Heat transfer for gas turbine internal cooling

High turbine inlet temperature is required for an efficient gas turbine engine. To maximise the turbine temperature, the internal channel of a turbine blade consists of rib-turbulators to enhance the heat transfer of the cooling air. This report focus on the effect of various rib configurations on c...

Full description

Saved in:
Bibliographic Details
Main Author: Ng, Chean Yuan
Other Authors: Chow Wai Tuck
Format: Final Year Project
Language:English
Published: 2018
Subjects:
Online Access:http://hdl.handle.net/10356/74952
Tags: Add Tag
No Tags, Be the first to tag this record!
Institution: Nanyang Technological University
Language: English
id sg-ntu-dr.10356-74952
record_format dspace
spelling sg-ntu-dr.10356-749522023-03-04T18:57:39Z Heat transfer for gas turbine internal cooling Ng, Chean Yuan Chow Wai Tuck School of Mechanical and Aerospace Engineering DRNTU::Engineering High turbine inlet temperature is required for an efficient gas turbine engine. To maximise the turbine temperature, the internal channel of a turbine blade consists of rib-turbulators to enhance the heat transfer of the cooling air. This report focus on the effect of various rib configurations on cooling performance of internal channel of a turbine blade. High thermal hydraulic performance (THP) for a ribbed channel is desired to have good cooling performance. There are 6 types of different rib configurations in this study, that are square-extruded rib, cylinder-extruded rib, V-extruded rib, W-extruded rib, Jigsaw-extruded rib and 60˚-extruded rib. The averaged friction factor and Nusselt number in fully-developed region was determined at Reynolds number of 30,000 to calculate THP. Square-extruded rib and cylinder-extruded rib were further modified to have different base height and rib height to investigate its effect on THP. Uniform heat flux of 950W/m2 was supplied on both the bottom and upper ribbed walls. K-omega SST turbulence model in CFD Fluent was utilised to simulate the flow inside the internal channel. Results shows that square-extruded rib increases the THP value by 1.838% compared to the baseline channel. Besides that, an averaged Nusselt number between ribs in the fully-developed region for square-extruded and cylinder-extruded rib is also higher. Although increasing base height or extruded height raises averaged Nu values, their THP value drops by 7% due to the simultaneous increase in friction factor. Lastly, the V-extruded and W-extruded ribs have highest averaged Nu values among test channels yet their THP values are the lowest of values around 0.61 among test channel which makes them poor cooling channel design. Bachelor of Engineering (Aerospace Engineering) 2018-05-25T04:45:02Z 2018-05-25T04:45:02Z 2018 Final Year Project (FYP) http://hdl.handle.net/10356/74952 en Nanyang Technological University 71 p. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering
spellingShingle DRNTU::Engineering
Ng, Chean Yuan
Heat transfer for gas turbine internal cooling
description High turbine inlet temperature is required for an efficient gas turbine engine. To maximise the turbine temperature, the internal channel of a turbine blade consists of rib-turbulators to enhance the heat transfer of the cooling air. This report focus on the effect of various rib configurations on cooling performance of internal channel of a turbine blade. High thermal hydraulic performance (THP) for a ribbed channel is desired to have good cooling performance. There are 6 types of different rib configurations in this study, that are square-extruded rib, cylinder-extruded rib, V-extruded rib, W-extruded rib, Jigsaw-extruded rib and 60˚-extruded rib. The averaged friction factor and Nusselt number in fully-developed region was determined at Reynolds number of 30,000 to calculate THP. Square-extruded rib and cylinder-extruded rib were further modified to have different base height and rib height to investigate its effect on THP. Uniform heat flux of 950W/m2 was supplied on both the bottom and upper ribbed walls. K-omega SST turbulence model in CFD Fluent was utilised to simulate the flow inside the internal channel. Results shows that square-extruded rib increases the THP value by 1.838% compared to the baseline channel. Besides that, an averaged Nusselt number between ribs in the fully-developed region for square-extruded and cylinder-extruded rib is also higher. Although increasing base height or extruded height raises averaged Nu values, their THP value drops by 7% due to the simultaneous increase in friction factor. Lastly, the V-extruded and W-extruded ribs have highest averaged Nu values among test channels yet their THP values are the lowest of values around 0.61 among test channel which makes them poor cooling channel design.
author2 Chow Wai Tuck
author_facet Chow Wai Tuck
Ng, Chean Yuan
format Final Year Project
author Ng, Chean Yuan
author_sort Ng, Chean Yuan
title Heat transfer for gas turbine internal cooling
title_short Heat transfer for gas turbine internal cooling
title_full Heat transfer for gas turbine internal cooling
title_fullStr Heat transfer for gas turbine internal cooling
title_full_unstemmed Heat transfer for gas turbine internal cooling
title_sort heat transfer for gas turbine internal cooling
publishDate 2018
url http://hdl.handle.net/10356/74952
_version_ 1759856502142664704