Enhanced load management and distribution system
View Patent ↗A system for managing distribution of electrical power includes a power management circuit, power control units, a first keyline and a second keyline. The power management circuit includes a device configured to measure power consumed by an electrical load, and a comparator comparing the measured power with a power limit. Each power control unit includes an outlet for delivering power to a load; a timing control circuit coupled to each outlet and configured to deliver an enabling signal to each outlet individually with a time delay; a signal input; and a signal output. The first keyline connects the power management circuit with the signal input of one power control unit; the second keyline connects the signal output of that power control unit with the signal input of another power control unit. Each power control unit is configured to propagate a signal to another power control signal via the second keyline.
1. A system for managing distribution of electrical power, comprising:
a power management circuit including
a device configured to measure power consumed by an electrical load, and
a comparator configured to compare the measured power with a power limit;
a plurality of power control units each including
a plurality of outlets for delivering power to a load,
a timing control circuit coupled to each said outlet, the timing control circuit configured to deliver an enabling signal to each outlet individually with a time delay,
a signal input, and
a signal output;
a first keyline connecting the power management circuit with the signal input of one of said plurality of power control units; and
a second keyline connecting the signal output of said one of said plurality of power control units with the signal input of another one of said plurality of power control units,
wherein each power control unit is configured to propagate a signal to another power control unit via the second keyline;
wherein each power control unit is configured to, when receiving a SET signal, evaluate whether an outlet associated with it is requesting power, and if so, start a time delay using the timing control circuit and after the expiration of the time delay, determine whether the SET signal remains, and if so, sequentially evaluate the other outlets associated with the power control unit while the SET signal is being received.
2. The system according to claim 1 , wherein each power control unit further comprises a power input coupled to a power keyline connected to the power management circuit.
3. The system according to claim 2 , wherein each power control unit further comprises an outlet control device coupled to each said outlet and to the power keyline, for delivering power to the outlet in accordance with the outlet being enabled.
4. The system according to claim 1 , wherein
the first keyline is characterized as a first ENABLE keyline for delivering one of the SET signal and a RESET signal,
the second keyline is characterized as a second ENABLE keyline over which one of the SET signal and the RESET signal, in accordance with the signal from the first ENABLE keyline, is propagated to another power control unit.
5. The system according to claim 4 , wherein a comparison indicating the measured power exceeding the power limit causes a reset condition in which the RESET signal is delivered to the first keyline.
6. The system according to claim 5 , wherein in said reset condition, outlets without a consumer device connected thereto at initiation of the reset condition are prevented from being enabled.
7. The system according to claim 1 , wherein each outlet is configured to deliver a signal indicating a request for power in accordance with a consumer device being connected to the outlet.
8. The system according to claim 3 , wherein said power management circuit is a standalone unit.
9. The system according to claim 3 , wherein said power management circuit is integrated into an aircraft power management system.
10. The system according to claim 9 , wherein said outlets are consumer electrical outlets on an aircraft.