Numerical Study on Vortex Structures and Loss Characteristics in a Transonic Turbine with Various Squealer Tips

Cavity width and height are two key geometric parameters of squealer tips, which could affect the control effect of squealer tips on tip leakage flow (TLF) of gas turbines. To explore the optimal values and the control mechanisms of cavity width and height, various cases with different cavity widths...

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Published in:Energies
Main Authors: Yufan Wang, Weihao Zhang, Dongming Huang, Shoumin Jiang, Yun Chen
Format: Article
Language:English
Published: MDPI AG 2022-01-01
Subjects:
Online Access:https://www.mdpi.com/1996-1073/15/3/1018
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author Yufan Wang
Weihao Zhang
Dongming Huang
Shoumin Jiang
Yun Chen
author_facet Yufan Wang
Weihao Zhang
Dongming Huang
Shoumin Jiang
Yun Chen
author_sort Yufan Wang
collection DOAJ
container_title Energies
description Cavity width and height are two key geometric parameters of squealer tips, which could affect the control effect of squealer tips on tip leakage flow (TLF) of gas turbines. To explore the optimal values and the control mechanisms of cavity width and height, various cases with different cavity widths and heights are investigated by solving the steady Reynolds Averaged Navier–Stokes (RANS) equations. In this study, the range of cavity width is 9.2–15.1 <i>τ</i>, and that of cavity height is 1.0–3.5 <i>τ</i>. The results show that the optimal value of cavity height is 2.5–3.0 <i>τ</i>, and that of cavity width is about 10.0–10.5 <i>τ</i>. The small cavity width could restrain the breakdown of tip leakage vortex (TLV) and reduce the extra mixing loss. Both small cavity width and large cavity height could enhance the blocking effect on the TLF, reducing the corresponding mixing loss. However, both of them will inhibit the length of the scraping vortex (SV), which is bad for the control of loss. In addition, large cavity height could reduce the loss inside the clearance, while small cavity width could not. This work could provide a reference for the design of squealer tip.
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spelling doaj-art-e2dfe0ba3dc641dab348fafab64abd252025-08-20T00:04:52ZengMDPI AGEnergies1996-10732022-01-01153101810.3390/en15031018Numerical Study on Vortex Structures and Loss Characteristics in a Transonic Turbine with Various Squealer TipsYufan Wang0Weihao Zhang1Dongming Huang2Shoumin Jiang3Yun Chen4National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, School of Energy & Power Engineering, Beihang University, Beijing 100191, ChinaNational Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, School of Energy & Power Engineering, Beihang University, Beijing 100191, ChinaNational Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, School of Energy & Power Engineering, Beihang University, Beijing 100191, ChinaAECC Shenyang Engine Research Institute, Shenyang 110015, ChinaAECC Shenyang Engine Research Institute, Shenyang 110015, ChinaCavity width and height are two key geometric parameters of squealer tips, which could affect the control effect of squealer tips on tip leakage flow (TLF) of gas turbines. To explore the optimal values and the control mechanisms of cavity width and height, various cases with different cavity widths and heights are investigated by solving the steady Reynolds Averaged Navier–Stokes (RANS) equations. In this study, the range of cavity width is 9.2–15.1 <i>τ</i>, and that of cavity height is 1.0–3.5 <i>τ</i>. The results show that the optimal value of cavity height is 2.5–3.0 <i>τ</i>, and that of cavity width is about 10.0–10.5 <i>τ</i>. The small cavity width could restrain the breakdown of tip leakage vortex (TLV) and reduce the extra mixing loss. Both small cavity width and large cavity height could enhance the blocking effect on the TLF, reducing the corresponding mixing loss. However, both of them will inhibit the length of the scraping vortex (SV), which is bad for the control of loss. In addition, large cavity height could reduce the loss inside the clearance, while small cavity width could not. This work could provide a reference for the design of squealer tip.https://www.mdpi.com/1996-1073/15/3/1018squealer tiptip leakage flowtip leakage lossvortex breakdowntransonic turbine
spellingShingle Yufan Wang
Weihao Zhang
Dongming Huang
Shoumin Jiang
Yun Chen
Numerical Study on Vortex Structures and Loss Characteristics in a Transonic Turbine with Various Squealer Tips
squealer tip
tip leakage flow
tip leakage loss
vortex breakdown
transonic turbine
title Numerical Study on Vortex Structures and Loss Characteristics in a Transonic Turbine with Various Squealer Tips
title_full Numerical Study on Vortex Structures and Loss Characteristics in a Transonic Turbine with Various Squealer Tips
title_fullStr Numerical Study on Vortex Structures and Loss Characteristics in a Transonic Turbine with Various Squealer Tips
title_full_unstemmed Numerical Study on Vortex Structures and Loss Characteristics in a Transonic Turbine with Various Squealer Tips
title_short Numerical Study on Vortex Structures and Loss Characteristics in a Transonic Turbine with Various Squealer Tips
title_sort numerical study on vortex structures and loss characteristics in a transonic turbine with various squealer tips
topic squealer tip
tip leakage flow
tip leakage loss
vortex breakdown
transonic turbine
url https://www.mdpi.com/1996-1073/15/3/1018
work_keys_str_mv AT yufanwang numericalstudyonvortexstructuresandlosscharacteristicsinatransonicturbinewithvarioussquealertips
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AT dongminghuang numericalstudyonvortexstructuresandlosscharacteristicsinatransonicturbinewithvarioussquealertips
AT shouminjiang numericalstudyonvortexstructuresandlosscharacteristicsinatransonicturbinewithvarioussquealertips
AT yunchen numericalstudyonvortexstructuresandlosscharacteristicsinatransonicturbinewithvarioussquealertips