发射药药型结构对燃速测试结果的影响

为了研究药型结构对发射药燃速测试结果的影响,以高能硝胺发射药为研究对象,采用密闭爆发器燃烧实验和数据处理的分析方法,研究了4种药型及其不同内孔长径比发射药的燃速特性及其变化规律;采用中止燃烧实验研究了发射药内孔长径比对侵蚀燃烧的影响,并与太根发射药对比研究了燃速特性对侵蚀燃烧的影响关系。结果表明,多孔药的燃速压力指数明显小于单孔药,在内孔长径比相同的条件下,随着发射药内孔数量的增加,正比式燃速系数减小,燃速压力指数减小;在药型相同的条件下,随着内孔长径比增大,发射药侵蚀燃烧现象加剧,正比式燃速系数增大,燃速压力指数减小;燃速较高的发射药,侵蚀燃烧现象对燃速参数测试结果的影响更大。

Influence of Propellant Structure on Test Results of Burning Rate

In order to study the influence of charge structure on the test results of the burning rate of propellants,high energy nitramine propellants was taken as study object.By using closed bomb fired test and data treatment methods,the burning rate of propellants of four type structures and different inner hole aspect ratio of the burning rate and its variation character were researched.Using intermission burning test,the influence of the inner hole aspect ratio of propellant on erosive burning was studied.Compared with TEGN propellant,the influence of the burning rate on erosive burning was investigated.Results show that,the burning rate pressure exponent of multiperforated propellant is significantly less than that of the cylindrical monoperforated grain;under the same inner hole aspect ratio condition,the proportional burning rate coefficient u1decreases with the increase of inner holes of propellants,and the burning rate pressure exponent n decreases.Under the same charge structure condition,propellant erosive burning intensifies with increase of the inner hole aspect ratio,and the proportional burning rate coefficient u1 increases,and the burning rate pressure exponent n decreases.The higher the burning rate of propellant,the more significant the impact of erosive combustion on burning rate parameters.