Installation for controlling power in an aircraft
AssigneePrecilec
InventorsThierry Marin-Martinod, Jean-Claude Robert
Life of this patent
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Abstract
The installation (10) for controlling power in an aircraft comprises a power distribution network (22); at least two subscribers (14A, 14B, 14C) connected to the network (22); a central power control unit (20) which is capable of allocating a total available power level to each subscriber; and a device for determining the total power effectively consumed for each load of the subscribers. The central power control unit (20) acquires information which represents the total power effectively consumed by each subscriber and is capable of allocating the total available power to each subscriber in accordance with the total power levels effectively consumed by the subscribers.
Claims9
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 allocates 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 allocates the total available power (Pdi) to each subscriber in accordance with the total power levels (Pci) effectively consumed by the subscribers.
Dependencies are inferred from the claim text.