倾转旋翼无人机混合动力系统的建模与仿真研究  

Modeling and Simulation Research on Hybrid Power System for Tilt Roto UAV

作　　者：翟世杰 傅鑫[1] ZHAI Shijie;FU Xin(College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China)

机构地区：[1]南京航空航天大学能源与动力学院,江苏南京210016

出　　处：《机械制造与自动化》2023年第2期105-108,共4页Machine Building & Automation

摘　　要：为了分析油电混合动力系统的工作性能,以燃气涡轮发动机为基础,建立倾转旋翼无人机的油电混合动力系统模型。根据倾转旋翼无人机的工作特点,给出油电混合动力系统的功率配置方案,计算分析混合动力系统在倾转旋翼无人机典型飞行任务剖面下的工作性能,为后续研究倾转旋翼无人机的动力系统奠定基础。In order to analise the working performance of oil-electric hybrid system,the oil electric hybrid system model of rotary rotor UAV is established based on gas turbine engine.According to the working characteristics of tilt rotor UAV,the power configuration scheme of hybrid system is given,and the working performance of oil-electric hybrid system under the typical mission profile of tilt rotor UAV is calculated and analyzed,which lays the foundation for the reserch on the hybrid power system of tilt rotor UAV.

关 键 词：混合动力系统 燃气涡轮发动机 倾转旋翼无人机 功率分配 

分 类 号：V279[航空宇航科学与技术—飞行器设计]