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炮膛内底排装置燃烧特性计算分析 被引量:6

Calculation and Analysis on the Combustion Characteristics of a Base Bleed Unit in the Gun Bore
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摘要 为了研究内弹道过程中底排装置的燃烧特性,基于两组不同底排药剂试样装填密度下的密闭爆发器燃烧试验数据,优化计算得到了高压工况下某底排药剂燃速模型为de/dt=8.51×10-8p0.579.建立了底排装置膛内燃烧模型与火炮—底部排气弹内弹道零维模型。针对某155 mm底排装置,在理想发射环境下,计算分析表明:膛内底排装置压力与弹底压力之间的压差经历了增大—减小—平衡—增大—减小的过程;底排装置喷口燃气流入与流出量基本趋于平衡;膛内过程底排药剂燃烧量约为8.22 g;底排药剂全面点火燃烧延迟时间引起的弹丸初速变化量不大,最大不超过0.4 m/s,故可忽略不计;底排药剂燃烧量随延迟时间的增加近似呈指数递减趋势。研究结果为分析底部排气弹出膛口瞬间药柱质量偏差引起的射程散布提供基础数据。 To research the combustion characteristics of base bleed unit in the interior ballistic process,a high pressure burning rate model of base bleed propellant described as de/dt=8.51×10-8p0.579 was obtained by utilizing an optimization method based on two sets of closed bomb experimental data with different loading density.Both the general combustion model of base bleed unit in bore and 0-D interior ballistic model of gun-base bleed projectile were established.For a 155mm base bleed unit,the research results obtained under an ideal firing condition are as follows: the difference between the pressures in the base bleed unit and under the projectile base is subjected to an increasing-decreasing-balancing-increasing-decreasing history;the mass of inflow is approximately equal to the outflow at the unit exit;the calculated burning mass of base bleed propellant is about 8.22 g;the maximum change of the muzzle velocity caused by the ignition-combustion delay time is less than 0.4 m/s which could be ignored;the burning mass of base bleed propellant is reduced exponentially with the increase in delay time.The results provide the basic data for analyzing the range dispersion caused by the mass deviation of the propellant from the gun muzzle.
出处 《兵工学报》 EI CAS CSCD 北大核心 2011年第5期526-531,共6页 Acta Armamentarii
基金 南京理工大学自主科研专项计划项目(2010GJPY023)
关键词 应用力学 底排装置 内弹道 燃烧特性 数值计算 applied mechanics base bleed unit interior ballistics combustion performance numerical calculation
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  • 1James E Danberg. Analysis ofthe flight performance of the 155 mm M864 base bsrn projectile, AD-A222-624 [R ]. US: DTIC, 1990.
  • 2Lyle D Kayser, John D Kuzan, David N Vazguez. Flight testing for a 155 mm base burn projectile, AD-A222-562 [ N]. US: DTIC, 1990.
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  • 4张领科,周彦煌,余永刚.底排装置工作不一致性对射程散布影响的研究[J].兵工学报,2010,31(4):442-446. 被引量:14

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