JAST  >> Vol. 4 No. 2 (June 2016)

    通用飞机油电混合动力系统设计与陆上性能仿真
    Design and Simulation Performance on Land for General Aircraft Oil-Electric Hybrid System

  • 全文下载: PDF(725KB) HTML   XML   PP.41-48   DOI: 10.12677/JAST.2016.42006  
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作者:  

毛鞠盛,王 云,宗 剑:南昌航空大学飞行器工程学院,江西 南昌

关键词:
油电动力系统MATLAB通用航空混合动力Petrol-Electric Hybrid System MATLAB General Aircraft Hybrid Power

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.

文章引用:
毛鞠盛, 王云, 宗剑. 通用飞机油电混合动力系统设计与陆上性能仿真[J]. 国际航空航天科学, 2016, 4(2): 41-48. http://dx.doi.org/10.12677/JAST.2016.42006