Effect of Bolts on Flow and Heat Transfer in a Rotor-Stator Disk Cavity

被引:3
|
作者
Mohamed, Sulfickerali Noor [1 ]
Chew, John W. [1 ]
Hills, Nicholas J. [1 ]
机构
[1] Univ Surrey, Fac Engn & Phys Sci, Thermofluid Syst UTC, Guildford GU2 7XH, Surrey, England
关键词
gas turbine; internal air systems; unsteady flow; heat transfer; URANS; aero-engine; rotor-stator disk cavity; bolts; RIM SEAL; PREDICTION;
D O I
10.1115/1.4035144
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Previous studies have indicated some differences between steady computational fluid dynamics (CFD) predictions of flow in a rotor-stator disk cavity with rotating bolts compared to measurements. Recently, time-dependent CFD simulations have revealed the unsteadiness present in the flow and have given improved agreement with measurements. In this paper, unsteady Reynolds averaged Navier-Stokes (URANS) 360 deg model CFD calculations of a rotor-stator cavity with rotor bolts were performed in order to better understand the flow and heat transfer within a disk cavity previously studied experimentally by other workers. It is shown that the rotating bolts generate unsteadiness due to wake shedding which creates time-dependent flow patterns within the cavity. At low throughflow conditions, the unsteady flow significantly increases the average disk temperature. A systematic parametric study is presented giving insight into the influence of number of bolts, mass flow rate, cavity gap ratio, and the bolts-to-shroud gap ratio on the time-dependent flow within the cavity.
引用
收藏
页数:9
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