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Method for fin deployment using gun gas pressure

机译:使用枪气压进行鳍部署方法

摘要

A projectile and method of deploying a projectile includes a gun-launched projectile having a pressure reservoir that is fluidly connected to an ejection piston and fin deployment pistons. The fin deployment pistons are actuatable to engage deployable fins of the projectile to move the fins from a folded position to a deployed position. Gas pressure is generated by an external burning propellant to pressurize the pressure reservoir that retains the gas until a muzzle exit of the projectile. When the projectile exits the barrel, the reservoir gas expands thereby causing movement of the ejection piston. When a trailing end of the piston moves past fin deployment piston ports, the remaining reservoir gas pressure acts on the fin deployment pistons which subsequently push on the fins. The fins rotate toward the deployed position in which the fins are locked before the ejection piston is fully ejected.
机译:展开射弹的射弹和方法包括具有压力储存器的枪发射射弹,其流体连接到喷射活塞和翅片展开活塞。 翅片部署活塞可致动以接合射弹的可展开翅片以将翅片从折叠位置移动到展开位置。 通过外部燃烧推进剂产生气体压力以加压保持气体的压力储存器,直到射弹的枪口出口。 当射弹离开桶时,储液气体膨胀,从而导致喷射活塞的移动。 当活塞的后端移动过去的鳍片部署活塞端口时,剩余的储层气体压力作用在翅片展开活塞上,其随后推动翅片。 翅片朝向展开位置旋转,在喷射活塞完全弹出之前剥落的翅片被锁定。

著录项

  • 公开/公告号US11187506B1

    专利类型

  • 公开/公告日2021-11-30

    原文格式PDF

  • 申请/专利权人 RAYTHEON COMPANY;

    申请/专利号US202016939865

  • 发明设计人 PAUL A. MEREMS;

    申请日2020-07-27

  • 分类号F42B10/20;

  • 国家 US

  • 入库时间 2022-08-24 22:15:44

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