Przegląd, analiza porównawcza i symulacja wybranych komponentów architektury elektroenergetycznego systemu zasilania samolotów ”konwencjonalnych” i ”more electric aircraft” (MEA)

The purpose of this paper is to review and make a comparative analysis of advanced architecture of the power supply system, both civil aircraft "conventional"` companies aviation Airbus and Boeing (A-320, B-767) and military Lockheed Martin (F-16), as well as civilian aircraft more electrical MEA (A-380 and A-350, B-787) and military (F-22 Raptor, F-35 JSF). In the context of the literature review, and made a general comparative analysis, special attention was paid to the advantages and disadvantages of each solution of the power supply system of classic and advanced aircraft in line with the trend of more electric aircraft MEA (More Electric Aircraft). Based on the above, perform a simulation of exemplary components of the power supply system architecture was made which were selected from the group of civil aircraft and military aircraft in terms of "conventional" and "More Electric Aircraft". The final part of the paper presents the main conclusions arising from the analysis and simulation of selected components of the architecture of the power supply system EPS (Electric Power System) aircraft of classic and more electric. Słowa kluczowe: MEA, symulacja, maszyny elektryczne, elektroenergetyczne systemy zasilania

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