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首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers >Investigation, manufacture, and testing of damage-resistant airframe structures using low-cost carbon fibre composite materials and manufacturing technology
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Investigation, manufacture, and testing of damage-resistant airframe structures using low-cost carbon fibre composite materials and manufacturing technology

机译:使用低成本碳纤维复合材料和制造技术的耐损机身结构的研究,制造和测试

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摘要

A BAE systems/UK Government funded project, Flaviir, is investigating the design and manufacture of low-cost and damage-resistant carbon fibre composite airframe structure for large-scale unmanned aircraft vehicles (UAVs). The article discusses requirements and design concepts for low-cost wing structure. Techniques for manufacturing cost reduction and damage resistance enhancement are investigated through the design and test of spar to skin joints. The use of vacuum infusion processing with slotted-type joints and stitching of the detail parts by tufting were demonstrated to greatly increase the strength of spar to skin joints and to reduce the manufacturing cost. The results will be used for the design and manufacture of a large wing box demonstrator test structure, to be manufactured in 2009.
机译:BAE系统/英国政府资助的项目Flaviir正在研究设计和制造用于大型无人机的低成本且耐损坏的碳纤维复合材料机身结构。本文讨论了低成本机翼结构的要求和设计概念。通过对翼梁至皮肤关节的设计和测试,研究了降低制造成本和增强抗损伤性的技术。事实证明,使用带有缝缝型接头的真空灌注工艺以及通过簇绒缝合细部可以显着提高翼梁对皮肤接头的强度并降低制造成本。研究结果将用于设计和制造将于2009年生产的大型机翼盒演示器测试结构。

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