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Pyrotechnic riveting for aircraft - uses explosion generated shock wave to drive rivet with relatively hard head onto anvil

机译:飞机烟火铆接-使用爆炸产生的冲击波将铆钉相对硬的头部推到砧座上

摘要

The riveting process may be used in the mfr. of aeroplane bodies, utilising a pyrotechnical explosion to drive the rivet (1). The explosion generates a shock wave which is transformed into a force wave and applied to one end of the rivet. A domed head (1a) acts as a force wave guide, the wave being passed axially through the shaft (1b) to be reflected. The material at the tip is momentarily plasticised and expanded radially (1c) to effect the connection. Anvil (4) may reflect the force wave, both head (1a) and anvil (4) being of harder material than shaft (1b), and anvil (4) being of significantly greater mass than shaft (1b). Anvil (4) and head (1a) may have a Brinell hardness of 270 and hammer (3) may fit snugly onto head (1a).
机译:铆接过程可用于制造。利用烟火爆炸来驱动铆钉(1)。爆炸产生冲击波,该冲击波转化为力波并施加到铆钉的一端。圆顶头(1a)用作力波导管,该波沿轴向通过轴(1b)进行反射。尖端处的材料会瞬间塑化并径向膨胀(1c)以实现连接。砧座(4)可能会反射力波,头部(1a)和砧座(4)的材料都比轴(1b)硬,砧座(4)的质量明显大于轴(1b)。砧座(4)和头部(a)的布氏硬度可能为270,锤子(3)可以紧贴头部(1a)。

著录项

  • 公开/公告号FR2481623B1

    专利类型

  • 公开/公告日1983-05-27

    原文格式PDF

  • 申请/专利权人 HAUTE GARONNE ETS AURIOL ET CIE;

    申请/专利号FR19800010020

  • 发明设计人

    申请日1980-04-30

  • 分类号B21J15/02;B21J15/18;

  • 国家 FR

  • 入库时间 2022-08-22 10:01:20

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