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A numerical study on various pin-fin shaped surface air-oil heat exchangers for an aero gas-turbine engine

机译:航空燃气轮机各种销形表面空气-油热交换器的数值研究

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摘要

In this study, the performance of a surface air-oil heat exchanger for an aero gas-turbine engine having plate- and pin-fin shaped geometries was investigated numerically. Basic heat-transfer and pressure-drop characteristics were examined using a simplified channel model. Performance of pin-shaped fins is compared with that of the plate fin as a baseline. Using a parametric study, optimal fin pitches of the pin-fin geometries in stream- and span-wise directions were determined. Finally, the high-speed bypass effect of the surface air-oil heat exchanger was calculated using the geometry of a real engine. Aero-thermal performance for such as the heat transfer rate, pressure-drop along the bypass stream of the engine, and distorted velocity boundary layer profiles, were evaluated quantitatively. The entropy generation rate due to the surface air-oil heat exchanger is summarized to assess the irreversibility loss inside the bypass stream and the cooler region.
机译:在这项研究中,对具有板翅形和销翅形几何形状的航空燃气涡轮发动机的表面空气-油热交换器的性能进行了数值研究。使用简化的通道模型检查了基本的传热和压降特性。将销形散热片的性能与作为基准的平板散热片的性能进行比较。通过参数研究,确定了沿流向和跨度方向的针式翅片几何形状的最佳翅片间距。最后,使用实际发动机的几何结构计算了地面空气-油热交换器的高速旁路效果。定量评估了空气热性能,例如传热速率,沿发动机旁通流的压降和速度边界层变形的情况。总结归因于地面空气-油热交换器的熵产生速率,以评估旁路流和较冷区域内部的不可逆损失。

著录项

  • 来源
  • 作者单位

    School of Mechanical Engineering, Pusan National University, 2, Busandaehak-ro 63beon-gil, Busan 46241, Republic of Korea;

    School of Mechanical Engineering, Pusan National University, 2, Busandaehak-ro 63beon-gil, Busan 46241, Republic of Korea;

    Rolls-Royce and Pusan National University Technology Centre in Thermal Management, Pusan National University, 2, Busandaehak-ro 63beon-gil, Busan 46241, Republic of Korea;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Surface air-oil heat exchanger; Aero gas-turbine engine; Bypass effect;

    机译:地表油气热交换器;航空燃气涡轮发动机;旁路效果;

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