| 摘要 |
A power management installation in an aircraft includes a power distribution network and at least two subscribers, each subscriber having loads consuming electric power and local control means. The power management installation has means for allocating, to each subscriber, a maximum total power for all the loads; means of evaluating for each subscriber, the total electric power consumed; and means for modifying the conditions for controlling the loads of each subscriber, according to the control loads of the subscriber, the total electric power consumed by the subscriber and the maximum total power allocated to the subscriber.
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