Patent · US Active

Power supply unit for use with an aircraft electrical system

US7750496B2 · kind B2 · utility

4Cited by
4References
15Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMar 21, 2008
Grant dateJul 6, 2010
Priority date
Expiry dateMar 21, 2028

Classification

  • Technology area (CPC H)Electricity
  • CPC primaryH02J2310/44
  • WIPO fieldElectrical machinery, apparatus, energy
  • WIPO sectorElectrical engineering

Abstract

A power supply unit that provides uninterrupted power to an aircraft power bus during switchovers of the aircraft bus from one power source to another. The power supply unit includes circuitry to distinguish between loss of bus power due to switchovers between power sources and loss of bus power due to shutdown of the aircraft. The power supply unit includes a low voltage lockout circuit to interrupt the supply of power when the aircraft bus voltage falls below a minimum value.

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