Assessment of Selection of Suitable for Spar of the HumanPowered Aircraft Using COPRAS Method

Balasubramaniam Sudha, M. Ramachandran, S. Vimala, Raja Chandrasekar
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Abstract

Generally speaking, while making decisions, it is more customary to rely on intuition rather than any form of numerical technique. In areas where there are many options and many factors impacting the choice, such as the selection of materials, a more precise approach would be necessary. It is necessary to understand the material's characteristics, price, design principles, and interactions while making mechanical parts. Material science has not only produced traditional materials such as metals, ceramics, and polymers but has also given rise to various novel materials like composites, smart (intelligent) materials, and functionally graded materials. A designer now has access to a wider range of materials than ever before thanks to the growth of knowledge. In these instances, a strategic choice must be made in order to satisfy all the functional specifications of the product while upholding client requests and preferences. The performance criteria of the component must be specified, along with a general description of the properties and processing needs of the primary material, As the first stage of the material selection process. Consequently, certain material types might be ruled out, while others are chosen as potential options for the component. The relevant material properties are subsequently listed and assigned a priority ranking. The best material can then be chosen using optimization techniques. The result of the COPRAS analysis is followed by Al 2024-T4 is the first rank, Carbon 63% Epoxy is last rank. Based on the analysis, the materials ranked highest for usage are as follows: Al 2024-T4 aluminum alloy, E-glass 73%-Epoxy, E-glass 56% Epoxy, and E-glass 65% Polyester. These selections have been carefully assessed and determined to be the most suitable options, taking into account their specific properties and how well they align with the intended application. The Al 2024-T4 aluminum alloy exhibits excellent strength-to-weight ratio and corrosion resistance, making it an ideal choice for structural components. E-glass 73%-Epoxy, E-glass 56% Epoxy, and E-glass 65% Polyester offer a combination of strength, flexibility, and durability, catering to various requirements within the application. The meticulous evaluation of these materials ensures that the chosen ones will deliver optimal performance and reliability in the designated context.
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基于COPRAS方法的人力飞机翼梁优选评估
一般来说,在做决定时,更习惯地依靠直觉,而不是任何形式的数字技术。在有许多选择和许多因素影响选择的领域,例如材料的选择,需要更精确的方法。在制造机械零件时,有必要了解材料的特性、价格、设计原则和相互作用。材料科学不仅产生了传统的材料,如金属、陶瓷和聚合物,而且还产生了各种新型材料,如复合材料、智能材料和功能梯度材料。由于知识的增长,设计师现在比以往任何时候都能接触到更广泛的材料。在这些情况下,必须做出战略选择,以满足产品的所有功能规范,同时支持客户的请求和偏好。必须指定部件的性能标准,以及对主要材料的性能和加工需求的一般描述,作为材料选择过程的第一阶段。因此,某些材料类型可能会被排除在外,而其他材料类型则被选为组件的潜在选项。随后列出相关的材料属性并分配优先级。然后可以使用优化技术选择最佳材料。COPRAS分析结果依次为Al 2024-T4为第一等级,Carbon 63% Epoxy为最后等级。通过分析,使用量最高的材料依次为:Al 2024-T4铝合金、E-glass 73%-Epoxy、E-glass 56% Epoxy、E-glass 65% Polyester。这些选择经过仔细评估,并确定为最合适的选择,考虑到它们的特定属性以及它们与预期应用程序的一致程度。Al 2024-T4铝合金具有优异的强度重量比和耐腐蚀性,是结构部件的理想选择。E-glass 73%环氧树脂,E-glass 56%环氧树脂和E-glass 65%聚酯树脂提供强度,灵活性和耐用性的组合,满足应用中的各种要求。对这些材料进行细致的评估,确保所选材料在指定的环境中提供最佳的性能和可靠性。
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