Combustion laws of dished head conic-column grain
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摘要:
装药设计方法影响发动机内弹道性能,为提高装药利用率,分别采用UG NX和MATLAB软件进行了建模和编程计算,得到了药柱燃烧过程中燃烧面积推移规律和残药率与设计参数的函数关系图,进行了算例分析。计算结果表明:以药柱外径
D 为基准,当环向槽圆弧半径$ r \in$ (0,0.05D ),圆柱段内孔半径$ {R_2} \in $ (0.1D ,0.4D ),环向槽圆弧圆心旋转半径$ {R_3} \in $ ($ {R_2} $ ,0.42D ),圆柱段长$ {L_2} \in $ (0.4D ,1.53D )时,药柱燃烧呈现先增面性后减面性。残药率与$ r $ 和$ {R_2} $ 的变化趋势同为单调递减,残药率与$ {L_2} $ 的变化趋势为单调递增,残药率与$ {R_3} $ 的变化趋势为先增大后减小。从减轻重量,提高强度和提高产品加工制造的工艺性等方面综合考虑,建议优先选择碟形封头。计算结果与实际数据的最大相对误差为0.078%。Abstract:Charge design methods affect the ballistic performance of the engine. In order to improve the charge utilization rate, UG NX and MATLAB software were used for modeling and programming of the calculation, and the function relationship diagram of the combustion surface, the residual drug rate and the design parameters during the combustion process of the drug column was obtained, and finally the example analysis was carried out. The results showed that when
D was defined as the outer diameter of grain, and the relative radius of circular groove$ r $ was (0, 0.05D ), the relative radius of the hole in the cylindrical section$ {R_2} $ was (0.1D , 0.4D ), the relative radius of the circular center of the circular groove$ {R_3} $ was ($ {R_2} $ , 0.42D ) and the length of the cylinder$ {L_2} $ was (0.4D , 1.53D ), the combustion law was progressive at first and then regressive. The waste grain rate and the change trend of$ r $ and$ {R_2} $ monotonically decreased, the waste grain rate and the change trend of$ {L_2} $ monotonically increased, and the waste grain rate and the change trend of$ {R_3} $ first increased and then decreased. From the aspects of weight reduction, improvement of the strength, processing and manufacturing, it is recommended to give priority to the dished head. The maximum relative error between the calculated result and the actual data was 0.078%.-
Key words:
- dished head conic-column grain /
- waste grain rate /
- burning law /
- solid rocket motor /
- wall thickness
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表 1 计算燃烧面积与UG提取燃烧面积数据对比
Table 1. Data comparison between burning areas by calculated and extracted from UG
e 面积/mm2 相对
误差/%UG提取 公式计算 0 238436.16 238309.56 0.053 e1 334076.46 334069.78 0.002 (e1+e2)/2 310675.48 310631.99 0.014 e2 277875.48 277769.92 0.039 e3 271807.12 271676.71 0.048 e4 249780.29 249712.87 0.027 e5 231567.18 231407.51 0.069 (e5+e6)/2 206687.47 206668.87 0.009 e6 161727.81 161601.76 0.078 -
