Power management installation in an aircraft

Electrical transmission or interconnection systems – Plural load circuit systems – Control of current or power

Reexamination Certificate

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Details

C307S031000, C307S032000, C307S038000, C307S029000

Reexamination Certificate

active

06921987

ABSTRACT:
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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patent: 5754445 (1998-05-01), Jouper et al.
patent: 6046513 (2000-04-01), Jouper et al.
patent: 6058288 (2000-05-01), Reed et al.
patent: 6225776 (2001-05-01), Chai
patent: 6301528 (2001-10-01), Bertram et al.
patent: 6633802 (2003-10-01), Sodoski et al.
patent: 39 36 638 (1991-03-01), None
patent: WO 98/19223 (1992-05-01), None

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