Architecture and a multiple function power converter for aircraft

A method and apparatuses are implemented for electric power systems. An apparatus for power conversion according to one embodiment comprises: a multiple function power converter, the multiple function power converter being capable of performing functions of a static inverter, and being capable of at least one of performing functions of a motor controller, and performing functions of a start converter to use a generator as a starter. An architecture system for aircraft according to another embodiment comprises: one or more rectifiers, wherein the one or more rectifiers receive at least one high frequency AC power input; and a plurality of power conversion devices optionally connectable to drive at least one high frequency generator as a starter and at least one load, the input of each power conversion device being connected to at least one rectifier.