[1] 晁侃,王健儒,陆贺建. 残余限燃环对大型分段式固体火箭发动机凝相沉积的影响[J]. 固体火箭技术,2021,44(1): 9-15. doi: 10.7673/j.issn.1006-2793.2021.01.003CHAO Kan,WANG Jianru,LU Hejian. Influence of residual annular insulator on slag accumulation in segmented SRM[J]. Journal of Solid Rocket Technology,2021,44(1): 9-15. (in Chinese) doi: 10.7673/j.issn.1006-2793.2021.01.003 [2] 王元有. 固体火箭发动机设计[M]. 北京: 国防工业出版社, 1984. [3] 鲍福廷, 侯晓. 固体火箭发动机设计[M]. 北京: 中国宇航出版社, 2016. [4] OH S H,LEE H J,ROH T S. Development of a hybrid method in a 3-D numerical burn-back analysis for solid propellant grains[J]. Aerospace Science and Technology,2020,106: 106103. doi: 10.1016/j.ast.2020.106103 [5] KI W,KO T,KIM S,et al. 3D grain burnback analysis using the partial interface tracking method[J]. Aerospace Science and Technology,2017,68: 58-67. doi: 10.1016/j.ast.2017.04.023 [6] 苗海玉,刘少伟,朱柏银. 基于动网格的装药燃烧的燃面退移仿真[J]. 火力与指挥控制,2019,44(1): 156-160, 165. doi: 10.3969/j.issn.1002-0640.2019.01.031MIAO Haiyu,LIU Shaowei,ZHU Baiyin. A simulation research of surface regression in propellant charge combustion process based on dynamic mesh[J]. Fire Control & Command Control,2019,44(1): 156-160, 165. (in Chinese) doi: 10.3969/j.issn.1002-0640.2019.01.031 [7] ZHENG Jinyang, YU Yehong, CHEN Yehong, et al. Comparison of ellipsoidal and equivalent torispherical heads under internal pressure: buckling, plastic collapse and design rules[J]. Journal of Pressure Vessel Technology, 2021, 143(2): 021301. [8] ZHENG Jinyang,ZHANG Zekun,LI Keming,et al. A simple formula for prediction of plastic collapse pressure of steel ellipsoidal heads under internal pressure[J]. Thin-Walled Structures,2020,156: 106994. doi: 10.1016/j.tws.2020.106994 [9] 席运志,王宁飞,李军伟,等. 基于旋转阀的固体火箭发动机燃烧室压强振荡特性[J]. 兵工学报,2021,42(1): 33-44. doi: 10.3969/j.issn.1000-1093.2021.01.004XI Yunzhi,WANG Ningfei,LI Junwei,et al. Oscillation characteristics of pressure in combustor with rotary valve for solid rocket engine[J]. Acta Armamentarii,2021,42(1): 33-44. (in Chinese) doi: 10.3969/j.issn.1000-1093.2021.01.004 [10] LIU Weitao,LI Qiang,ZHAO Jiyuan. Application on floor water inrush evaluation based on AHP variation coefficient method with GIS[J]. Geotechnical and Geological Engineering,2018,36(5): 2799-2808. doi: 10.1007/s10706-018-0502-2 [11] OTAY İ,OZTAYSI B,CEVIK ONAR S,et al. Multi-expert performance evaluation of healthcare institutions using an integrated intuitionistic fuzzy AHP & DEA methodology[J]. Knowledge-Based Systems,2017,133: 90-106. doi: 10.1016/j.knosys.2017.06.028 [12] ALI S A,AHMAD A. Mapping of mosquito-borne diseases in Kolkata Municipal Corporation using GIS and AHP based decision making approach[J]. Spatial Information Research,2019,27(3): 351-372. doi: 10.1007/s41324-019-00242-8 [13] LIU Sainan. E-shop transshipment selection evaluation based on cloud model[J]. Journal of Shanghai Jiaotong University (Science),2018,23(5): 643-649. doi: 10.1007/s12204-018-1978-x [14] 姚枫秋,相升海,张德键. 车轮型药柱燃烧规律研究[J]. 兵器装备工程学报,2021,42(2): 76-81, 126. doi: 10.11809/bqzbgcxb2021.02.014YAO Fengqiu,XIANG Shenghai,ZHANG Dejian. Study on burning law of wheel-shaped grain[J]. Journal of Ordnance Equipment Engineering,2021,42(2): 76-81, 126. (in Chinese) doi: 10.11809/bqzbgcxb2021.02.014 [15] 张维星, 唐国金. 基于三维参数化建模的翼柱形发动机药形优化[J]. 