The Boeing Company
Bus transfer for a flight test system

Abstract:

A power conditioning unit includes unit a rectifier having an input terminal coupled to a power transfer unit output terminal and a regulator having an input terminal coupled to an output terminal of the rectifier. The power conditioning unit also includes an energy buffer coupled to an output terminal of the regulator. The power conditioning unit includes an inverter having an input terminal coupled to the energy buffer and having an output terminal configured to couple to a load.