Patent · US Active

Power rectifier circuit and systems, associated method, and aircraft comprising such a circuit or systems

US8467206B2 · kind B2 · utility

2Cited by
7References
15Claims
0Family size

Assignees

Inventors

Key dates

Filing dateJan 21, 2009
Grant dateJun 18, 2013
Priority date
Expiry dateSep 27, 2029

Classification

  • Technology area (CPC H)Electricity
  • CPC primaryH02M7/10
  • WIPO fieldElectrical machinery, apparatus, energy
  • WIPO sectorElectrical engineering

Abstract

A power rectifying circuit for an electric current signal supplied by an alternating power source, which includes: two separate switching assemblies adapted to be connected to a power terminal of the source, wherein at least one switching assembly includes a plurality of boost cells in cascade, each boost cell including a diode, a switch mechanism and a capacitor, the capacitors of the two terminal boost cells of the switching assemblies having one terminal in common. The circuit may include two assemblies of boost cells, and can be used in electric systems onboard aircrafts.

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