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Integrally reinforced composite sandwich joint and process for making the same

机译:整体增强复合材料夹芯接头及其制造方法

摘要

The present invention generally relates to a multi-layered structure which for a given external geometry a section of interest may be integrally reinforced by varying the relative proportions of the layers in that section. That is, the layers making up the structure may have varying relative proportions to the structure's overall thickness between two or more positions while the structure maintains a constant thickness between the positions. By varying the relative proportions of the structure's layers, the mechanical properties of the structure may be selectively altered from a first position to a second position without altering the structure's external profile. This is especially desirable in composite sandwich structures used in aerospace applications which often require additional reinforcement at structural interfaces. By adjusting the relative proportions of the composite sandwich structure's layers, one or more structurally enhanced sections may be created for structural interfaces without altering the structure's profile.
机译:本发明总体上涉及一种多层结构,该多层结构对于给定的外部几何形状,可以通过改变在该部分中各层的相对比例来整体地增强感兴趣的部分。即,构成该结构的各层在两个或多个位置之间可具有相对于该结构的整体厚度的变化的相对比例,而该结构在这些位置之间保持恒定的厚度。通过改变结构层的相对比例,可以在不改变结构的外部轮廓的情况下从第一位置到第二位置选择性地改变结构的机械性能。在航空航天应用中使用的复合夹层结构中,这通常是需要的,这些结构通常需要在结构界面处进行额外的加固。通过调整复合夹层结构各层的相对比例,可以在不改变结构轮廓的情况下为结构界面创建一个或多个结构增强型截面。

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