Reconstruction of Aircraft Electrical Power DistributionSystem Using Solid State Fault Current Limiter
محل انتشار: دومین کنفرانس ملی اویونیک ایران
سال انتشار: 1393
نوع سند: مقاله کنفرانسی
زبان: انگلیسی
مشاهده: 865
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شناسه ملی سند علمی:
ICADI02_001
تاریخ نمایه سازی: 11 اردیبهشت 1394
چکیده مقاله:
Recently, More Electric Aircrafts (MEAs) needadvanced electric power systems to answer the variety kinds ofelectrical loads through power electronic equipments.Furthermore, the power electronic converters can be used toconnect all alternative, energy storage systems, and distributedenergy sources to the aircraft electric grid. So, the protection ofsensitive loads and avionic equipments against the fault currentand switching overvoltage is an important task. This paperproposes the Solid State Fault Current Limiter (SSFCL)application in the aircraft electrical distribution system. Thisdevice is connected in series with the main bus-burs and candecrease the fault current amplitude during fault. In order toconfirm the SSFCL operation during normal and faultoperation modes, the MATLAB software is used to simulate thereconstructed electrical distribution network of the aircraftwhile the suggested SSFCL is connected in this network. Thesimulation results show the SSFCL ability to control the faultcurrent and fix the bus-bur voltage to an acceptable level. So,the sensitive loads do not experience the sever voltage drop.
کلیدواژه ها:
نویسندگان
Hamid Radmanesh
Electrical Engineering Department, Amirkabir University of technology, Tehran, Iran Institute of Space Science and Technology, Amirkabir University of technology, Tehran, Iran
Seyed Hamid Fathi
Electrical Engineering Department, Amirkabir University of technology, Tehran, Iran Institute of Space Science and Technology, Amirkabir University of technology, Tehran, Iran
G.B Gharehpetian
Electrical Engineering Department, Amirkabir University of technology, Tehran, Iran
Amin Radmanesh
Institute of Space Science and Technology, Amirkabir University of technology, Tehran, Iran