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原始链接: https://news.ycombinator.com/item?id=38917820
Riveting provides several advantages in this context compared to using bolts:
1. No risk of loose or improperly torqued bolts leading to potential issues.
2. Reduced weight due to elimination of bolts and nuts.
3. 由于铆接接头提供了更牢固的连接,从而提高了结构完整性(例如,在飞机在湍流条件下飞行而导致振动载荷较高的情况下),同时减少了必须在结构上打孔以容纳的孔数 bolts and washers.
These points aside, riveted joints also offer reduced cost in terms of manufacture, inspection, and replacement.
铆接的替代方案也可以使用高强度粘合剂,特别是考虑到这些接头是静态的而不是动态的(意味着它们主要承受拉伸载荷)。 Adhesives can provide equal or greater bond strength compared to that of bolts and rivets, while simultaneously reducing mass.
无论如何,切换到单一的、最好是更简单的、可以更好地处理频繁移除的解决方案似乎是提高安全标准的明智之举。
此外,由于该设计中缺少铆钉,因此可以在同一结构或零件中混合使用螺栓连接和铆接连接。 例如,飞机翼梁可能具有多个采用螺栓接头的纵梁(在主箱体部分之间垂直连接的结构构件),而靠近蒙皮的短梁可能采用铆钉。 同样,可能存在这样的情况:螺栓和铆接接头的组合可以提供设计灵活性与耐用性之间的卓越平衡。 最终,它取决于相关特定组件的位置和应用。
Those bolts being loose (and they are BIG bolts) would mean multiple people in the installation process didn’t do their jobs, and signed their life on the line saying they did.
When I did maintenance, there was someone (QA) there to witness every torqued bolt, inspect every safety wire and installed part.
There is something rotten in Boeing.
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