中国电机工程学报2024，Vol.44Issue(12)：4966-4985,中插31,21.DOI:10.13334/j.0258-8013.pcsee.222487
小型全电/混动飞机技术路线与动力系统综述
Overview of the Technical Roadmap and Powertrain System for Small All-electric or Hybrid Aircraft
摘要
Abstract
This paper analyzes and summarizes the technical development route of manned aircraft,the architecture of propulsion motors and powertrain systems.First,from the aspects of the aerodynamic layout,structural topology,power source and takeoff and landing form,six technical routes are classified.The technical indexes of passenger number,maximum takeoff weight,cruising speed,power and range are analyzed.Then,the technical parameters and application models of the installed or uninstalled aircraft propulsion motor are summarized.The development status of three-phase permanent magnet(PM)motor,multi-phase PM motor,megawatt turbine-driven motor/generator,high temperature superconducting(HTS)motor as advanced aviation propulsion motor is discussed according to the power class.Finally,the characteristics and key technologies of five kinds of the powertrain architectures are given and the future development direction of manned spacecraft is forecasted.This paper aims to serve as a reference for the overall aerodynamic layout design,power requirements,device selection and powertrain design of manned electric/hybrid spacecraft.关键词
航空电气化/电动/混动飞机/电动垂直起降/飞行汽车/电机/动力系统Key words
aviation electrification/electric/hybrid aircraft/electric vertical take-off and landing(eVTOL)/flying car/motors/powertrain system分类
动力与电气工程引用本文复制引用
陈起旭,王群京,钱喆,李国丽,曹文平,丁石川,孙泽辉..小型全电/混动飞机技术路线与动力系统综述[J].中国电机工程学报,2024,44(12):4966-4985,中插31,21.基金项目
国家自然科学基金(重点项目)(51637001) （重点项目）
国家自然科学基金区域创新联合基金重点项目(U23A20647) （U23A20647）
安徽高校自然科学研究项目(KJ2021A0014). Project Supported by National Natural Science Foundation of China(Key Project)(51637001) （KJ2021A0014）
Regional Innovation Joint Fund of the National Natural Science Foundation of China(U23A20647) （U23A20647）
Project Supported by Education Department of Anhui Province(KJ2021A0014). （KJ2021A0014）
