Electronic aircraft braking system with brake wear measurement, running clearance adjustment and plural electric motor- actuator ram assemblies

Abstract

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.

1 . A brake system comprising: 
 a brake disk stack;    a reciprocating ram;    a motive device operatively connected to the reciprocating ram for selectively moving the reciprocating ram into and out of forceful engagement with the brake disk stack for applying and releasing braking force on a rotatable wheel;    a controller for controlling the motive device for selective control of the reciprocating ram and regulation of the force applied by the reciprocating ram against the brake disk stack, and    a position sensor which supplies a position signal representative of the position of the reciprocating ram; and    wherein the controller includes means for effecting displacement of the reciprocating ram to load the brake disk stack by a predetermined amount based on a present displacement value of the position signal obtained from the position sensor.    
   
   
       2 . A brake system as set forth in  claim 1 , wherein the position sensor includes a LVDT transducer.  
   
   
       3 . A brake system as set forth in  claim 2 , comprising a brake housing to which said motive device is mounted, and said LVDT transducer is connected between said reciprocating ram and brake housing.  
   
   
       4 . A brake system as set forth in  claim 1 , wherein the motive device is a servo motor.  
   
   
       5 . A brake system as set forth in  claim 1 , in combination with an aircraft wheel assembly.  
   
   
       6 . A method for controlling operation of a brake system, the brake system including a motive device operatively connected to a reciprocating ram for selectively moving the reciprocating ram into and out of forceful engagement with the brake disk stack for applying and releasing braking force on a rotatable member, and a controller for controlling the motive device for selective control of the reciprocating ram and regulation of the force applied by the reciprocating ram against the brake disk stack, said method comprising the steps of: 
 using a position sensor to supply a position signal representative of the position of the reciprocating ram;    effecting displacement of the reciprocating ram to load the brake disk stack by a predetermined amount based on a present displacement value of the position signal obtained from the position sensor.    
   
   
       7 . A method as set forth in  claim 6 , wherein the step of using a position sensor includes using a LVDT transducer.  
   
   
       8 . A method as set forth in  claim 6 , wherein a torque motor is used as the motive device for selectively moving the reciprocating ram into and out of forceful engagement with the brake disk stack.