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船舶燃气轮机双通道进气系统流场特性研究

  • Qi Xin Ma
  • , Tao Pan
  • , Yan Ming Liu*
  • , Yu Fu
  • , Jian Hua Wang
  • *此作品的通讯作者
  • Beijing Institute of Technology
  • Systems Engineering Research Institute of China State Shipbuilding Cooperation

科研成果: 期刊稿件文章同行评审

摘要

A detailed numerical simulation on the flow field of a double-channel intake system is carried out for marine gas turbine by using the method of automatic flow distribution. The flow distribution law of the double-channel intake was explored, the characteristics of the full flow field are analyzed and the system performance is evaluated under the static wind condition of 1.0 state of the sea. The results show that the design of two channel intake system can ensure the flow distribution of upper and lower intake chambers is reasonable, obtain uniform flow in the intake chamber and improve the condition of airflow rush in the shaft. For the total pressure loss of the system, the flow loss accounts for about 47.2%, while the total pressure loss of components accounts for about 52.8%. Additionally, the loss of primary air filter accounts for 45.9% of the total pressure loss of components, which is the main component to produce the total pressure loss. If possible, perforated plate of muffler and shaft shapes can be further optimized to reduce the flow loss. The flow uniformity coefficient of cooling pipe outlet reaches 0.99, which meets the requirement of uniformity degree. When the design length of the volute is greater than 0.6 times of the characteristic length, the flow velocity and total pressure meet the requirement of uniformity. It can be considered that the outlet air flow is uniform.

投稿的翻译标题Investigation on Flow Field Characteristics of a Double-Channel Intake System for Marine Gas Turbine
源语言繁体中文
页(从-至)2508-2516
页数9
期刊Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics
42
10
出版状态已出版 - 10月 2021

联合国可持续发展目标

此成果有助于实现下列可持续发展目标:

  1. 可持续发展目标 14 - 水下生物
    可持续发展目标 14 水下生物

关键词

  • Flow distribution
  • Flow uniformity
  • Marine intake system
  • Total pressure loss

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