Dynamic Response of the Polyetherimide Sabot of a Long Rod Projectile under Bore Pressure Load
-
摘要: 建立了长杆弹的动力学计算模型,弹托采用新型玻璃纤维增强聚醚酰亚胺复合材料,利用LS-DYNA软件模拟了长杆弹在轻气炮膛压载荷下的运动过程,分析了复合材料弹托的动力学响应规律,并对弹托结构进行了改进。结果表明:最大膛压时弹托各处应力达到最大,高应力区分布在弹托尾部外围附近及后齿齿根上,齿根、齿顶应力大小不同;弹托头部强度裕度较大,通过改进弹托结构,在满足发射强度的同时,弹托质量减少了16 g,弹丸初速提高了612.2 m/s。Abstract: A dynamic calculation model for launching a long rod projectile was established in this paper, where the sabot used a new type of glass fiber reinforced polyetherimide composite material, and then the dynamic deformation of the sabot under the light gas gun pressure load was analyzed by the LS-DYNA software. The results show that the maximum stress inside the sabot occurs at the maximum bore pressure. The high stress area is distributed on the outer periphery and the root tooth of the sabot tail. The stresses at the tooth root and tooth tip are different with the overplus of material strength at the sabot head. By improving the structure of the sabot, the mass of the sabot is reduced by 16 g with the extra velocity gain of 612.2 m/s at given launching pressure.
-
Key words:
- composite material sabot /
- dynamic model /
- dynamic response /
- structural optimization
-
表 1 塑性随动硬化模型材料参数
Table 1. Material parameters in plastic-kinematic strength model
Material $\;\rho $0/(g∙cm–3) Ep/GPa $\;\mu $ Y/GPa $\varepsilon $eff 40CrNiMo 7.86 207.0 0.30 0.920 0.9 PEI GF30 1.51 9.5 0.33 0.185 0.6 -
[1] 赵国志, 王晓鸣, 潘正伟, 等. 杆式穿甲弹设计理论 [M]. 北京: 兵器工业出版社, 1997: 1–3.ZHAO G Z, WANG X M, PAN Z W, et al. Design theory of rod armor-piercing projectile [M]. Beijing: Ordnance Industry Press, 1997: 1–3. [2] 王迎春, 王洁, 管维乐. 穿甲弹的现状及发展趋势研究 [J]. 飞航导弹, 2013, 43(1): 48–52.WANG Y C, WANG J, GUAN W L. Research on current situation and development trend of armor-piercing projectile [J]. Aerodynamic Missile Journal, 2013, 43(1): 48–52. [3] 杨淑丽. 塑料及复合材料弹托 [J]. 弹箭技术, 1998(2): 42–45.YANG S L. Plastic and composite material sabot [J]. Projectile and Rocket Technology, 1998(2): 42–45. [4] 张文栓, 蒋文玲, 吴忠泉, 等. S-2玻纤增强树脂基复合材料弹托的试验研究 [J]. 兵工学报, 2000, 21(1): 77–79. doi: 10.3321/j.issn:1000-1093.2000.01.022ZHANG W S, JIANG W L, WU Z Q, et al. An experimental study sabots made of S-2 glass fiber reinforced composites [J]. Acta Armamentarii, 2000, 21(1): 77–79. doi: 10.3321/j.issn:1000-1093.2000.01.022 [5] 秦长虎, 杨艺竹. 关于脱壳穿甲弹弹托材料发展方向的探讨 [J]. 兵器材料科学与工程, 2001, 24(3): 69–71. doi: 10.3969/j.issn.1004-244X.2001.03.019QIN C H, YANG Y Z. Study on development trend of APDS sabot material [J]. Ordnance Material Science and Engineering, 2001, 24(3): 69–71. doi: 10.3969/j.issn.1004-244X.2001.03.019 [6] 佟文敏, 赵国志. 复合材料弹托结构的发射强度计算分析 [C]//中国兵工学会弹药学术年会. 张家界, 1998: 118–123.TONG W M, ZHAO G Z. Calculation and analysis of launching strength of composite material sabot structure [C]//China Ordnance Society Ammunition Academic Annual Meeting. Zhangjiajie, 1998: 118–123. [7] BURNS B P, DRYSDALE W H, HOPPEL C P R, et al. The development of composite sabots for kinetic energy projectiles [C]//19th International Symposium of Ballistics. Switzerland, 2001: 347–353. [8] 唐蜜, 沈培辉, 李平, 等. 间隙啮合技术在大威力穿甲弹上的应用 [J]. 弹道学报, 2006, 18(3): 84–86. doi: 10.3969/j.issn.1004-499X.2006.03.021TANG M, SHEN P H, LI P, et al. Application of interval meshing technology to the high power armor piercing projectiles [J]. Journal of Ballistics, 2006, 18(3): 84–86. doi: 10.3969/j.issn.1004-499X.2006.03.021 [9] 刘世国. 某异形穿甲弹强度与模态分析及结构优化 [D]. 南京: 南京理工大学, 2009: 47–68.LIU S G. Strength and modal analysis and structural optimization of a special-shaped armor-piercing projectile [D]. Nanjing: Nanjing University of Science and Technology, 2009: 47–68. [10] 闫季华. 尼龙弹托结构尾翼稳定脱壳穿甲弹 [D]. 南京: 南京理工大学, 2010: 11–39.YAN J H. Nylon sabot structure of the armor-piercing fin-stabilized discarding-sabot projectile [D]. Nanjing: Nanjing University of Science and Technology, 2010: 11–39. [11] WANG C K, CHEN G, LU D X, et al. Emission intensity of composite material sabot after material deletion using ABAQUS [C]//Mechanics and Mechanical Engineering: Proceedings of the 2015 International Conference. Chengdu, 2016: 671–677. [12] 苑明华. 小口径全塑弹总体设计分析 [D]. 南京: 南京理工大学, 2004: 27–35.YUAN M H. Analysis of overall design of small caliber full plastic projectile [D]. Nanjing: Nanjing University of Science and Technology, 2004: 27–35. [13] 王秦安. 长杆式尾翼稳定脱壳穿甲弹结构强度的有限元计算方法及计算分析 [J]. 弹箭与制导学报, 1989(2): 7–19.WANG Q A. Finite element calculation method and calculation analysis of the structural strength of the armor-piercing fin-stabilized discarding-sabot projectile [J]. Journal of Projectiles, Rockets, Missiles and Guidance, 1989(2): 7–19. [14] 钱民刚. 联合计算穿甲弹弹体与弹托的应力及变形 [J]. 兵工学报, 1986(3): 28–34.QIAN M G. Combined calculation of deformation and stress for the body and the sabot of an APFSDS [J]. Acta Armamentarii, 1986(3): 28–34. [15] 沈观林, 胡更开. 复合材料力学 [M]. 2版. 北京: 清华大学出版社, 2013: 86–94.SHEN G L, HU G K. Composite material mechanics [M]. 2nd ed. Beijing: Tsinghua University Press, 2013: 86–94.