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Installation for controlling power in an aircraft

  • US 20060085100A1
  • Filed: 01/31/2005
  • Published: 04/20/2006
  • Est. Priority Date: 01/30/2004
  • Status: Active Grant
First Claim
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1. Installation for controlling power in an aircraft, comprising:

  • a power distribution network;

    at least two subscribers connected to the network, each subscriber comprising a group of loads which consume electrical power and local means for controlling the loads;

    a central power control unit which is capable of allocating a total available power level (Pdi) to each subscriber;

    means for determining the total power effectively consumed for each load; and

    for each subscriber, means for allocating power between the various loads of the subscriber in accordance with the total available power (Pdi) allocated to the subscriber, wherein the central power control unit comprises means for acquiring information which represents the total power (Pci) effectively consumed by each subscriber;

    and in that the central power control unit is capable of allocating the total available power (Pdi) to each subscriber in accordance with the total power levels (Pci) effectively consumed by the subscribers.

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