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Electromagnetic rail launcher armatures

机译:电磁轨道发射器电枢

摘要

This invention is concerned with improvements in the efficiency of Electromagnetic Rail Launcher armatures. The armature has two or more electrically conducting solid parts 10 in contact with the rails 11. Electric current flows from the rails to and from the armature between the adjacent rail and armature surfaces 14 and across the or each gap 12 by electric arcing between the conducting solid parts 10. The resulting electromagnetic forces on the armature accelerate it and any attached projectile along the rails. A member of insulating or high resistivity material located forward of the armature closes the or each gap 12 to confine the electric arcing across the smallest gap spacing to minimise the arc voltage and armature resistive losses. Exhaust chambers for the confinement and/or cooling of arcing erosion products are provided at the rear of the armature. IMAGE
机译:本发明涉及电磁轨道发射器电枢效率的改进。电枢具有与轨道11接触的两个或更多个导电实心部分10。电流通过导电之间的电弧从轨道流向和来自相邻轨道和电枢表面14之间的电枢,并且通过导电间隙流过每个间隙12。固体零件10.在电枢上产生的电磁力会加速电枢和沿轨道附着的弹丸。位于电枢前面的绝缘或高电阻率材料的构件封闭该间隙或每个间隙12,以将电弧限制在最小间隙间隔内,以最小化电弧电压和电枢电阻损耗。在电枢的后部设有用于限制和/或冷却电弧腐蚀产物的排气室。 <图像>

著录项

  • 公开/公告号GB2267142A

    专利类型

  • 公开/公告日1993-11-24

    原文格式PDF

  • 申请/专利权人 TREVOR EVANS * JAMES;

    申请/专利号GB19920010965

  • 发明设计人 TREVOR EVANS * JAMES;

    申请日1992-05-22

  • 分类号F41B6/00;

  • 国家 GB

  • 入库时间 2022-08-22 04:33:23

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