| 摘要 |
A power management installation in an aircraft includes a power distribution network and at least two subscribers. Each subscriber has loads consuming electric power and local control means. The power management installation allocates, to each subscriber, a maximum total power for all the loads and evaluates, for each subscriber, the total electric power consumed. The conditions for controlling the loads of each subscriber are modified according to the controlled 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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