公开(公告)号：US20050109565A1

公开(公告)日：2005-05-26

申请号：US10796776

申请日：2004-03-09

申请人： Mihai Ralea ,  Franklin Christ

发明人： Mihai Ralea ,  Franklin Christ

IPC分类号： B60T8/32 ,  B60T13/74 ,  B64C25/44 ,  F16D55/00 ,  F16D55/36 ,  F16D65/14 ,  F16D65/18 ,  F16D65/38 ,  F16D65/56 ,  F16D66/00 ,  F16D66/02

CPC分类号： B60T8/1703 ,  B60T8/325 ,  B60T8/885 ,  B60T13/74 ,  B64C25/44 ,  F16D55/36 ,  F16D65/18 ,  F16D65/56 ,  F16D66/00 ,  F16D66/02 ,  F16D66/021 ,  F16D2055/0058 ,  F16D2055/0091 ,  F16D2065/386 ,  F16D2066/003 ,  F16D2066/005 ,  F16D2121/24 ,  F16D2125/40 ,  F16D2125/48 ,  F16D2125/52 ,  F16D2127/06

摘要： An electrically actuated aircraft brake system and method which provides for brake wear measurement, brake running clearance adjustment, ram position-based control and improved construction and operation. Brake wear and running clearance measurement are obtained by analyzing the output of position sensing circuitry. The position sensing circuitry, preferably including a LVDT position sensor, is also used to determine braking load, a brake controller including circuitry for effecting displacement of one or more reciprocating rams to load a brake disk stack by a predetermined amount based on a present displacement value of the position signal obtained from the position sensor. The position sensor preferably includes a LVDT transducer connected between the reciprocating ram and a brake housing, and the motive device preferably includes a servo motor. Also provided is an actuator housing including a guideway for each ram, the guideway and ram having the same polygonal cross-section, whereby the ram nut is guided and restrained from rotation by the guideway as it is translated by a ball screw in threaded engagement with the ram nut for selective movement into and out of forceful engagement with the brake disk stack for applying and releasing braking force on a rotatable wheel. An electric motor is drivingly connected to each ball screw by a first gear integral with the ball screw, a second gear in mesh with the first gear, and a pinion on a rotating drive shaft of the electric motor.

摘要翻译： 一种电动飞行器制动系统和方法，其提供制动磨耗测量，制动器行程间隙调节，基于位置的控制和改进的构造和操作。 通过分析位置检测电路的输出获得制动磨损和行驶间隙测量。 优选地包括LVDT位置传感器的位置感测电路也用于确定制动负载，制动控制器包括用于根据当前位移值实现一个或多个往复式游隙的位移以将制动盘叠加载预定量的电路 从位置传感器获得的位置信号。 位置传感器优选地包括连接在往复运动滑块和制动器壳体之间的LVDT换能器，并且动力装置优选地包括伺服电动机。 还提供了一种致动器壳体，其包括用于每个冲头的导轨，导轨和冲头具有相同的多边形横截面，由此当拉杆螺母被滚珠丝杠平移时，推杆螺母被导轨旋转，并与 用于选择性地移动进入和离开用于在可旋转轮上施加和释放制动力的制动盘叠层的活塞螺母。 电动机通过与滚珠丝杠一体化的第一齿轮，与第一齿轮啮合的第二齿轮和电动机的旋转驱动轴上的小齿轮驱动地连接到每个滚珠丝杠。

公开(公告)号：US20070125607A1

公开(公告)日：2007-06-07

申请号：US11533180

申请日：2006-09-19

申请人： Mihai Ralea ,  Franklin Christ

发明人： Mihai Ralea ,  Franklin Christ

IPC分类号： F16D55/08

CPC分类号： B60T8/1703 ,  B60T8/325 ,  B60T8/885 ,  B60T13/74 ,  B64C25/44 ,  F16D55/36 ,  F16D65/18 ,  F16D65/56 ,  F16D66/00 ,  F16D66/02 ,  F16D66/021 ,  F16D2055/0058 ,  F16D2055/0091 ,  F16D2065/386 ,  F16D2066/003 ,  F16D2066/005 ,  F16D2121/24 ,  F16D2125/40 ,  F16D2125/48 ,  F16D2125/52 ,  F16D2127/06

摘要： An electrically actuated aircraft brake system and method which provides for brake wear measurement, brake running clearance adjustment, ram position-based control and improved construction and operation. Brake wear and running clearance measurement are obtained by analyzing the output of position sensing circuitry. The position sensing circuitry, preferably including a LVDT position sensor, is also used to determine braking load, a brake controller including circuitry for effecting displacement of one or more reciprocating rams to load a brake disk stack by a predetermined amount based on a present displacement value of the position signal obtained from the position sensor. The position sensor preferably includes a LVDT transducer connected between the reciprocating ram and a brake housing, and the motive device preferably includes a servo motor. Also provided is an actuator housing including a guideway for each ram, the guideway and ram having the same polygonal cross-section, whereby the ram nut is guided and restrained from rotation by the guideway as it is translated by a ball screw in threaded engagement with the ram nut for selective movement into and out of forceful engagement with the brake disk stack for applying and releasing braking force on a rotatable wheel. An electric motor is drivingly connected to each ball screw by a first gear integral with the ball screw, a second gear in mesh with the first gear, and a pinion on a rotating drive shaft of the electric motor.

摘要翻译： 一种电动飞行器制动系统和方法，其提供制动磨耗测量，制动器行程间隙调节，基于位置的控制和改进的构造和操作。 通过分析位置检测电路的输出获得制动磨损和行驶间隙测量。 优选地包括LVDT位置传感器的位置感测电路也用于确定制动负载，制动控制器包括用于根据当前位移值实现一个或多个往复式游隙的位移以将制动盘叠加载预定量的电路 从位置传感器获得的位置信号。 位置传感器优选地包括连接在往复运动滑块和制动器壳体之间的LVDT换能器，并且动力装置优选地包括伺服电动机。 还提供了一种致动器壳体，其包括用于每个冲头的导轨，导轨和冲头具有相同的多边形横截面，由此当拉杆螺母被滚珠丝杠平移时，推杆螺母被导轨旋转，并与 用于选择性地移动进入和离开用于在可旋转轮上施加和释放制动力的制动盘叠层的活塞螺母。 电动机通过与滚珠丝杠一体化的第一齿轮，与第一齿轮啮合的第二齿轮和电动机的旋转驱动轴上的小齿轮驱动地连接到每个滚珠丝杠。