Design and Numerical Analysis of a Vane Shaped Receiver Hole in a Cover-Plate Preswirl SystemSource: Journal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 004::page 41001DOI: 10.1115/1.4041628Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: In a cover-plate system, rotating receiver hole is an important component, because its structure and characteristics directly influence the aerodynamic loss and cooling performance in the preswirl system. A new type of vane shaped (VS) receiver hole was designed and presented in this paper. Numerical simulations were carried out to compare the performances among high-radius direct transfer system (model-A), low-radius cover-plate system with simple drilled (SD) receiver holes (model-B), and low-radius cover-plate system with VS receiver holes (model-C). Results indicate that for the operating conditions simulated here, temperature drop effectiveness of the high-radius preswirl system is much better compared to the low-radius system with SD receiver hole. With VS receiver hole, the aerodynamic loss in model-C is the lowest. The nondimensional static pressure at preswirl nozzle exit is only 0.93, around 10% lower than model-B. Moreover, it has a more remarkable cooling performance. The temperature drop effectiveness of model-C can be as high as 0.52, around 67.7% higher compared to model-A. The system with VS receiver hole could not only realize the advantage of low leakage flow as a low-radius system, but also could achieve higher temperature drop compared to high-radius system.
|
Show full item record
contributor author | Liu, Yuxin | |
contributor author | Liu, Gaowen | |
contributor author | Kong, Xiaozhi | |
contributor author | Wang, Yangang | |
date accessioned | 2019-03-17T10:42:33Z | |
date available | 2019-03-17T10:42:33Z | |
date copyright | 11/1/2018 12:00:00 AM | |
date issued | 2019 | |
identifier issn | 0742-4795 | |
identifier other | gtp_141_04_041001.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4256275 | |
description abstract | In a cover-plate system, rotating receiver hole is an important component, because its structure and characteristics directly influence the aerodynamic loss and cooling performance in the preswirl system. A new type of vane shaped (VS) receiver hole was designed and presented in this paper. Numerical simulations were carried out to compare the performances among high-radius direct transfer system (model-A), low-radius cover-plate system with simple drilled (SD) receiver holes (model-B), and low-radius cover-plate system with VS receiver holes (model-C). Results indicate that for the operating conditions simulated here, temperature drop effectiveness of the high-radius preswirl system is much better compared to the low-radius system with SD receiver hole. With VS receiver hole, the aerodynamic loss in model-C is the lowest. The nondimensional static pressure at preswirl nozzle exit is only 0.93, around 10% lower than model-B. Moreover, it has a more remarkable cooling performance. The temperature drop effectiveness of model-C can be as high as 0.52, around 67.7% higher compared to model-A. The system with VS receiver hole could not only realize the advantage of low leakage flow as a low-radius system, but also could achieve higher temperature drop compared to high-radius system. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Design and Numerical Analysis of a Vane Shaped Receiver Hole in a Cover-Plate Preswirl System | |
type | Journal Paper | |
journal volume | 141 | |
journal issue | 4 | |
journal title | Journal of Engineering for Gas Turbines and Power | |
identifier doi | 10.1115/1.4041628 | |
journal fristpage | 41001 | |
journal lastpage | 041001-10 | |
tree | Journal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 004 | |
contenttype | Fulltext |