Multi-resolution Modeling In Application Of Power Supply System Compatibility On More Electric Aircraft
- 10.2991/icsmim-15.2016.76How to use a DOI?
- multi-resolution modeling, power system compatibility, more electric aircraft
In order of saving energy and improving the performance of the airborne systems, modern aircraft increasingly uses electrical energy to replace the current hydraulic, pneumatic energy on the plane. The goal of more electric aircraft is that electric drive equipments replace mechanical, hydraulic and pneumatic equipments directly driven by the original engine to obtain high performance and high efficiency. The increase of electrical loads leads to cause power supply system compatibility problems. The concerned issue is power interference by power electronic loads, including electric actuator which is the most typical interference load. The common research method of solving power system compatibility is integrated simulation and analysis which include power, cables, electric equipments. Due to diversity of system compatibility issues, it is difficult to realize the large-scale integrated simulation. This paper applies multi-resolution modeling in power supply system compatibility simulation, and describes conductive electromagnetic interference, power stability interference and disturbance of dynamic load power which is electric actuator as typical electrical equipment.
- © 2016, the Authors. Published by Atlantis Press.
- Open Access
- This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).
Cite this article
TY - CONF AU - Lirong Sun AU - Zheng Cao AU - Liang Liu AU - Yuanjun Zhou PY - 2016/01 DA - 2016/01 TI - Multi-resolution Modeling In Application Of Power Supply System Compatibility On More Electric Aircraft BT - Proceedings of the 2015 4th International Conference on Sensors, Measurement and Intelligent Materials PB - Atlantis Press SP - 402 EP - 409 SN - 2352-538X UR - https://doi.org/10.2991/icsmim-15.2016.76 DO - 10.2991/icsmim-15.2016.76 ID - Sun2016/01 ER -