52kg MTOW四倾螺旋桨无人机螺旋桨旋翼系统研制论证

Deog-Kwan Kim, Seong-wook Choi, Danbi Hong, H. Kang, Youngjoong Kee, Taijoo Kim, Myeong-Gyu Lee, S. Wie, C. Yun
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摘要

小型电动无人机(uav)被广泛地介绍给公众和发达国家。200多家公司开发了各种类型的电动无人机。特别是有四个螺旋桨的多旋翼飞机,被称为四旋翼飞机,在公众中非常受欢迎,人们享受个人休闲,运动和爱好。国际市场对无人机的技术趋势要求逐渐增大载荷、提高悬停性能和提高前向飞行速度。通过世界市场需求和技术趋势,KARI对具有悬停和垂直起降(VTOL)能力的高速电动无人机(UAV)市场产生了兴趣。特别是具有侦察和观测任务的电动无人机,受到了政府、工业和军队的高度关注。为了实现这些目标和目标,KARI通过之前KARI的智能无人机、旋翼系统开发经验和倾转旋翼技术,开始开发52公斤最大起飞重量(MTOW)的四倾螺旋桨无人机(QTP无人机)。本文介绍了QTP无人机螺旋桨旋翼系统的整个研究工作。20多年来,KARI已经为旋翼飞机和无人机开发了一些旋翼系统。本文介绍了KARI QTP无人机螺旋桨旋翼系统的多学科设计和分析优化工作的进展,并利用优化工具开发了具有更好悬停和前飞性能的螺旋桨旋翼系统。为研究和开发新型螺旋桨转子系统,对螺旋桨进行了新的气动设计和结构设计,并简要介绍了这些工作。最后进行了飞行演示,验证了该系统的性能。在整个开发过程中,KARI验证并展示了基于主旋翼系统原有知识和新的优化流程的高性能QTP无人机螺旋桨旋翼系统的整个研发工作。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Demonstration of Prop-Rotor System Development for 52kg MTOW Quad-Tilt Prop UAV
Small electric drones (UAVs) were introduced to public people and developed world widely. Companies more than 200 have developed various types of electric drones. Specially the multi-copter which has four propellers, called as quad-copter, was very popular in public people that enjoy personal leisure, sport and hobby. The drone’s technical tendency of worldwide market requested to increase payload, better hover performance and high forward flight speed gradually. Through world market's requirement and technical tendency, KARI had interests in electric drone (UAV) market such as the high flight speed electric drones which have hover and vertical take-off and landing (VTOL) capabilities. In special, the electric UAV which has the reconnaissance and observation mission gives a deep attention to government people, industries and military people. For these targets and goals, KARI had launched to develop 52kg Maximum Take-off Weight (MTOW) Quad-Tilt Prop UAV (QTP UAV) through the previous KARI's smart UAV, rotor system development experience and tilt-rotor technologies. The paper describes that the whole research activity works of its prop-rotor system for QTP UAV. KARI had developed some rotor systems for rotorcraft and UAV more than 20 years. This paper introduces the development of the multidisciplinary design and analysis optimization work for developing prop-rotor system of KARI QTP UAV by using optimization tools which cover better hover and forward flight performance. To research and develop the new prop-rotor system, the new aerodynamic and structural design of propeller had been conducted and these activities were described briefly. Finally, flight demonstration was shown to verify the performance of this prop-rotor system of QTP. For these whole development period, KARI had verified and shown the whole research and development works of the prop-rotor system which as a high performance for QTP UAV founded on main rotor system's previous knowledge and new optimization process.
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