An Induction Generator based AC/DC Hybrid Electric Power Generation System for Additional Electrically Powered Airliner
DOI:
https://doi.org/10.55524/Keywords:
Electric vehicles, power system, battery power, Dynamic Wireless Power TransferAbstract
For an additional aircraft power system, both AC and DC power having high voltage levels are required. with various flight loads. This paper introduces an induction generator based on AC / DC hybrid MEA power generation system. In the proposed system structure, a high-speed generator/generator and a low-speed generator are fitted with high pressure (HP) and low pressure (LP) of the spools of the engine, respectively. In production mode, all alternating AC power is generated by the HP generator while the DC power supply is supplied by both HP and LP generators. The control system is designed to control the AC power supply and direct the DC power supply between the two generators. The proposed AC / DC-based induction generator system results in reduced demand for computer hardware compared to the AC and DC production systems.
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References
for IFO induction motor," in IEEE Transactions. [2] P. J. Coussens, A. P. Van den Bossche and J. A. Melkebeek, "Magnetizing current control strategies for nonlinear indirect field-oriented control," Industry Applications Conference, 1995. Thirtieth.
M. Tarbouchi and H. Le Huy, "Control by exact linearization of an induction motor in field weakening regime," Industrial Electronics Society, 1998.
Department of Defense (United States of America) Interface Standard, Aircraft Electric Power Characteristics, MIL-STD 704F, Mar. 2004
Shi, M. Krishnamurthy, "Concept and implementation of a simplified speed control strategy for survivable induction motor drives,".