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Reinforced composites formed using induction thermoplastic welding

机译:使用感应热塑性焊接形成的增强复合材料

摘要

We form welded reinforced composites by heating a susceptor along the bond line with a time-varying magnetic field produced with a moving induction coil. To obtain more uniform heating across the susceptor when welding composite parts using induction heating, edge regions of lower absolute impedance or a lower longitudinal impedance than the transverse impedance counterbalance the higher current density and current that occurs near the edges. The susceptor has lower impedance at the edges by altering the aspect ratio (length/width) of openings in the susceptor, by folding the susceptor over onto itself, or both. Uniform heating is important to obtaining a uniform, consistent weld on which aerospace designers can rely.
机译:我们通过沿键合线加热基座并利用感应线圈移动产生的随时间变化的磁场来形成焊接的增强复合材料。为了在使用感应加热焊接复合零件时在基座上获得更均匀的加热,比横向阻抗更低的绝对阻抗或纵向阻抗更低的边缘区域可以抵消较高的电流密度和在边缘附近产生的电流。通过改变基座上的开口的纵横比(长度/宽度),将基座折叠到其自身上或两者,基座在边缘处具有较低的阻抗。均匀加热对于获得航空航天设计师可以依靠的均匀,一致的焊缝很重要。

著录项

  • 公开/公告号US5705796A

    专利类型

  • 公开/公告日1998-01-06

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号US19960608454

  • 发明设计人 KARL A. HANSEN DECEASED;C. DAVID LUNDEN;

    申请日1996-02-28

  • 分类号H05B6/10;

  • 国家 US

  • 入库时间 2022-08-22 02:40:27

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