STRENGTH ANALYSIS OF CARGO-X UAV WING STRUCTURE USING SANDWICH COMPOSITE MATERIALS

IF 0.1 0 MUSIC
D. Hartini, B. Junaidin, Habibi Habibi
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引用次数: 0

Abstract

The Cargo-X UAV aircraft is a UAV aircraft designed to carry medicines, packages and blood bags in areas that require fast and efficient handling. One of the important components of the Cargo-X UAV aircraft is the wing, so the strength of the wing structure must be seriously considered to ensure safety during flight under unexpected conditions. The purpose of this study was to analyze the wing structure of the UAV Cargo-X aircraft made of sandwich composite material to determine the level of safety of the wing structure. The loading of the wing structure uses the load due to the lift. The wing structure modeling uses CATIA software, while the analysis uses PATRAN/NASTRAN software. From the analysis results, the skin and spar wing structures are safe against loading, while the core section is not safe against loading.
基于夹层复合材料的cargo-x无人机机翼结构强度分析
Cargo-X无人机是一种无人机飞机,设计用于在需要快速有效处理的地区运送药品、包裹和血袋。Cargo-X无人机的重要部件之一是机翼,因此必须认真考虑机翼结构的强度,以确保意外情况下的飞行安全。本研究的目的是分析由夹层复合材料制成的无人机Cargo-X飞机的机翼结构,以确定机翼结构的安全水平。机翼结构的载荷利用升力产生的载荷。机翼结构建模采用CATIA软件,分析采用PATRAN/NASTRAN软件。从分析结果来看,蒙皮和翼梁结构的抗载安全性较好,而核心部分的抗载安全性较差。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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12 weeks
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