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Fabrication and testing of thin composite isogrid stiffened panel

机译:薄复合等强度加筋板的制作与测试

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The composite isogrid structures are feasible for use in space and civil applications where weight and damage tolerances are critical. However, isogrid stiffened structures are susceptible to failure by buckling. This paper describes the fabrication and axial compression testing of the composite isogrid stiffened panel to identify various failure modes that are present in the structures such as rib crippling, skin (pocket) buckling, and genera instability. The rib buckling was found to be the critical failure mode for the isogrid plate. The isogrid plate has been demonstrated to be tolerant to structural damage due to the multiplicity of load paths. The plate continued to resist compression loading even after one or more ribs had fractured. The small imperfections in the plate resulted in reduced buckling resistance but this problem can be overcome by advancement in the manufacturing method.
机译:这种复合等距结构在重量和破坏承受能力至关重要的空间和民用应用中是可行的。但是,等斜刚度结构容易因屈曲而失效。本文介绍了复合材料等强度加筋板的制造和轴向压缩测试,以识别结构中存在的各种破坏模式,例如肋骨瘫痪,皮肤(口袋)屈曲和类属不稳定性。肋骨屈曲被发现是等厚板的关键失效模式。由于载荷路径的多样性,等斜板已被证明可以承受结构破坏。即使在一个或多个肋破裂后,该板仍继续承受压缩载荷。板中的小缺陷导致减小的抗屈曲性,但是可以通过改进制造方法来克服该问题。

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