公开(公告)号：US5054320A

公开(公告)日：1991-10-08

申请号：US503123

申请日：1990-03-28

申请人： Amand Yvon

发明人： Amand Yvon

IPC分类号： G01P15/125 ,  G01P15/13

CPC分类号： G01P15/131 ,  G01P15/125 ,  G01P2015/0831

摘要： The accelerometer is suitable for use on missiles subjected to high acceltion forces on start. It comprises a base and a flat pendulum mounted on the base for oscillation about a rotation axis located in the plane of the pendulum. The distance between the center of gravity of the pendulum and the rotation axis is small as compared with the span of the pendulum. Electrodes are carried by a face of the pendulum on both sides of the axis and cooperate with electrodes carried by the base for generating an electrostatic balancing field. The pendulum has electrodes on one face only and that results in easier construction.

摘要翻译： 加速度计适用于起动时承受高加速力的导弹。 它包括安装在基座上的底座和平摆，围绕位于摆锤平面内的旋转轴线进行摆动。 与摆的跨度相比，摆锤重心与旋转轴之间的距离较小。 电极由轴的两侧的摆锤的表面承载，并与由底座承载的电极配合，以产生静电平衡场。 钟摆仅在一个面上具有电极，结果更容易构造。