无喷管助推器药柱结构优化设计研究

推进技术 ›› 2017, Vol. 38 ›› Issue (5): 1173-1179.

无喷管助推器药柱结构优化设计研究

黄礼铿,杨玉新,霍东兴,马利锋

西安航天动力技术研究所，陕西西安 710025,西安航天动力技术研究所，陕西西安 710025,西安航天动力技术研究所，陕西西安 710025,西安航天动力技术研究所，陕西西安 710025

发布日期:2021-08-15
作者简介:黄礼铿，男，博士，研究领域为固体火箭冲压发动机。

Optimization Design of Nozzleless Booster Grain

The Xi’an Institute of Aerospace Propulsion Technology，Xi’an 710025，China,The Xi’an Institute of Aerospace Propulsion Technology，Xi’an 710025，China,The Xi’an Institute of Aerospace Propulsion Technology，Xi’an 710025，China and The Xi’an Institute of Aerospace Propulsion Technology，Xi’an 710025，China

Published:2021-08-15

摘要/Abstract

摘要： 为了得到无喷管助推器药柱设计的最优解，采用无喷管助推器一维非定常内弹道计算方法和粒子群模式搜索混合优化算法，构建了无喷管助推器药柱优化设计框架，优化框架中粒子群算法用于全局搜索，模式搜索算法用于局部搜索。对圆柱内孔装药无喷管助推器的药柱结构进行了优化设计，最大化总冲设计在不增大峰值压强的条件下总冲提升了5.4%，最小化峰值压强设计在总冲不降低的条件下峰值压强降低了33.8%，表明设计框架适用于无喷管助推器药柱优化设计过程，能够满足不同药柱设计的需求，混合优化算法的采用大大降低了优化设计代价。

关键词: 无喷管助推器；药柱结构；优化设计；粒子群算法；模式搜索算法

Abstract: In order to obtain optimum design of nozzleless booster grain，an integrated framework is presented to perform the design optimization of nozzleless booster propellant grains. The proposed framework consists of one dimension unsteady interior ballistics analysis methods and hybrid optimization approach，which use particle swarm optimization algorithm to do global search，and pattern search method to do local search. Two case studies have been performed to verify the feasibility and reliability of the developed grain optimization design framework. The total impulse maximum optimization received 5.4% total impulse increase at the condition of no peak pressure rising，and the peak pressure minimum optimization reduced the peak pressure about 33.8% with no total impulse decrease. These results show that the proposed design framework facilitates the grain optimization process and various grain design requirements can be met. The design cost has been remarkably reduced by the introduction of hybrid optimization method.

Key words: Nozzleless booster；Grain；Optimization design；Particle swarm algorithm；Pattern search algorithm

黄礼铿,杨玉新,霍东兴,马利锋. 无喷管助推器药柱结构优化设计研究[J]. 推进技术, 2017, 38(5): 1173-1179.

HUANG Li-keng,YANG Yu-xin,HUO Dong-xing,MA Li-feng. Optimization Design of Nozzleless Booster Grain[J]. Journal of Propulsion Technology, 2017, 38(5): 1173-1179.

参考文献

[1] 胡建新, 朱伯鹏, 夏智勋, 等. 固体火箭冲压发动机无喷管助推器性能分析[J]. 导弹与航天运载技术,2004, 271(4): 37-41.
[2] 汪志清. 无喷管固体发动机装药技术研究[J]. 推进技术, 1994, 15(3): 56-61. (WANG Zhi-qing. An Investigation of Charging Technology for Solid Propellant of Nozzleless Rocket Motors[J]. Journal of Propulsion Technology, 1994, 15(3): 56-61.)
[3] 李磊, 申志彬, 唐国金, 等. 考虑结构完整性和装填分数的星形药柱形状优化[J]. 推进技术, 2011, 32(2): 235-239. (LI Lei, SHEN Zhi-bin, TANG Guo-jin, et al. Shape Optimization of Star Shape Grain Considering Structure Integrity and Loading Fraction[J]. Journal of Propulsion Technology, 2011, 32(2): 235-239.)
[4] 丁林, 鲍福廷, 胡海峰, 等. 无喷管助推器组合装药研究[J]. 固体火箭技术, 2011, 34(3): 295-299.
[5] 霍东兴, 陈林泉, 严利民. 双燃速串装药柱无喷管助推器性能分析[J]. 航空兵器, 2008, (4): 40-43.
[6] 王永杰, 陈林泉, 霍东兴. 扩张半角对无喷管助推器性能的影响分析[J]. 固体火箭技术, 2009, 29(4): 431-435.
[7] 曹任刚. 无喷管固体火箭发动机内弹道计算[J]. 航空兵器, 2006, (1): 57-60.
[8] Alon Gany, Israel Aharon. Internal Ballistics Considerations of Nozzleless Rocket Motors[J]. Journal of Propulsion and Power, 1999, 15(6): 866-873.
[9] Aamir Raza M, Liang W. Robust Design Optimization of Dual Thrust Solid Propellant Motors Due to Burning Rate Uncertainties[J]. Propellants, Explosives, Pyrotechnics, 2012, 37(4): 476-488.
[10] Rao D L, Cai G B, Zhu H, et al. Design and Optimization of Variable Thrust Hybrid Rocket Motors for Sounding Rockets[J]. Science China Technological Sciences, 2012, 55(1): 125-135.
[11] Kamran A, Guozhu L. An Integrated Approach for Optimization of Solid Rocket Motor[J]. Aerospace Science and Technology, 2012, 17(1): 50-64.
[12] Dong-Hui W, Yang F, Fan H, et al. An Integrated Framework for Solid Rocket Motor Grain Design Optimization[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2014, 228(7): 1156-1170.
[13] Raza M A, Liang W. Design and Optimization of 3D Wagon Wheel Grain for Dual Thrust Solid Rocket Motors[J]. Propellants, Explosives, Pyrotechnics, 2013, 38(1): 67-74.
[14] Mukunda H S, Paul P J, Afroz Javed, et al. Extension of the Universal Erosive Burning Law to Partly Symmetric Propellant Grain Geometries[J]. Acta Astronautic, 2014, 93: 176-181.
[15] Lewis R M, Torczon V J. Pattern Search Methods for Linearly Constrained Minimization[J]. SIAM Journal on Optimization, 2000, 10(3): 917-941.
[16] Kennedy J, Eberhart R C. Particle Swarm Optimization[C]. Perth: IEEE International Conference on Neural Networks, 1995: 1942-1948.　　　　　　　　　　　　　*　收稿日期:2016-01-02；修订日期:2016-05-03。作者简介:黄礼铿,男,博士,研究领域为固体火箭冲压发动机。E-mail: hjlk68@126.com(編輯:朱立影)