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Redesign of an experimental Unmanned Aerial Vehicle (UAV) for its conversion into an operational laboratory platform

机译:重新设计实验无人驾驶飞行器(UAV),转换为运营实验室平台

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摘要

Following its maiden flight in 2016, the VANT SOLvendus of the Fundacion Universitaria Los Libertadores underwent the first iteration of design improvements. Various shortcomings of the design had been observed, including lack of torsional rigidity of the twin booms, limited transportability and maintainability. Furthermore, the damage incurred from just one flight demonstrated that attrition to the primary and secondary structure would make it difficult (if not impossible) to continue operating the platform for more than a handful of flights before a major overhaul would be necessary. Plans were therefore made to improve its design in preparation for its conversion into an operational laboratory platform. A tubular cross section was proposed as the replacement for the I-beams currently used for the twin boom structure and conceptual designs were developed for the implementation of this tubular structure into the current overall design. This article presents the technical analysis performed with regards to the rigidity of the new structure and its suitability in the design whilst also detailing the conceptual designs of the supporting structural components.
机译:在2016年的少女航班之后,Fundacion Universitaria Los Libertadores的Vant Solvendus经历了第一次迭代设计改进。已经观察到设计的各种缺点,包括缺乏双臂动臂的扭转刚度,可运输性有限和可维护性。此外,只有一班航班所产生的损失证明了主要和二级结构的磨损将使困难(如果不是不可能的)继续经营平台,以便在主要的大修之前进行多次飞行。因此,计划改进其设计,以准备转换为运营实验室平台。提出了一种管状横截面作为当前用于双臂结构的I-梁的替换,并且开发了概念设计,用于实现该管状结构进入当前的整体设计。本文介绍了对新结构刚性的技术分析及其在设计中的适用性,同时还详细说明了支撑结构部件的概念设计。

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