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首页> 外文期刊>The Aeronautical Journal >Riveted Lap Joints in Aircraft Fuselage: Design, Analysis and Properties
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Riveted Lap Joints in Aircraft Fuselage: Design, Analysis and Properties

机译：飞机机身铆接搭接接头：设计，分析和性能

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The design and construction of pressurised fuselage shells, comprising a skin joined longitudinally and/or laterally by lap joints and supported by shear tie frames and/ or stronger clip connections, typical of Boeing aircraft, is admirably presented in Chapter 1. Worthy of note is the high quality of illustrations, which zoom in on typical builds and show every detail. Under the heading loading conditions for a longitudinal lap joint the authors explain how in an unstiffened pressure vessel a tensile hoop stress, twice the longitudinal stress, is set up. Hence it is the longitudinal joint that is likely to be the more critical. The simple membrane equation is quoted, but soon usurped by a much more complex equation, developed by Flugge in 1952, which is applicable to stiffened pressurised fuselages. 'Bonded and Riveted-Bonded Lap Joints' are briefly discussed in Section 1.3.
机译：压机身机身的设计和结构，包括波音飞机典型的纵向和/或横向通过搭接接头连接，并由剪力系架和/或更牢固的夹子连接支撑的外壳，在第1章中得到了很好的说明。值得一提的是高质量的插图，可放大典型的作品并显示每个细节。作者解释了在纵向搭接的航向载荷条件下，作者解释了在未加强的压力容器中如何建立拉伸箍应力，即纵向应力的两倍。因此，纵向连接可能更重要。引用了简单的膜方程，但很快就被更复杂的方程所取代，该方程由Flugge在1952年开发，适用于加劲的加压机身。在第1.3节中简要讨论了“粘合和铆接的搭接接头”。

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