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首页> 外文期刊>Journal of Materials Engineering and Performance >Advances in Fabricating Superplastically Formed and Diffusion Bonded Components for Aerospace Structures
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Advances in Fabricating Superplastically Formed and Diffusion Bonded Components for Aerospace Structures

机译:航空航天结构超塑性成形和扩散粘结零件的制备进展

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摘要

Superplastic forming and diffusion bonding (SPF/DB) production hardware is being fabricated today for aerospace applications. Metal tooling is being used to bring the titanium sheets into contact so diffusion bonding can occur. However, due to material sheet and tooling tolerances, good bond quality is difficult to achieve over large areas. A better method for achieving DB is to use "stop-off inside sealed sheets of titanium, which constitutes a pack, and then the pack is bonded using external gas pressure. A good method for heating the pack for this process is to use induction heating. Components using "stop-off that were diffusion bonded first and then superplastically formed have shown much better bond quality than components that were produced using matched metal tooling. This type of tooling has been successful at bonding small areas as long as the exerted pressure is concentrated on the area where bonding is required. Finite element modeling is providing weight effect solutions for titanium SPF/DB aerospace structures.
机译:今天,正在为航空航天应用制造超塑性成形和扩散粘结(SPF / DB)生产硬件。使用金属工具使钛板接触,从而可能发生扩散结合。但是,由于材料薄板和工具的公差,很难在大面积上获得良好的粘结质量。达到DB的更好方法是使用“封闭密封的钛金属片,该钛构成包装,然后使用外部气压将包装粘合。在此过程中加热包装的好方法是使用感应加热使用“挡块”的零件首先进行扩散粘结,然后进行超塑性成形,其粘结质量比使用匹配金属模具生产的组件要好得多。只要施加的压力集中在需要粘合的区域,这种工具就可以成功粘合小区域。有限元建模为钛SPF / DB航空航天结构提供了重量效应解决方案。

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