Reduced power mode for an aircraft electric brake system

Reduced power mode for an aircraft electric brake system

  • CN 101,568,458 A
  • Filed: 12/20/2007
  • Published: 10/28/2009
  • Est. Priority Date: 12/21/2006
  • Status: Active Application
First Claim
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1. method of operating full electric brake system with different power consumption modes, described method comprises:

  • Operate described full electric brake system with full-power mode, described full-power mode is corresponding to first maximum brake performance capability;

    Detect the condition of the depowering pattern that triggers described full electric brake system;

    Switch to described depowering pattern from described full-power mode;

    WithIn described depowering pattern, operate described full electric brake system with low-power mode, described low-power mode is corresponding to second maximum brake performance capability lower than described first maximum brake performance capability.

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