drive tool, a second end of the secondary shaft in rotation coupled with the outlet shaft, and an activation rod opening out into the connector is secured to the frame and arranged to prevent the secondary shaft from being coupled in rotation with the outlet shaft only when the complementary connector is connected to the connector secured to the frame.

摘要翻译： 一种致动器，包括框架，紧固到框架的电动机和被限制为与出口轴一起旋转的转子，以及电连接到电动机并固定到框架以连接到互补连接器的连接器。 所述致动器包括辅助驱动装置，所述辅助驱动装置具有副轴，所述副轴具有延伸到所述框架外部的第一端，并且被布置成与旋转驱动工具连接以旋转，所述次级轴的第二端与所述出口轴一起旋转，以及 打开到连接器中的激活杆被固定到框架并被布置成仅当辅助连接器连接到固定到框架的连接器时，防止副轴与出口轴旋转联接。