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ELECTRICAL DISTRIBUTION SYSTEM FOR AN AIRCRAFT

  • US 20160048186A1
  • Filed: 08/14/2015
  • Published: 02/18/2016
  • Est. Priority Date: 08/14/2014
  • Status: Active Grant
First Claim
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1. Electrical distribution system for an aircraft comprising at least one electrical supply path comprising at least one power unit capable of opening or closing the connection between at least one electrical energy source and at least one device of the aircraft, characterized in that it comprisesprotection cards (2b, 2n) each comprising at least two microcontrollers each capable of sending a command to each power unit of the electrical supply paths protected by each protection card, andamong the set of microcontrollers of the protection cards, at least two microcontrollers are provided with a communication and computation function with all of the microcontrollers of the protection cards (2b, 2n).

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