Abstract

This paper presents the possibility of using Gallium Nitride (GaN) high-electron-mobility transistors (HEMTs) instead of the conventional silicon metal oxide semiconductor field effect transistor (MOSFET) to implement a high-frequency intermediate bus converter (IBC) as part of a typical distributed power architecture used in a space power application. The results show that processing the power at greater frequencies is possible with a reduction in mass and without impacting the system efficiency. The proposed solution was experimentally validated by the implementation of a 1 MHz zero-voltage and zero-current switching (ZVZCS) current-fed half-bridge converter with synchronous rectification compared with the same converter using silicon as the standard technology on power switches and working at 100 kHz. In conclusion, the replacement of silicon (Si) transistors by GaN HEMTs is feasible, and GaN HEMTs are promising next-generation devices in the power electronics field and can coexist with silicon semiconductors, mainly in some radiation-intensive environments, such as power space converters. The best physical properties of GaN HEMTs, such as inherent radiation hardness, low on resistance and parasitic capacitances, allow them to switch at higher frequencies with high efficiency achieving higher power density. We present an optimized design procedure to guaranty the zero-voltage switching condition that enables the power density to be increased without a penalization of the efficiency.

Highlights

  • Mass is one of the most critical parameters in aerospace applications due to the cost of launching and the need to accommodate increasing payloads

  • We propose the use of Gallium Nitride (GaN) high-electron-mobility transistors (HEMTs) in a real DC/DC converter for a space power application

  • An intermediate bus converter based on an GaN HEMTs half-bridge zero-voltage and zero-current switching (ZVZCS) resonant converter working at 1 MHz was designed and implemented

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Summary

Introduction

Mass is one of the most critical parameters in aerospace applications due to the cost of launching and the need to accommodate increasing payloads. The mass reduction of the power systems is one of the main aims of advances in aerospace technology. This mass reduction is associated with (1) an increase of the efficiency of DC/DC power conversion units, which reduces the associated thermal dissipation and permits the use of smaller solar panels and batteries, and (2) a size reduction of the reactive components of power converters (inductors, transformers, and capacitors) when switching frequency is increased. DC/DC power converters used in the aerospace field are based on hard rad Si (Silicon) metal oxide semiconductor field effect transistor (MOSFETs) as switching devices.

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