首页> 外国专利> CAP-BASED HEAT-MITIGATING NOSE INSERT FOR A PROJECTILE AND A PROJECTILE CONTAINING THE SAME

CAP-BASED HEAT-MITIGATING NOSE INSERT FOR A PROJECTILE AND A PROJECTILE CONTAINING THE SAME

机译:基于CAP的弹射式散热鼻插入物以及包含该弹射物的弹射物

摘要

Techniques and architecture are disclosed for a nose insert for use in a projectile. The nose insert includes a polymer nose element and a metal cap. The polymer nose element includes a rear shank portion and a tapered head portion. Disposed onto the tapered head portion of the polymer nose is the metal cap. The metal includes an outer curved portion that terminates at a forward end in a meplat. In some embodiments, the metal cap prevents deformation of the polymer nose element caused by high stagnation temperatures experienced by the projectile during flight. In some other embodiments, the metal cap includes a locking ridge. The locking ridge is disposed on an inner surface of the metal cap component and interfaces with an outer surface of the tapered head portion of the polymer nose element.
机译:公开了用于射弹的鼻插入物的技术和结构。鼻插入件包括聚合物鼻元件和金属盖。聚合物鼻元件包括后柄部分和锥形头部。金属盖设置在聚合物鼻的锥形头部上。该金属包括外部弯曲部分,该外部弯曲部分终止于金属板的前端。在一些实施例中,金属盖防止由飞行期间弹丸经历的高停滞温度引起的聚合物鼻元件的变形。在一些其他实施例中,金属盖包括锁定脊。锁定脊设置在金属盖部件的内表面上,并且与聚合物鼻元件的锥形头部的外表面接合。

著录项

  • 公开/公告号US2018245896A1

    专利类型

  • 公开/公告日2018-08-30

    原文格式PDF

  • 申请/专利权人 SIG SAUER INC.;

    申请/专利号US201815906440

  • 发明设计人 THOMAS J. BURCZYNSKI;

    申请日2018-02-27

  • 分类号F42B10/38;F42B12/78;F42B12/34;

  • 国家 US

  • 入库时间 2022-08-21 12:57:31

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