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AIRCRAFT ELECTRICAL BRAKE CONTROL SYSTEM ARCHITECTURE

  • US 20080030069A1
  • Filed: 08/04/2006
  • Published: 02/07/2008
  • Est. Priority Date: 08/04/2006
  • Status: Active Grant
First Claim
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1. An electric brake system for an aircraft having at least one left landing gear wheel and at least one right landing gear wheel, the system comprising:

  • a right brake system control unit configured to generate brake control signals for the at least one right landing gear wheel in response to pilot input;

    a left brake system control unit configured to generate brake control signals for the at least one left landing gear wheel in response to pilot input;

    at least one right electric brake actuator control coupled to and controlled by the right brake system control unit, the at least one right electric brake actuator control unit being configured to generate brake mechanism control signals for the at least one right landing gear wheel; and

    at least one left electric brake actuator control coupled to and controlled by the left brake system control unit, the at least one left electric brake actuator control unit being configured to generate brake mechanism control signals for the at least one left landing gear wheel.

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