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新能源飞机动力系统仿真研究 被引量:1

Simulation Research on Power System of New Energy Aircraft
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摘要 对锐翔新型电动飞机的动力系统进行模拟仿真及仿真结果分析。在Matlab仿真软件环境中建立新能源飞机的动力系统模型,分别对电动机、电池、传动机构单独进行模块建立并连接,利用Matlab中添加的AeroSim模块完成仿真,并对得到的数据进行分析。能更直接观察和分析各个模块运行原理与模拟仿真过程,仿真结果与实飞数据误差较小,得出搭建模块结构和相应数据计算是正确的。 This paper analyzes the simulation and simulation results of the power system of Ruixiang’s new electric aircraft.In the Matlab simulation software environment, the power system model of the new energy aircraft is established. The motor,battery and transmission mechanism modules are separately established and connected. The AeroSim module added in Matlab is used to complete the simulation and obtain specific data for analysis. It can directly observe and analyze the operating principle and simulation process of each module. The error between the simulation result and the real flight data is small,and it is concluded that the construction of the module structure and the corresponding data are correct.
作者 佟刚 赵志朋 王锋 TONG Gang;ZHAO Zhipeng;WANG Feng(Shenyang Aerospace University, Key Laboratory of General Aviation, Shenyang 110136, China;Shenyang Aerospace University, College of Electromechanical Engineering, Shenyang 110136, China;Liaoning Academy of General Aviation, Shenyang 110136, China)
出处 《机械工程师》 2019年第6期12-15,共4页 Mechanical Engineer
基金 辽宁省自然科学基金项目(2014024012)
关键词 新能源飞机 锐翔新型电动飞机 动力系统仿真 Aerosim模块 仿真结果对比 new energy aircraft Ruixiang new electric aircraft power system simulation Aerosim module simulation results comparison
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  • 1吕胜利,左曙光.并联混合动力汽车控制策略的综合分析[J].上海汽车,2005(7):26-30. 被引量:11
  • 2马晓丽,马履中,周兆忠.新型4自由度并联机构的运动学建模与分析[J].农业机械学报,2006,37(3):100-104. 被引量:22
  • 3童宝宏,桂长林,孙军,赵小勇,陈华.计入热变形影响的内燃机主轴承热流体动力润滑分析[J].机械工程学报,2007,43(6):180-185. 被引量:23
  • 4方振平.飞机飞行动力学[M].北京:北京航空航天大学出版社,2008:128-136.
  • 5Rippl M D. Sizing analysis for aircraft utilizing hy- brid-electric propulsion systems[ R]. Air force inst of tech wright-patters on AFB OH engineering and man- agement, 2011.
  • 6Hung J Y, Gonzalez L F. On parallel hybrid-electric propulsion system for unmanned aerial vehicles [ J ]. Progress in Aerospace Sciences,2012 (51 ) : 1 - 17.
  • 7Romeo G, Borello F, Correa G. ENT/CA-FC: Design, realization and flight test of all electric 2-seat aircraft powered by fuel cells [ C ]. International Congress of the Aeronautical Sciences(ICAS2010) ,2010 :1 - 3.
  • 8Batill S M, Stelmack M A, Qing Y X. Multidisciplinary design optimization of an electric-powered unmanned air vehicle [ J ]. Aircraft Design, 1999 ( 8 ) : 1 - 18.
  • 9Berton J J, Joshua F E, Timpthy W J. An analytical performance assessment of a fuel cell-powered, small electric airplane[ J ]. NASA, 2003 : 6 (2) : 210 - 215.
  • 10Xiao Li. Stability analysis and control design for hy- brid AC-DC more electric aircraft power systems [ M]. University of Pittsburgh,2013:41 -42.

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