当大型的飞机另件重新设计为更加整体化的结构时,减少紧固件和节省在另件上钻孔与安装的费用是可以实现的。有严重卷边与尖锐角度的另件和通常只能用棒材或锻件机加工的小而复杂的另件也能用该工艺制造。这样就能增加材料的利用率和降低切削加工的消耗。但是,试图用常规的成形工艺来随意地利用金属的超塑性是不可能的。 When large aircraft parts are redesigned for a more integrated structure, it is achievable to reduce the number of fasteners and to save on the cost of drilling and mounting the parts. Parts with severe hemming and sharp angles, and small, intricate parts usually machined with bars or forgings, can also be made using this process. This will increase material utilization and reduce machining costs. However, it is not possible to attempt to utilize the superplasticity of metals at will by conventional forming processes.