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Anatomy of a V-bomber

机译:V型轰炸机的解剖

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The victor's wing structure was based on three mainspars which carried the major loads. Sandwich panels that took internal pressure and fuel loads had supporting local spars. There were relatively few ribs, but those at the root and kinks were massive, and were joined, flange to flange, by what were termed "pipe joints". Thus the wing could be built in three portions per side, and was relatively easy to transport. The wing was essentially a "multi-load-path" component, having sandwich panels and multiple webs.
机译:胜利者的机翼结构基于承载主要载荷的三个主梁。承受内部压力和燃料负荷的夹芯板支撑了局部的稀疏。肋骨相对较少,但在根部和扭结处的肋骨很大,并通过所谓的“管接头”以法兰与法兰相连。因此,机翼每侧可以分为三个部分,并且相对易于运输。机翼本质上是一个“多载荷路径”组件,具有夹心板和多个腹板。

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    《Aeroplane 》 |2009年第7期| 82-8386| 共3页
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