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Redundant aircraft braking system architecture

  • US 6,390,571 B1
  • Filed: 06/29/2000
  • Issued: 05/21/2002
  • Est. Priority Date: 06/29/2000
  • Status: Expired due to Term
First Claim
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1. A redundant brake control and anti-skid system for providing braking to a vehicle, comprising:

  • a primary brake control assembly comprising a primary wheel control circuit for performing brake control and anti-skid functions and outputting electrical control signals relating thereto, and a primary interface control circuit for interfacing with the vehicle and providing emergency shutoff function;

    a secondary brake control assembly separate from the primary brake control assembly and comprising a secondary wheel control circuit for performing brake control and anti-skid functions and outputting electrical control signals relating thereto, and a secondary interface control circuit for interfacing with the vehicle and providing emergency shutoff function;

    a bus for enabling electrical communications between the primary brake control assembly and the secondary brake control assembly; and

    at least one brake actuator controlled by the electrical control signals from the primary brake control assembly and at least one other brake actuator controlled by the electrical control signals from the secondary brake control assembly for providing braking force to wheels of the vehicle.

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