固体火箭技术, 2014, 37(4): 490-495.ZHANG Weixing, TANG Guojin. Optimization of finocyl grain based on the three-dimensional parameterized modeling[J]. Journal of Solid Rocket Technology, 2014, 37(4): 490-495. (in Chinese) finocyl grain based on the three-dimensional parameterized modeling[J]. Journal of solid rocket technology, 2014, 37(4): 490-495. [16] 褚佑彪,张岗,苑博,等. 固体火箭发动机装药燃面计算方法[J]. 固体火箭技术,2016,39(4): 488-491, 502.CHU Youbiao,ZHANG Gang,YUAN Bo,et al. Burning surface computing method for solid rocket motor grain[J]. Journal of Solid Rocket Technology,2016,39(4): 488-491, 502. (in Chinese) [17] 相升海,杨艳羽,李世鹏,等. 减小半球锥柱型药柱残药率的研究[J]. 航空动力学报,2019,34(6): 1389-1398. doi: 10.13224/j.cnki.jasp.2019.06.022XIANG Shenghai,YANG Yanyu,LI Shipeng,et al. Study on reduction of waste grain rate for semi-spherical conic-column grain[J]. Journal of Aerospace Power,2019,34(6): 1389-1398. (in Chinese) doi: 10.13224/j.cnki.jasp.2019.06.022 [18] 鲁雨,贺小华. 内压标准椭圆封头弹塑性屈曲分析及失效载荷研究[J]. 压力容器,2019,36(11): 25-33.LU Yu,HE Xiaohua. Investigation on elastic-plastic buckling and failure load of standard elliptical head under internal pressure[J]. Pressure Vessel Technology,2019,36(11): 25-33. (in Chinese) [19] 刘江涌. 关于几种形式封头特点的比较[J]. 广东化工,2012,39(7): 202-203. doi: 10.3969/j.issn.1007-1865.2012.07.109LIU Jiangyong. On the characteristics of several forms of head[J]. Guangdong Chemical Industry,2012,39(7): 202-203. (in Chinese) doi: 10.3969/j.issn.1007-1865.2012.07.109 [20] 朱燕梅,许进文. 碟形封头的几何参数和应力分析[J]. 石油化工设计,2008,25(4): 8-10, 21. doi: 10.3969/j.issn.1005-8168.2008.04.004ZHU Yanmei,XU Jinwen. Geometrical parameter and stress analysis on dished head[J]. Petrochemical Design,2008,25(4): 8-10, 21. (in Chinese) doi: 10.3969/j.issn.1005-8168.2008.04.004 [21] 王战辉,马向荣,范晓勇,等. 凸形封头压力容器优化设计[J]. 轻工机械,2019,37(2): 98-104. doi: 10.3969/j.issn.1005-2895.2019.02.019WANG Zhanhui,MA Xiangrong,FAN Xiaoyong,et al. Optimization design of pressure vessel with convex head[J]. Light Industry Machinery,2019,37(2): 98-104. (in Chinese) doi: 10.3969/j.issn.1005-2895.2019.02.019 [22] 唐保威,徐平. 内压碟形封头塑性垮塌压力预测方法[J]. 压力容器,2021,38(4): 34-41. doi: 10.3969/j.issn.1001-4837.2021.04.005TANG Baowei,XU Ping. Method for prediction of plastic collapse pressure of torispherical heads under internal pressure[J]. Pressure Vessel Technology,2021,38(4): 34-41. (in Chinese) doi: 10.3969/j.issn.1001-4837.2021.04.005 [23] 杨艳羽. 火箭发动机装配机设计及锥柱型药柱燃烧规律研究[D]. 沈阳: 沈阳理工大学, 2019.YANG Yanyu. Design of rocket motor assembly machine and study on burning law of conocyl grain[D]. Shenyang: Shenyang Ligong University, 2019. (in Chinese) [24] 杨艳羽,相升海,刘瑞东,等. 平底锥柱型药柱燃烧规律研究[J]. 弹箭与制导学报,2019,39(1): 79-83. doi: 10.15892/j.cnki.djzdxb.2019.01.017YANG Yanyu,XIANG Shenghai,LIU Ruidong,et al. Study on burning law of fat-bottome conic-column grain[J]. Journal of Projectiles, Rockets, Missiles and Guidance,2019,39(1): 79-83. (in Chinese) doi: 10.15892/j.cnki.djzdxb.2019.01.017 -