两相流对燃料颗粒点火及其偏离弹壳的影响

L. L. Minkov
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引用次数: 0

摘要

假热目标对飞机和直升机的安全起着重要作用。其主要任务是确保燃料颗粒在离开弹壳前稳定点燃。为了优化这一过程,必须研究各种参数的影响,例如弹壳与燃料颗粒圆柱表面之间的间隙大小,以及来自引发剂和燃料颗粒的颗粒大小。本文提供了燃料颗粒点火和离火过程的物理和数学模型,并研究了指定参数对点火时间的影响。本文估算了不同粒径(r = 1 μm 和 r = 25 μm)颗粒端面的点火时间,弹壳与颗粒圆柱面之间的间隙为 0.5 毫米至 2 毫米。在颗粒大小分别为 1 μm 和 25 μm 以及弹壳与燃料颗粒圆柱表面之间的间隙不同的情况下,获得了颗粒从弹壳中输出的速度。
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EFFECT OF TWO-PHASE FLOW ON THE FUEL GRAIN IGNITION AND ITS DEPARTURE FROM THE CARTRIDGE CASE
False heat targets play an important role in the safety of aircraft and helicopters. The main task is to ensure stable ignition of the fuel grain before leaving the cartridge case. In order to optimize this process, it is important to study the influence of various parameters, such as the size of the gap between the cartridge case and the cylindrical surface of fuel grain, as well as the size of the particles coming from the initiator and fuel grain. This article offers a physical and mathematical model of the ignition and departure process of the grain, and studies the influence of the specified parameters on the ignition time. The ignition times of the grain end surface for different particle sizes equals r = 1 μm and r = 25 μm have been estimated, the gap between the cartridge case and the cylindrical surface of grain ranged from 0.5 mm to 2 mm. The output velocities of the grain from the cartridge case are obtained for particles equal to 1 μm and 25 μmand different gap between the cartridge case and the cylindrical surface of fuel grain.
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