저온 분사 코팅을 이용한 성형작약탄 라이너의 기공경사 반응성 코팅 형성방법 및 이에 따라 제조된 고반응성 코팅층을 갖는 성형작약탄의 라이너
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    发明授权
    저온 분사 코팅을 이용한 성형작약탄 라이너의 기공경사 반응성 코팅 형성방법 및 이에 따라 제조된 고반응성 코팅층을 갖는 성형작약탄의 라이너 有权
    使用动力喷雾涂层制造分级多层多层反应形状充电衬板的方法及其制造的分级多层多层反应形状充电衬板

    公开(公告)号:KR101346238B1

    公开(公告)日:2014-01-03

    申请号:KR1020120116617

    申请日:2012-10-19

    CPC classification number: F42B1/032 F42B33/14 C23C24/04

    Abstract: A graded porous multi-layered reactive coating method for a shaped charge liner using low temperature spray coating, given in the present invention, includes: a heating and pressurizing step (S120) of heating and pressurizing process gas to make the gas reach a preset temperature and a preset pressure; an acceleration step (S130) of accelerating the gas to supersonic speed by being compressed and expanded while passing through a nozzle (25); a powder supply step (140) of supplying powder for enacting a thermite reaction stored separately from the process gas into the nozzle where the process gas flows to transfer the powder along the nozzle; a powder spray step of spraying the powder which is accelerated by the process gas while moving together with the process gas within the nozzle from the nozzle onto the surface of a basic material (S) which is to be a liner for a shaped charge; and a plastic deformation step of forming a highly-reactive coating layer through plastic deformation on the surface of the basic material by making the powder from the nozzle collide with the basic material. The liner for a shaped charge having a highly-reactive layer manufactured by the method described above has a highly-reactive coating layer (13a) which comprises: a surface coating layer (13aa) which does not have pores from the surface of the liner to a certain depth; and a graded porous coating layer (13ab) of which the pore density decreases as the depth from the surface of the liner grows. [Reference numerals] (AA) Pore density (%); (BB) Depth from the surface(關m)

    Abstract translation: 在本发明中给出的使用低温喷涂的成形电荷衬垫的分级多孔多层反应性涂布方法包括:加热和加压工艺气体以使气体达到预设温度的加热和加压步骤(S120) 和预设压力; 加速步骤(S130),其通过在通过喷嘴(25)的同时被压缩和膨胀而将气体加速至超音速; 粉末供给步骤(140),其供应粉末,用于将与所述处理气体分开存储的铝热反应分配到所述工艺气体流动的喷嘴中,以沿着所述喷嘴转移所述粉末; 粉末喷射步骤,喷射由处理气体加速的粉末,同时与喷嘴内的处理气体一起从喷嘴移动到作为成形填料的衬垫的基础材料(S)的表面上; 以及通过使来自喷嘴的粉末与基材碰撞而在基材表面上通过塑性变形形成高反应性涂层的塑性变形步骤。 用于通过上述方法制造的具有高反应性层的成形装料的衬垫具有高反应性涂层(13a),其包括:表面涂层(13aa),其不具有从衬垫的表面到 一定深度; 和梯度多孔涂层(13ab),其密度随着衬垫表面的深度增加而减小。 (AA)孔密度(%); (BB)表面深度(关)

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