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垂直起降固定翼无人机技术发展及趋势分析
引用本文:王科雷,周洲,马悦文,杜万闪,郭佳豪,李旭,张阳,孙蓬勃.垂直起降固定翼无人机技术发展及趋势分析[J].航空工程进展,2022,13(5):1-13.
作者姓名:王科雷  周洲  马悦文  杜万闪  郭佳豪  李旭  张阳  孙蓬勃
作者单位:西北工业大学,西北工业大学 航空学院,西北工业大学 航空学院,西北工业大学 航空学院,西北工业大学 航空学院,西北工业大学 航空学院,西北工业大学 航空学院,西北工业大学 航空学院
摘    要:垂直起降固定翼无人机具有对起降场地要求低、机动性好、巡航速度高、航时长等优势,是目前航空领域研究热点。本文阐述了国内外现有垂直起降固定翼无人机研究现状和基本特征,详细分析了不同类型垂直起降固定翼无人机的技术特点,提出更高的飞行速度、更长的续航时间、更强的任务载荷能力将是未来垂直起降固定翼无人机技术的主要发展方向和必然趋...

关 键 词:垂直起降固定翼无人机  发展现状  倾转旋翼式  尾座式  分布式电推进
收稿时间:2021/9/3 0:00:00
修稿时间:2021/11/3 0:00:00

Development and Trend Analysis of VTOL Fixed Wing UAV
WANG Kelei,ZHOU Zhou,MA Yuewen,DU Wanshan,GUO Jiahao,LI Xu,ZHANG Yang and SUN Pengbo.Development and Trend Analysis of VTOL Fixed Wing UAV[J].Advances in Aeronautical Science and Engineering,2022,13(5):1-13.
Authors:WANG Kelei  ZHOU Zhou  MA Yuewen  DU Wanshan  GUO Jiahao  LI Xu  ZHANG Yang and SUN Pengbo
Institution:Northwestern Polytechnical University,,,,,,,
Abstract:The vertical takeoff and landing (VTOL) fixed wing unmanned aerial vehicle (UAV) has many advantages, such as low requirements for takeoff and landing site, good maneuverability, high cruise speed and long endurance, etc., which is a hot topic in the aviation field. This paper describes the existing VTOL fixed wing UAV development status and their features around the world, and then analyzes the technical problems faced by these different types of VTOL fixed wing UAVs. It indicates that the VTOL fixed wing UAV with higher cruise speed, longer battery life, and stronger ability of task load seems to be the main developing direction and inevitable trend in the future. Although the tilting rotor configuration and tailstock configuration are still the mainstream configuration of the VTOL fixed wing UAV in nowadays, the distributed electric propulsion (DEP) VTOL fixed wing UAV technology will become the hottest issues in the field of aerospace, therefore, it is necessary to enhance the evolutionary research in the new-concept configurations and new principles of the high-performance VTOL fixed wing UAVs.
Keywords:VTOL fixed wing UAV  development status  tilting rotor configuration  tail seat configuration  distributed electric propulsion  
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