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[1]程宏川,吴 剑,廖云龙,等.利用气浮技术进行贮箱晃动试验方法研究[J].火箭推进,2017,43(02):47-51.
　CHENG Hongchuan,WU Jian,LIAO Yunlong,et al.Research on new method of tank liquid sloshing test based on air flotation technology[J].Journal of Rocket Propulsion,2017,43(02):47-51.
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利用气浮技术进行贮箱晃动试验方法研究

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 43 期数: 2017年02期 页码: 47-51 栏目: 研究与设计 出版日期: 2017-06-01
Title:
Research on new method of tank liquid sloshing test based on air flotation technology
作者:
程宏川1; 2; 吴 剑1; 2; 廖云龙1; 2; 张银勇1; 2
1.上海空间推进研究所，上海201112；2.上海空间发动机工程技术研究中心，上海201112
Author(s):
CHENG Hongchuan1; 2;  WU Jian1; 2;  LIAO Yunlong1; 2;  ZHANG Yinyong1; 2
1. Shanghai Institute of Space Propulsion, Shanghai 201112, China; 2. Shanghai Engineering Research Center of Space Engine, Shanghai 201112, China
关键词:
贮箱晃动试验; 气垫悬浮技术; CFD仿真计算
Keywords:
tank liquid sloshing test; air cushion flotation technology; CFD simulation calculation
分类号:
V433.9-34
摘要:
针对某型号大容积贮箱,其晃动特性直接影响到整个系统的动力学特性及轨道控制系统.为了获得该贮箱不同工况下的一阶自由晃动频率,首次提出利用气垫悬浮技术进行贮箱晃动试验的新方法,利用该方法设计出一整套试验系统,该系统包含试验件、激励系统、气浮控制系统、数据采集系统及加注排放系统等.使用试验系统开展不同工况条件下的液体晃动试验,并用CFD软件对该贮箱进行时域分析,结合傅立叶变换最终获得仿真结果.分析比较晃动试验结果、理论计算结果及CFD仿真计算结果,结果显示3种结果一致吻合,测试系统的可靠性和理论CFD仿真结果的正确性均得到验证.
Abstract:
The sloshing characteristics of a type of large volume tank affect the whole system dynamic characteristics and orbit control system directly.In order to get the free sloshing frequency of the tank under different working conditions,a new method of tank liquid sloshing test based on air cushion flotation technology is proposed.A set of experiment system,including tank,excitation system,air flotation control system,data acquisition system and filling & draining system,is designed by this method to solve the liquid sloshing problem under different working conditions.The final simulation results were achieved by Fourier transform and time domain simulation analysis results obtained by CFD software.The results indicate that the test result,theory result and the CFD simulation result are consistent,and prove that the test system is reliable and the simulation results of CFD are correct.The test results provide an important reference and supporting data for tank design optimization and launch vehicle attitude & orbit control system design optimization.

参考文献/References:

[1]胡齐, 李永, 姚灿, 等. 大容积推进剂贮箱液体晃动性能试验[J]. 空间控制技术及应用, 2016, 42(3): 44-48．
[2]李青, 王天舒, 马兴瑞. 充液航天器液体晃动和液固耦合动力学的研究及应用[J]. 力学进展, 2012, 42(4): 472- 480．
[3]黄愉太, 杜发喜, 刘海, 等. 基于SPH方法的弹性体贮箱内液体晃动特性分析[J]. 计算机辅助工程, 2015, 24(2): 36-41.
[4]闫锦, 于洪亮, 宋玉超. 矩形液箱内液体晃动分析计算[J]. 大连海事大学学报, 2013, 39(1): 74-77.
[5]李松, 高芳清, 杨翊仁, 等. 液体晃动有限元模型分析及试验研究[J]. 核动力工程, 2007, 28(4): 54-57.
[6]陈健, 范晴云. 贮箱内推进剂微重力下晃动的有限元模拟及试验[J]. 上海航天, 2003 (4): 15-19.
[7]林宏, 彭慧, 董锴. 推进剂贮箱液体晃动的仿真研究与验证[J]. 强度与环境, 2011, 38(5): 25-30.
[8]WU Nanjing, HSIAO Shih-Chun, WU Hanlun. Mesh-free simulation of liquid sloshing subjected to harmonic excitations[J]. Engineering analysis with boundary element, 2016, (64): 90-100.
[9]QJ 2117-91. 地-地导弹、运载火箭液体推进剂晃动设计规范[S]. 北京: 中华人民共和国航空航天工业部, 1991.

备注/Memo

收稿日期：2016-09-21；修回日期：2016-12-16 作者简介：程宏川（1984—），男，工程师，研究领域为结构仿真及应用

更新日期/Last Update: 1900-01-01