Method of simultaneously forming rocket thrust chamber cooling tubes
    1.
    发明授权
    Method of simultaneously forming rocket thrust chamber cooling tubes 失效
    同时形成火箭推进室冷却管的方法

    公开(公告)号:US5477613A

    公开(公告)日:1995-12-26

    申请号:US213306

    申请日:1994-03-14

    IPC分类号: B23P15/00 F02K9/64

    摘要: A plurality of tubes are placed side-by-side on the forming surface of a die, another die is brought into contact with the tubes, thus sandwiching the tubes therebetween. The two dies are then placed into a press that forces the dies together, simultaneously deforming the tubes into intimate contact with each other, thereby producing an exacting fit between adjacent tubes.

    摘要翻译: 将多个管并排放置在模具的成形表面上,使另一个管芯与管接触,从而将管夹在其间。 然后将两个模具放置在压力机中,该压力机将模具压在一起,同时使管彼此变形成紧密接触,从而在相邻的管之间产生严格的配合。