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METHOD FOR GENERATION OF AIR SHOCK WAVE ON THE BASIS OF DETONATION OF FUEL-AIR MIXTURE AND DEVICE FOR ITS REALIZATION

机译:基于炸药混合气爆轰产生气震波的方法及其实现方法

摘要

FIELD: applied gas dynamics, applicable for investigation of objects and constructions for mechanical action of fluctuation pressures. SUBSTANCE: the method consists in the fact that a fine- disperse aerosol cloud is produced by ejection of liquid fuel by a powder charge through the channel of fuel delivery and a sprayer, its detonation is initiated by blasting of the charge of the trinitrotoluene exploder. Forming of the fine- disperse aerosol cloud of the fuel-air mixture is effected in the charging section of the shock tube in the form of a horizontal cylinder, and the fuel mass is calculated depending on the preset value of positive pressure in the front of the generated air shock wave and the distance from object of tests and the place of bursting of the fuel-air mixture. The device realizing the method has a sealed chamber with liquid fuel and powder charge, fuel feeding channels, sprayer, as well as an initiation system, the sprayer is positioned in the shock tube, located in the axis of the shock tube channel, made composite in the form of several, for example two aligned horizontal channels, with equidistant, transverse, opposite-directed sector slots with an opening angle of 165 to 175 deg made along their axis and a vertical axis of symmetry, and the distance between the slots is determined by calculation. EFFECT: expanded range of obtained parameters of the air shock wave. 2 cl, 4 dwg
机译:领域:所应用的气体动力学,适用于研究物体和结构的波动压力的机械作用。实质:该方法的事实在于,粉状装料通过燃料输送通道和喷雾器通过喷射液态燃料而产生细分散的气溶胶云,其爆炸是通过炸裂三硝基甲苯爆炸器的装料而引发的。燃料-空气混合物的细分散气溶胶云的形成是在水平管形式的减震管的充气段中进行的,并且燃料质量的计算取决于在前部的正压的预设值。产生的空气冲击波,与测试对象之间的距离以及燃油-空气混合物的爆破位置。实现该方法的装置具有带液体燃料和粉料的密封腔,燃料进料通道,喷雾器以及引发系统,喷雾器位于减震管中,位于减震管通道的轴线上,制成复合材料以几个例如两个对准的水平通道的形式,具有等距的,横向的,相反方向的扇形槽,沿着它们的轴线和垂直对称轴线形成的打开角度为165至175度,并且槽之间的距离为通过计算确定。效果:扩大了空气冲击波参数的范围。 2 cl,4 dwg

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