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NEAR SYNCHRONOUS CONTROLLED INDUCTION MOTOR DRIVE ACTUATION SYSTEM

  • US 20120018578A1
  • Filed: 07/21/2011
  • Published: 01/26/2012
  • Est. Priority Date: 07/22/2010
  • Status: Active Grant
First Claim
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1. A control system for controlling a plurality of actuators, the system comprising:

  • a plurality of actuators for actuating movement of one or more adjustable components of an aircraft, wherein each actuator has a first end coupled to a structure of the aircraft and a second end coupled to one of the one or more adjustable components and each actuator additionally includes a motion control assembly that includes a drive path from a motion provider to the one adjustable component, wherein the one or more components is configured to move along a respective drive path; and

    a controller operable to output motor drive power through a common bus to a plurality of the motion providers in a synchronous manner to actuate movement of the one or more adjustable components.

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