Power supply circuit for an ion engine sequentially operated pow

Electric power conversion systems – Current conversion – Having plural converters for single conversion

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363 41, H02M 112, H02M 114, H02M 700

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active

061543837

ABSTRACT:
A power supply circuit for an ion engine suitable for a spacecraft has a voltage bus having input line and a return line. The power supply circuit includes a pulse width modulation circuit. A plurality of bridge inverter circuits is coupled to the bus and the pulse width modulation circuit. The pulse width modulation circuit generates operating signals having a variable duty cycle. Each bridge inverter has a primary winding and a secondary winding. Each secondary winding is coupled to a rectifier bridge. Each secondary winding is coupled in series with another of the plurality of rectifier bridges.

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