海洋温差能发电装置中冷水管动力性能分析
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  • 英文篇名:Dynamics of cold water pipe in ocean thermal energy conversion
  • 作者:司东洋 ; 吕海宁 ; 陈刚 ; 肖龙飞
  • 英文作者:SI Dongyang;LV Haining;CHEN Gang;XIAO Longfei;State Key Laboratory of Ocean Engineering,Shanghai Jiao Tong University;Collaborative Innovation Center for Advanced Ship and Deep-Sea Exploration (CISSE);Marine Design & Research Institute of China;
  • 关键词:冷水管 ; 动态失稳 ; 进流口流场参数 ; 临界流速 ; 进流口压降 ; 海洋温差能 ; 稳定性分析
  • 英文关键词:cold water pipe;;flutter;;inlet flow-field parameter;;critical fluid velocity;;inlet depressurisation;;ocean thermal energy;;stability analysis
  • 中文刊名:HYGC
  • 英文刊名:The Ocean Engineering
  • 机构:上海交通大学海洋工程国家重点实验室;高新船舶与深海开发装备协同创新中心;中国船舶及海洋工程设计研究院;
  • 出版日期:2019-05-30
  • 出版单位:海洋工程
  • 年:2019
  • 期:v.37
  • 基金:国家重点研发计划课题“深海多金属结核采矿试验工程-水下输送系统开发”(2016YFC0304103);; 工信部深水半潜式支持平台研发专项经费资助(工信部联装函【2016】546号)
  • 语种:中文;
  • 页:HYGC201903014
  • 页数:8
  • CN:03
  • ISSN:32-1423/P
  • 分类号:124-131
摘要
不考虑波浪、海流以及平台运动的作用,研究管内流动对冷水管动力性能的影响。基于悬臂输液管道梁模型,通过轴向流速比α、流速角比ψ和切向流速比φ三个进流口流场参数描述自由端边界条件,获得冷水管在内流作用下的控制方程。从流体动力项对管道做功的角度分析发现,φ对管道失稳的临界流速有很大的影响,并且φ=0被认为是对进流口流场的正确描述;然而,通过Galerkin法分析发现,φ=0的进流口流场模型不能解释进流口压降Δp对动态失稳基本没有影响的试验现象。相反,φ≠0的进流口流场模型在使得进流口压降Δp的影响几乎为零的同时,还能够获得较大的临界流速,与Kuiper观察的试验现象相符。切向流速比φ的正确评估是准确预测临界流速的前提条件。
        Regardless of the role of waves,currents,and platform motions,the effect of the internal flow on the dynamics of the cold water pipe is studied. Based on the cantilevered conveying fluid pipe's beam model,the boundary condition at the free end is described by the axial flow velocity ratio α,the flow angle ratio ψ and the tangential flow velocity ratio φ,and the governing equation of the cold water pipe under the action of internal flow is obtained. From the perspective of the work done on the pipe by the fluid-dynamics forces,it is found that φ has a great influence on the critical flow velocity of the pipe instability,and φ = 0 is considered as the correct description of the inlet flow field. However,by the Galerkin method,the inlet flow-field model with φ = 0 cannot explain the experimental phenomenon that the inlet depressurisation Δp has almost no effect on the flutter. On the contrary,the inlet flow field model of φ ≠ 0 makes the influence of the depressurisation Δp almost zero,and also obtains a larger critical flow velocity,which is consistent with the experimental phenomenon observed by Kuiper. The correct assessment of φ is a prerequisite for accurately predicting the critical flow velocity.
引文
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