Voltage regulator for direct current aircraft power bus

Details Voltage regulator for direct current aircraft power bus Voltage regulator for direct current aircraft power bus

1990-09-04

1991-10-08

Stephan, Steven L.

Electricity: single generator systems

Automatic control of generator or driving means

Plural conditions

322 23, 322 25, 322 28, H02H 706, H02P 902

Patent

active

050557653

ABSTRACT:
A voltage regulator for an aircraft d.c. power supply in which the gain of the voltage regulator varies as a function of d.c. load current and a.c. generator speed. In addition, in a preferred embodiment of the invention, low noise lead compensation is provided by a network which models the system response to changing load currents. It predicts the change in d.c. voltage which would occur in response to load current changes and provides regulator lead compensation.

REFERENCES:
patent: 3652920 (1972-03-01), South et al.
patent: 3754183 (1973-08-01), Ibamoto et al.
patent: 4634954 (1987-01-01), Kato et al.

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