Volume 35 Issue 12
Dec.  2020
Turn off MathJax
Article Contents
HU Zhenggen, ZHAN Lihua, DONG Manhong. Effect of weld reinforcement methods on bearing performance of large diameter tank bottom[J]. Journal of Aerospace Power, 2020, 35(12): 2681-2688. doi: 10.13224/j.cnki.jasp.2020.12.022
Citation: HU Zhenggen, ZHAN Lihua, DONG Manhong. Effect of weld reinforcement methods on bearing performance of large diameter tank bottom[J]. Journal of Aerospace Power, 2020, 35(12): 2681-2688. doi: 10.13224/j.cnki.jasp.2020.12.022

Effect of weld reinforcement methods on bearing performance of large diameter tank bottom

doi: 10.13224/j.cnki.jasp.2020.12.022
  • Received Date: 2020-08-23
  • Publish Date: 2020-12-28
  • Based on the finite element method, the influence of weld reinforcement methods (double symmetry reinforcement, inner surface reinforcement,outside surface reinforcement) on internal pressure bearing capacity of typical 10 m class diameter tank bottom was studied. The two-dimensional symmetric plane model was used for numerical calculation, and the effects of the real boundary conditions of the tube segment and the short shell and the weld on the bearing capacity were considered. The nonlinear numerical analysis model considering the plasticity of the material was constructed to accurately obtain the meridional stress on the inner and outer surfaces of tank bottom. Results showed that the weld area of the top and melon flap was a weak area of tank bottom. Under operating pressure, meridional stress difference between inner and outside surfaces of double symmetric reinforcement was smallest, and none of them presented plasticity. Meridional stress difference of single-side reinforcement was much larger than double symmetric reinforcement, and local plasticity occurred. Compared with inner surface reinforcement, the maximum and minimum meridional stress differences of outside surface reinforcement increased by 9.7% and 27.2%, and all of them led to uncoordinated deformation. Under design pressure, inner and outside surface meridional stress of tank bottom had local plasticity, and material plasticity had certain coordination effect on the inner and outside surface meridional stress difference, which can significantly alleviate the additional bending moment caused by the inner and outside surface stress difference. Double symmetric reinforcement was better than outside surface reinforcement, and inner surface reinforcement was better than outside surface reinforcement. The single-side reinforcement was easy to generate additional bending moment, which was not conducive to the uniform bearing and deformation coordination of tank bottom. The research results provide a guidance to the optimization design of the bottom structure of large diameter storage tank.

     

