首页> 外国专利> CONSTRUCTION OF HYPERSONIC PROJECTILE WITH SELF-PRESSURIZING COMPRESSIVE DETONATION JET ENGINE HAVING HIGH WORKING PRESSURE AND USING HIGH EXPLOSIVE CHARGE FOR PROPULSION

CONSTRUCTION OF HYPERSONIC PROJECTILE WITH SELF-PRESSURIZING COMPRESSIVE DETONATION JET ENGINE HAVING HIGH WORKING PRESSURE AND USING HIGH EXPLOSIVE CHARGE FOR PROPULSION

机译:具有高工作压力和高爆药推进力的自加压压缩爆轰喷气发动机超音速弹药的研制

摘要

FIELD: weapons and ammunition.;SUBSTANCE: projectile comprises engine having an open-ended detonation chamber with a rear exhaust nozzle and annular exhaust windows that rise above the outer surface of said chamber at its front end face and are double-layer at the inlet and single-layer at the outlet. In the centre of the detonation chamber there is a double-layer cylindrical propulsion charge with semispherical end faces. Said propulsion charge consists of explosives having a higher brisance in the top layer and fourteen electric detonators that are mounted being diametrally opposed and equally spaced one to another in three planes perpendicular to the axis in the top layer and at the end faces. At the front end face of the propulsion charge over a hole in the centre of the interior end cover of the detonation chamber housing over there is a semispherical detonation wave baffle turned with its concave side towards the propulsion charge. The engine is connected via a welded coupling sleeve to the charge housing that is tightly inserted into the border of said sleeve. Walls of the coupling sleeve are provided with air vents, and inside the sleeve there are from 4 to 8 pyrovalves for discharging pressure from the cavity of the detonation chamber. Ejectable obturators are mounted on the surface of the charge housing.;EFFECT: increasing the flight velocity and destructive capacity of the projectile.;1 dwg
机译:领域:弹丸包括发动机,该发动机具有不定形的引爆室,该引爆室具有后部排气喷嘴和环形排气窗,该环形排气窗在所述腔室的前端面上方超出该腔室的外表面,并且在进气口处是双层的出口处是单层的。在爆轰室的中心有一个带有半球形端面的双层圆柱推进装药。所述推进装药由在顶层中具有较高辉度的炸药和十四个电雷管组成,这些电雷管在径向上相对并且在垂直于顶层中的轴线并且在端面处的三个平面中彼此等距地安装。在推进装药的前端表面上方的爆轰室壳体的内部端盖的中心的孔上,有一个半球形的爆轰波挡板,其凹侧朝向推进装药。发动机通过焊接的联轴器套筒连接到充气室,该充气室紧紧地插入所述套筒的边界。联轴器套筒的壁上设有通风孔,在套筒的内部有4到8个热解阀,用于从爆轰腔腔中释放压力。可装药的密闭装置安装在弹药外壳的表面上;效果:增加了弹丸的飞行速度和破坏能力; 1 dwg

著录项

  • 公开/公告号RU2325614C2

    专利类型

  • 公开/公告日2008-05-27

    原文格式PDF

  • 申请/专利权人 KOVALEVSKIJ SERGEJ NIKOLAEVICH;

    申请/专利号RU20050132691

  • 发明设计人 KOVALEVSKIJ SERGEJ NIKOLAEVICH;

    申请日2005-10-24

  • 分类号F42B15/10;F42B12/00;F42B10/38;F02K1/52;

  • 国家 RU

  • 入库时间 2022-08-21 19:50:38

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