Patent · US Expired

Voltage regulator for direct current aircraft power bus

US5055765A · kind A · utility

24Cited by
3References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 4, 1990
Grant dateOct 8, 1991
Priority date
Expiry dateSep 4, 2010

Classification

  • Technology area (CPC H)Electricity
  • CPC primaryH02P2101/30
  • WIPO fieldElectrical machinery, apparatus, energy
  • WIPO sectorElectrical engineering

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.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.