海洋工程装备与技术 ›› 2014, Vol. 1 ›› Issue (1): 55-61.

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超大型储液舱内晃荡载荷实验研究

卫志军1, 阮诗伦1, 岳前进1, 谢彬2   

  1. 1. 大连理工大学工业装备结构分析国家重点实验室, 辽宁 大连 116024
    2. 中海油研究总院, 北京 100027
  • 收稿日期:2014-01-23 出版日期:2014-01-30 发布日期:2017-12-07
  • 作者简介:

    卫志军(1985--), 女, 博士研究生, 主要从事超大型储液舱内晃荡冲击载荷及其抑制研究.

  • 基金资助:
    国家科技重大专项(2011ZX05026-006-06);国家自然科学基金创新研究群体项目(50921001)

Experimental Investigation of Liquid Sloshing Impact Load in a Large-Scale Prismatic Tank

Zhi-jun WEI1, Shi-lun RUAN1, Qian-jin YUE1, Bin XIE2   

  1. 1. State Key Laboratory of Sturcutral Analysis for Industrial Equipment, Dalian University of Technology, Dalian, Liaoning 116024, China
    2. CNOOC Research Institute, Beijing 100027, China
  • Received:2014-01-23 Online:2014-01-30 Published:2017-12-07

摘要:

超大型浮式液化天然气船薄膜型液舱内液体晃荡载荷是一个关键问题.采用实验方法研究纵荡,横荡和横摇下储舱内晃荡荷载的分布规律, 具体包括冲击载荷的时程分析,最大冲击荷载分布规律和其对应的危险载液率.在室内开展大比尺八边形模型液体晃荡实验, 采用阵列式布置压力传感器监测冲击压力的变化及其分布特性.实验结果表明: 60%~70%为最危险载液率, 液舱外形曲率突变的位置冲击压力较大.研究结果可为液舱结构加强设计及分析提供依据.

关键词: 晃荡载荷, 大比尺模型实验, 冲击压力, 激励, 危险载液率

Abstract:

Liquid sloshing load is one of the key issues in the design of the cargo container system of the very large-scale floating liquefied natural gas (FLNG) facility. Experimental investigation on liquid slamming in a large-scale prismatic tank under sway, surge, and roll excitations is performed, aiming at the time history of slamming pressure, the distribution of the largest impact pressure and the most serious filling rates. A series of experiments in a large-scale prismatic model is carried out. Pressure sensor array is employed to record the variation of impact pressure. The experimental results illustrate that the value between 60%~70% is the most serious filling rate. Furthermore, the position with change of curvature along the bulkhead is found to be the most serious position for tank structure. The results are useful for the research and design associated with slamming load in prismatic tank.

Key words: sloshing load, large-scale model experiment, slamming pressure, excitation, the most serious filling rate

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