摘要
本文在某型通用飞机的基础上设计了一个油电混合动力系统,并用MATLAB软件模拟验证该系统的实用性及优越性。根据运动学公式,使用MATLAB软件编程分别对原型机和该混合动力系统飞机的起飞距离、陆上行驶能量消耗、陆上行驶路程等性能进行模拟分析。结果表明,使用该动力系统的油电混合动力飞机,在上述各项性能中均优于原型机。
In this paper, a hybrid electric power system is designed on the basis of a certain type of general aircraft, and the practicability and superiority of the system are verified by MATLAB software. According to the kinematics formula, using MATLAB software programming respectively on the prototype and the hybrid system aircraft take-off distance, land travel energy consumption, land travel distance of performance is simulated and analyzed. The results show that the use of the power system of hybrid electric aircraft is better than the performance of the prototype.
出处
《国际航空航天科学》
2016年第2期41-48,共8页
Journal of Aerospace Science and Technology
基金
国家自然科学基金《水空两栖飞行器动力推进系统及其关键技术研究》资助,基金号:51266012。
