Starter/generator aero power system which is composed of induction machine and power electronic converter is significant.

In this paper, the author regarding the EMC testing of some airplane AC power supply system as the example, introduces the EMC test measurement and process of the aircraft power supply products, and analyzing of results and EMI control measures, bring upped the suggestion of solution for these problems.

Monolithic integrated circuit(IC)of the aircraft power supply product can help to design more effective,better-reliability,but electromagnetic interference(EMI)problem of the aircraft power supply product become more complicate than before and the potential damage to other device goes high risk.

In this paper,the author regarding the conducted emission (CE) detecting of some aircraft power supply product s power line as the example,introduces CB test measurement and process of the aircraft power supply product,and analyzed of results and EMI control measures.

A system used for on-line measurement and fault diagnosis of aircraft power supply system is designed.

A novel high frequency combined converter topology with low voltage and high current of input-end and high voltage of output-end is presented to meet the demands of high reliability and high power density in the aeronautical power supply applications.

A novel combined converter topology is present in this paper to meet the demands of high reliability and high power density in the application of aeronautical power supply.

The power matching calculation and model selection analysis on the aircraft power truck;