Solid-fluid interactions for internal cooling in a turbine blade

To achieve higher overall efficiency of aircraft engines, turbine blades are subjected to higher temperatures. Thus, more efficient cooling methods are required. The use of ribbed turbulators is one of the technologies for cooling. It induces turbulence in the cooling air to increase heat transferre...

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Main Author: Loy, Hong Tat
Other Authors: Chow Wai Tuck
Format: Final Year Project
Language:English
Published: Nanyang Technological University 2020
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Online Access:https://hdl.handle.net/10356/141880
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-1418802023-03-04T18:49:08Z Solid-fluid interactions for internal cooling in a turbine blade Loy, Hong Tat Chow Wai Tuck School of Mechanical and Aerospace Engineering wtchow@ntu.edu.sg Engineering::Aeronautical engineering To achieve higher overall efficiency of aircraft engines, turbine blades are subjected to higher temperatures. Thus, more efficient cooling methods are required. The use of ribbed turbulators is one of the technologies for cooling. It induces turbulence in the cooling air to increase heat transferred from the metal. To obtain greater cooling effect, past researches focused on inducing higher levels of turbulence in the cooling air with different rib configurations. These studies showed that the V ribs had excellent heat transfer capability, yet it was never used in turbine blades. This could be due to an overall increased stress concentration of the V rib on creep and fatigue performances. This research is thus focused on (1) building the bridge to translate the heat transfer performance of the V ribs in terms of creep and fatigue performances and (2) coming up with a design that reconciled enhanced heat transfer and structural performances. Through conjugate analysis, Computational Fluid Dynamics (CFD) results showed a ~140K reduction in temperature for the V ribs compared to the straight ribs. The reduced temperature led to improved creep performance, with a 83.2% reduction in creep strain for the V ribs. However, it experienced a 31.2% increase in stress and a 32.8% reduction in fatigue life compared to the straight ribs. To improve structural performance and retain the enhanced heat transfer characteristics, the V with spine configuration was designed. This design achieved a 4.17% reduction in stress level with similar enhanced heat transfer capability, when compared to the V ribs. Further improvements made to this novel design allowed it to achieve a stress level of 901MPa (~9% reduction in stress level compared to V ribs). Overall, the fatigue life of the improved V with spine increased by 20.1% from that of the V ribs. Both enhanced heat transfer and structural performances were achieved through this design. Bachelor of Engineering (Aerospace Engineering) 2020-06-11T06:57:21Z 2020-06-11T06:57:21Z 2020 Final Year Project (FYP) https://hdl.handle.net/10356/141880 en A146 application/pdf Nanyang Technological University
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic Engineering::Aeronautical engineering
spellingShingle Engineering::Aeronautical engineering
Loy, Hong Tat
Solid-fluid interactions for internal cooling in a turbine blade
description To achieve higher overall efficiency of aircraft engines, turbine blades are subjected to higher temperatures. Thus, more efficient cooling methods are required. The use of ribbed turbulators is one of the technologies for cooling. It induces turbulence in the cooling air to increase heat transferred from the metal. To obtain greater cooling effect, past researches focused on inducing higher levels of turbulence in the cooling air with different rib configurations. These studies showed that the V ribs had excellent heat transfer capability, yet it was never used in turbine blades. This could be due to an overall increased stress concentration of the V rib on creep and fatigue performances. This research is thus focused on (1) building the bridge to translate the heat transfer performance of the V ribs in terms of creep and fatigue performances and (2) coming up with a design that reconciled enhanced heat transfer and structural performances. Through conjugate analysis, Computational Fluid Dynamics (CFD) results showed a ~140K reduction in temperature for the V ribs compared to the straight ribs. The reduced temperature led to improved creep performance, with a 83.2% reduction in creep strain for the V ribs. However, it experienced a 31.2% increase in stress and a 32.8% reduction in fatigue life compared to the straight ribs. To improve structural performance and retain the enhanced heat transfer characteristics, the V with spine configuration was designed. This design achieved a 4.17% reduction in stress level with similar enhanced heat transfer capability, when compared to the V ribs. Further improvements made to this novel design allowed it to achieve a stress level of 901MPa (~9% reduction in stress level compared to V ribs). Overall, the fatigue life of the improved V with spine increased by 20.1% from that of the V ribs. Both enhanced heat transfer and structural performances were achieved through this design.
author2 Chow Wai Tuck
author_facet Chow Wai Tuck
Loy, Hong Tat
format Final Year Project
author Loy, Hong Tat
author_sort Loy, Hong Tat
title Solid-fluid interactions for internal cooling in a turbine blade
title_short Solid-fluid interactions for internal cooling in a turbine blade
title_full Solid-fluid interactions for internal cooling in a turbine blade
title_fullStr Solid-fluid interactions for internal cooling in a turbine blade
title_full_unstemmed Solid-fluid interactions for internal cooling in a turbine blade
title_sort solid-fluid interactions for internal cooling in a turbine blade
publisher Nanyang Technological University
publishDate 2020
url https://hdl.handle.net/10356/141880
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