Abstract

This paper presents an overview of technology related to on-board microgrids for the more electric aircraft. All aircraft use an isolated system, where security of supply and power density represents the main requirements. Different distribution systems (ac and dc) and voltage levels coexist, and power converters have the central role in connecting them with high reliability and high power density. Ensuring the safety of supply with a limited redundancy is one of the targets of the system design since it allows increasing the power density. This main challenge is often tackled with proper load management and advanced control strategies, as highlighted in this paper.

Highlights

  • In the recent years, research has focused in assisting the progressive increase in transportation electrification

  • The gradual substitution of hydraulic and pneumatic subsystem with their electric counterparts on conventional aircraft is already a market reality. This framework takes the name of More Electric Aircraft (MEA), but the propulsion remains completely traditional, in a MEA only the subsystems are electrified [2]

  • Considering that power electronics converters interface most of the loads, the interactions between the control system makes the stability of the microgrid a challenging task, because the voltage and frequency stability cannot be aided by the presence of large synchronous generator like the traditional grid [4]

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Summary

INTRODUCTION

Research has focused in assisting the progressive increase in transportation electrification. The gradual substitution of hydraulic and pneumatic subsystem with their electric counterparts on conventional aircraft is already a market reality. About 2-3% of the maximum power output is through a bleed valve in the jet engine that is used to draw high pressure air for the environmental control system. This system has proved to be effective for many years, the problems of this architecture are: I. In order to obtain the maximum efficiency, engineers have been studying alternatives to the bleed valve and to the hydraulic distribution, looking at the electric and electronic realms.

ON-BOARD MICROGRIDS IN THE MORE ELECTRIC AIRCRAFT
POWER SYSTEMS ON BOARD
Energy generation in MEA EPS
MEA ELECTRICAL POWER SYSTEM ARCHITECTURES
POWER CONVERTERS FOR ON-BOARD MICROGRIDS
AC Power Converter Topologies
DC Power Converter topologies
CONTROL SYSTEM AND RELIABILITY ASPECTS
PROTECTION SCHEMES IN THE MEA
Electrical safety and protection schemes
Power quality to sensitive loads
Findings
VIII. CONCLUSION
Full Text
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