航天推进技术研究院主办
SHI Bo,HUANG Xuegang,ZHOU Jie,et al.Discussion on topology optimal design of nozzle motion structure under dynamic load[J].Journal of Rocket Propulsion,2021,47(05):42-48.
动态载荷下的喷管运动结构拓扑优化设计探讨
- Title:
- Discussion on topology optimal design of nozzle motion structure under dynamic load
- 文章编号:
- 1672-9374(2021)05-0042-07
- 分类号:
- V432
- 文献标志码:
- A
- 摘要:
- 基于等效静态载荷法(ESL)的设计思想,针对可调喷管在复杂动态力热载荷下的结构优化问题,提出通过刚体动力学仿真提取动态力载荷,按照运动过程分离成多个工况,将动态载荷下的结构优化问题转化成静态载荷下的多工况联合结构优化问题,简化了问题的求解难度。通过这种方法对喷管运动结构开展拓扑优化得到改进结构,开展多工况力热载荷仿真修改模型,迭代获得最终优化方案。优化结构对应各个工况最大位移减少22%~34%,最大应力减少10%~15%,结构质量减少24%。设计方法的有效性得到验证,为动态力热载荷下的结构优化探索出实用的设计方法。
- Abstract:
- In order to optimize the variable nozzle motion structure under the complex dynamic force and variable thermal load,a new design method was proposed based on the idea of Equivalent Static Load(ESL). Firstly,the dynamic force load was extracted by rigid dynamics simulation,and then several working conditions were separated according to the motion process. In this way,the structure optimization under the dynamic load was transformed into the joint structure optimization under several static loads. The difficulty of solving problem was simplified. The topology optimization of nozzle motion structure was carried out with this method. The optimal structure was modified based on the calculation of strength and stiffness for multiple working conditions under force and thermal load. The final optimized structure was obtained by design iteration. The results show that the maximum displacement of the improved structure is reduced by 22% to 34%,the maximum stress is reduced by 10% to 15%,the weight is reduced by 24%. The effectiveness of the method has been proved,which provides a practical design method for structure optimization under dynamic force and variable thermal load.
参考文献/References:
[1] 易仕和,赵玉新,何霖.超声速与高超声速喷管设计[M].北京:国防工业出版社,2013. [2] 梁俊龙,吴宝元,李斌.几何结构可调的亚燃冲压发动机性能研究[J]. 火箭推进,2010,36(2):1-4.LIANG J L,WU B Y,LI B. Performance research of adjustable geometric structure ramjet engine[J]. Journal of Rocket Propulsion,2010,36(2):1-4. [3] 刘大响.航空发动机设计手册:进排气装置(第7册)[M].北京:航空工业出版社,2000. [4] 陈建军,车建文,崔明涛,等.结构动力优化设计述评与展望[J].力学进展,2001,31(2):181-192. [5] TSENG C H,ARORA J S.Optimum design of systems for dynamics and controls using sequential quadratic programming[J].AIAA Journal,1989,27(12):1793-1800. [6] KANG B S,CHOI W S,PARK G J.Structural optimization under equivalent static loads transformed from dynamic loads based on displacement[J].Computers & Structures,2001,79(2):145-154. [7] CHOI W S,PARK G J.Structural optimization using equivalent static loads at all time intervals[J].Computer Methods in Applied Mechanics and Engineering,2002,191(19/20):2105-2122. [8] VANDERPLAATS G N.Thirty years of modern structural optimization[J].Advances in Engineering Software,1993,16(2):81-88. [9] BARTHELEMY J F M,HAFTKA R T.Approximation concepts for optimum structural design—a review[J].Structural Optimization,1993,5(3):129-144. [10] CHOI W S,PARK G J.Transformation of dynamic loads into equivalent static loads based on modal analysis[J].International Journal for Numerical Methods in Engineering,1999,46:29-43. [11] 孙焕纯,石连栓,柴山.考虑动应力、动位移约束的离散变量结构优化设计[J].计算力学学报,1997,14:723-726. [12] 毛虎平,董小瑞,郭保全,等.面向所有节点等效静态载荷的模态叠加法的结构动态响应优化[J].计算机辅助设计与图形学学报,2017,29(9):1759-1766. [13] 芮强,王红岩,田洪刚.基于等效静态载荷法的结构动态优化[J].汽车工程,2014,36(1):61-65. [14] 刘宇,朱成章,尹剑,等.基于等效静态载荷法的平衡吊臂架结构优化[J].中国工程机械学报,2020,18(2):159-164. [15] 陆佑方.柔性多体系统动力学[M].北京:高等教育出版社,1996. [16] 李修峰,王亚斌,王晨.MotionView&MotionSolve 应用技巧与实例分析[M].北京:机械工业出版社,2013. [17] 何芝,雷阳,封硕,等.基于SIMP法的变刚度结构拓扑优化研究[J].装备制造技术,2020(1):8-14. [18] 洪清泉,赵康,张攀,等.OptiStruct & HyperStudy 理论基础与工程应用[M].北京:机械工业出版社,2012. [19] 张卫红,章胜冬,高彤.薄壁结构的加筋布局优化设计[J].航空学报,2009,30(11):2126-2131. [20] 刘双燕,涂玉倩,苗应刚,等.筋的截面形状对薄壁结构振动疲劳性能的影响[J].航空工程进展,2017,8(2):190-198.
备注/Memo
基金项目:国家自然科学基金(11702205)
作者简介:石波(1980—),男,硕士,高级工程师,研究领域为冲压发动机总体设计。