首页> 外国专利> RING AIRFOIL GLIDER EXPENDABLE CARTRIDGE AND GLIDER LAUNCHING METHOD

RING AIRFOIL GLIDER EXPENDABLE CARTRIDGE AND GLIDER LAUNCHING METHOD

机译:环形翼面滑翔机消耗的弹药和滑翔机发射方法

摘要

My Ring Airfoil Glider Expendable Cartridge and Glider Launching Method is form launching a reduced caliber ring airfoil glider from a conventional grenade launcher barrel with preferred application for less lethal use. A caseless ammunition base contains a primer communicating with a propellant in a rupture disk sealed chamber with a vent used to create, seal and channel propelling gas into a space behind a sabot mounted on a central guide on the base, whereupon releasing the gas, the sabot aligns, seals, pushes and rotates the glider in passage down the barrel, to a point of maximum velocity, whereon, the propelling gas is vented ahead of the glider by the central passage in the sabot as it leaves the guide, whereupon, the bore decelerates the sabot by friction freeing the glider to fly down the bore centered by a turbulent boundary layer of air until it exits the muzzle.
机译:我的“环翼型滑翔机”消耗性弹药筒和滑翔机发射方法是从常规手榴弹发射器发射筒,发射口径减小的环翼型滑翔机,首选应用,以减少致命性。无壳弹药基地在引爆盘密闭室中装有与推进剂连通的引物,该引爆室带有通气孔,用于将推进气体产生,密封并引导到安装在底座中央导向装置上的木桶后面的空间中,随后释放出气体, Sabot对准,密封,推动并旋转滑翔机,使其沿着枪管向下通过,直至达到最大速度点,在此,推进气体通过Sabot的中央通道从滑翔机前方排出,此时它离开导向装置,因此,膛孔通过摩擦使滑翔器减速,从而使滑翔机自由滑行,以沿着湍流边界层空气为中心向下滑动,直到其离开枪口为止。

著录项

  • 公开/公告号US2012073465A1

    专利类型

  • 公开/公告日2012-03-29

    原文格式PDF

  • 申请/专利权人 KIMBALL R. SCARR;

    申请/专利号US201113189147

  • 发明设计人 KIMBALL R. SCARR;

    申请日2011-07-22

  • 分类号F42B12/02;F42B14/06;F42B10/00;

  • 国家 US

  • 入库时间 2022-08-21 17:31:48

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