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METHOD OF jet formation shaped charges and shaped charges, realizing this approach

机译:射流形成的装药和装药的方法,实现了这种方法

摘要

1. A method for controlling the formation of the shaped charge jet, comprising the initiation and development of the detonation wave by a checker of explosive charge situated in a metal body, compression and throwing cumulative lining placed on the opposite side of the open drafts initiating shock and detonation products, collapse on the axis of symmetry of the inert charge cladding material and forming therefrom a cumulative jet with desired parameters, characterized in that the shape and specific gravity in tavki additionally introduced into the lower open part facing determines kinematic characteristics of this part of the shaped-charge jet penetration to optimize a particular target, while maintaining the dimensions and parameters of cumulative facing the head portion cumulative strui.2. A method according to claim 1, characterized in that during application of additional layers strueobrazuyuschego (with tungsten or other with high specific gravity material) on the outer side of the lining, to maintain a certain speed mode of each portion of the jet must be conserved cumulative integral density balance of each liner fragment from top to bottom due to a proportional reduction of cumulative oblitsovki.3 previous layer. Shaped charge comprising a metal housing axisymmetric checker explosive with an open cavity in the shape of the body of rotation (cone, ellipsoid, etc.) adjacent to the cavity surface of the combined liner disposed on the opposite end wall checkers initiating node, characterized in that the cladding accumulatively
机译:1.一种用于控制成形射流的形成的方法,包括:通过位于金属主体中的炸药的检查器来引发和产生爆轰波,将压缩的和投掷的累积衬里放置在开放吃水的相对侧上,以引发爆炸波。冲击和爆炸产物,在惰性装料材料的对称轴上塌陷,并由此形成具有所需参数的累积射流,其特征在于,塔夫基中的形状和比重还被引入下部开口面,从而决定了这种运动特性聚能射流穿透的一部分,以优化特定目标,同时保持面向头部的累积结构的尺寸和参数。2。 2.根据权利要求1所述的方法,其特征在于,在衬里的外侧上施加附加层strueobrazuyuschego(具有钨或其他具有高比重的材料)时,必须保持射流的每个部分的一定速度模式。由于累积oblitsovki.3前一层的成比例减少,每个衬里碎片从上到下的累积积分密度平衡。成形装药,包括金属外壳的轴对称方格炸药,该炸药的旋转体(圆锥形,椭圆形等)为开放腔,与组合衬套的腔体表面相邻,并位于相对端壁方格始发节点上,其特征在于覆层累积

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