  • loading
  • [1]
    吴会强,黄诚,常志龙.国外大型贮箱结构研制现状及展望[J].宇航材料工艺,2014,44(增刊1):7-13. WU Huiqiang,HUANG Cheng,CHANG Zhilong.Recent progress and prospects of large foreign tank structure[J].Aerospace Materials and Technology,2014,44(Suppl.1):7-13.(in Chinese)
    [2]
    王国庆,李曙光,吴会强.重型火箭贮箱大型结构制造技术现状及发展分析[J].宇航材料工艺,2014,44(增刊1):1-6. WANG Guoqing,LI Shuguang,WU Huiqiang.Status and development analyses on manufacturing technologies for large scale structures of heavy-lift launch vehicle propellant tanks[J].Aerospace Materials and Technology,2014,44(Suppl.1):1-6.(in Chinese)
    [3]
    MESCALL J.Stability of thin torispherical shells under uniform internal pressure[R].NASA TN D-1510,1962.
    [4]
    ADACHI J,BENICEK M.Buckling of torispherical shells under internal pressure[J].Experimental Mechanics,1964,4(8):217-222.
    [5]
    MICHAEL P N,RICHARD D Y,TIMOTHY J C,et al.Nonlinear analysis of the space shuttle superlight weight LO2 tank:Part Ⅱ behavior under 3g end-of-flight loads[R].NASA/TM-1998-207287,1998.
    [6]
    RICHARD D Y,MICHAEL P N,TIMOTHY J C,et al.Nonlinear analysis of the space shuttle superlight weight LO2 tank:Part Ⅰ behavior under booster ascent loads[R].NASA/TM-1998-208127,1998.
    [7]
    NEMETH M P,BRITT V O,COLLINS T J,et al.Nonlinear analysis of the space shuttle superlight weight external fuel tank[R].NASA-TM-112151,1996.
    [8]
    AHMED R,WILHELM J.Analysis and test of low profile aluminum aerospace tank dome[R].NASA-TP-3442,1993.
    [9]
    WILLIAM L.Structural analysis of helios filament wound tanks subjected to internal pressure and cooling[R].NASA/TM-2005-212855,2005.
    [10]
    THEODORE F J,DAVID W S,ROBERT A M.Structures and design phase Ⅰ summary for the NASA composite cryotank technology demonstration project[R].AIAA 2013-1825,2013.
    [11]
    DAVID W S,ROBERT A M,THEODORE F J.Structural design and sizing of a metallic cryotank concept[R].AIAA 2013-1844,2013.
    [12]
    周广文.推进剂贮箱优化设计的思考[J].导弹与航天运载技术,2011(1):26-28. ZHOU Guangwen.Optimal structure design for launch vehicle tank[J].Missiles and Space Vehicles,2011(1):26-28.(in Chinese)
    [13]
    章凌,黄诚,方岱宁,等.大型薄壁贮箱焊接区等应力优化设计[J].应用力学学报,2015,32(4):593-596. ZHANG Ling,HUANG Cheng,FANG Daining et al.Optimized design of welding area of large thin wall storage tank[J].Chinese Journal of Applied Mechanics,2015,32(4):593-596.(in Chinese)
    [14]
    王博,赵亮,郝鹏,等.改善贮箱Y形环焊缝应力水平的优化设计[J].宇航材料工艺,2014,44(增刊1):26-28. WANG Bo,ZHAO liang,HAO Peng,et al.Optimization of improving Y-ring welding stress level for tanks[J].Aerospace Materials and Technology,2014,44(Suppl.1):26-28.(in Chinese)
    [15]
    黄诚,胡正根,马云龙,等.筒段边界对大直径贮箱椭球箱底的内压稳定性影响研究[J].强度与环境,2015,42(5):19-26. HUANG Cheng,HU Zhenggen,MA Yunlong,et al.Impact study of shell segment boundary on internal pressure stability of the large diameter tank ellipsoid bottom[J].Structure and Environment Engineering,2015,42(5):19-26.(in Chinese)
    [16]
    黄诚,胡正根,常志龙,等.大直径贮箱三心箱底内压作用下的力学性能分析[J].强度与环境,2016,43(6).19-26. HUANG Cheng,HU Zhenggen,CHANG Zhilong,et al.Mechanical properties analysis of three-center bottom of the large diameter tank on internal pressure[J].Structure and Environment Engineering,2016,43(6):19-26.(in Chinese)
    [17]
    胡正根,黄诚,常志龙,等.基于缺陷敏感性的大直径贮箱椭球箱底内压稳定性研究[J].强度与环境,2017,44(5):19-26. HU Zhenggen,HUANG Cheng,CHANG Zhilong,et al.Analysis of the internal pressure stability on the large diameter tank ellipsoid bottom based on imperfection sensitivity[J].Structure and Environment Engineering,2017,44(5):19-26.(in Chinese)
    [18]
    辛腾达,王华,崔村燕,等.贮箱轻量化设计几何参数优化方法[J].西安交通大学学报,2019,53(7):153-159. XIN Tengda,WANG Hua,CUI Cunyan,et al.Geometric parameters optimization for tank lightweight design[J].Journal of Xi’an Jiaotong University,2019,53(7):153-159.(in Chinese)
    [19]
    赵亮.大直径薄壁箱体结构力学分析与精细优化设计[D].辽宁 大连:大连理工大学,2015. ZHAO Liang.The mechanical anslysis and refined optimization of large diameter and thin walled tank structures[D].Dalian Liaoning:Dalian University of Technology,2015.(in Chinese)
    [20]
    朱天宇.大型共底贮箱结构优化设计[D].辽宁 大连:大连理工大学,2018. ZHU Tianyu.Optimum design of large coplanar tank structures[D].Dalian Liaoning:Dalian University of Technology,2018.(in Chinese)
    [21]
    王鹏.传递发动机推力的贮箱箱底结构研究[D].北京:中国运载火箭技术研究院,2019. WANG Peng.Structural research propellant tank aft dome transmitting engine thrust[D].Beijing:China Academy of Launch Vehicle Technology,2019.(in Chinese)
    [22]
    周家麟.推进剂金属贮箱设计规范:Q/Dy 350-1995[S].北京:中国运载火箭技术研究院,1995:1-76.
    [23]
    利津,皮亚特金.薄壁结构设计[M].廖启端,王敬春,王其兴,等译.北京:国防工业出版社,1983.
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (223) PDF downloads(127) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return