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
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。
Abstract:
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.
参考文献
[1]
|
康桂文, 孙振祥. 通用飞机油电混合动力系统设计与性能仿真[J]. 沈阳航空航天大学学报, 2015, 32(2): 23-27.
|
[2]
|
曹政策, 等. 混合动力电动公交车动力系统的研制[D]: [硕士学位论文]. 武汉: 武汉理工大学, 2004: 3.
|
[3]
|
朱蔡良才, 郑汝海, 种小雷, 邵斌, 王何巍. 高原机场起飞着陆滑跑距离测试与分析[J]. 空军工程大学学报(自然科学版), 2000, 1(2): 4-7.
|
[4]
|
康桂文, 胡雨, 李亚东, 等. 超轻型电动飞机电动力系统的参数匹配[J]. 航空动力学报, 2013(12): 2641-2647.
|
[5]
|
方振平. 飞机飞行动力学[M]. 北京: 北京航空航天大学出版社, 2008: 18-31.
|