四轴飞行器设计阶段理论重量估算与比较

International Research Journal of Multidisciplinary Technovation Pub Date : 2022-10-05 DOI:10.54392/irjmt2261

Lijalem Gebrehiwet, S. Tilahun, Nathnael Geneti, Yeshurun Alemayehu

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引用次数: 0

摘要

根据材料的特征密度来估算材料的重量，对于分析工程初期投入的基本重量参数有很大的优势。在详细设计阶段，对每个部件进行基本尺寸设计和材料选择。选择的重量将与其他材料，如钢，铝和复合材料进行验证。将钢、铝和复合材料制造四轴飞行器的总重量与参数参考值、总部件重量进行比较，然后推荐四轴飞行器机身的最佳材料。与钢和铝框架相比，复合材料重量轻，强度高。如果我们使用这种材料，四轴飞行器将有更多的飞行时间进行喷涂。

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Quadcopter Theoretical Weight Estimation and Comparison during Design Phase

Weight estimation of materials from their characteristic density has a great advantage on analyzing the basic weight parameter put at initial stage of the project. During the detail design stage, each component is designed with basic dimensions and material selection. The selected weight will be verified with other materials such as steel, aluminum and composites. The total weight of the Quadcopter when made of steel, aluminum and composites are compared with the reference value of parameter, total component weight and then the bets material will be recommended for the Quadcopter airframe. The composite materials are found to be light and strong when compared to steel and aluminum frames. If we use this material the Quadcopter will have more flight time for spraying.

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来源期刊

International Research Journal of Multidisciplinary Technovation

CiteScore

0.50

自引率

0.00%

发文量