Models for the Prediction of Transients in Closed Regenerative Gas Turbine Cycles With Centrifugal ImpellersSource: Journal of Engineering for Gas Turbines and Power:;2005:;volume( 127 ):;issue: 003::page 505Author:Theodosios Korakianitis
,
James Watt Professor of Mechanical Engineering
,
N. E. Vlachopoulos
,
D. Zou
DOI: 10.1115/1.1806450Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This paper presents transient-flow component models for the prediction of the transient response of gas turbine cycles. The application is to predict the transient response of a small solar-powered regenerative gas-turbine engine with centrifugal impellers. The component sizes are similar to those under consideration for the solar-powered Space Station, but the models can easily be generalized for other applications with axial or mixed-flow turbomachinery. New component models for the prediction of the propagation of arbitrary transients in centrifugal impellers are developed. These are coupled with component models for the heat exchangers, receiver and radiator. The models are based on transient applications of the principles of conservation of mass, energy, and momentum. System transients driven by sinusoidal and double-step inputs in receiver salt temperature are presented and discussed. The new turbomachinery models and their coupling to the heat-exchanger models simulates disturbance-propagation in the components both upstream and downstream from the point of generation. This permits the study of the physical mechanisms of generation and propagation of higher-frequency contents in the response of the cycle.
keyword(s): Flow (Dynamics) , Compressors , Impellers , Gas turbines , Heat exchangers , Turbines , Cycles , Turbomachinery , Temperature , Fluids , Engines , Space stations AND Steady state ,
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contributor author | Theodosios Korakianitis | |
contributor author | James Watt Professor of Mechanical Engineering | |
contributor author | N. E. Vlachopoulos | |
contributor author | D. Zou | |
date accessioned | 2017-05-09T00:16:05Z | |
date available | 2017-05-09T00:16:05Z | |
date copyright | July, 2005 | |
date issued | 2005 | |
identifier issn | 1528-8919 | |
identifier other | JETPEZ-26871#505_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/131760 | |
description abstract | This paper presents transient-flow component models for the prediction of the transient response of gas turbine cycles. The application is to predict the transient response of a small solar-powered regenerative gas-turbine engine with centrifugal impellers. The component sizes are similar to those under consideration for the solar-powered Space Station, but the models can easily be generalized for other applications with axial or mixed-flow turbomachinery. New component models for the prediction of the propagation of arbitrary transients in centrifugal impellers are developed. These are coupled with component models for the heat exchangers, receiver and radiator. The models are based on transient applications of the principles of conservation of mass, energy, and momentum. System transients driven by sinusoidal and double-step inputs in receiver salt temperature are presented and discussed. The new turbomachinery models and their coupling to the heat-exchanger models simulates disturbance-propagation in the components both upstream and downstream from the point of generation. This permits the study of the physical mechanisms of generation and propagation of higher-frequency contents in the response of the cycle. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Models for the Prediction of Transients in Closed Regenerative Gas Turbine Cycles With Centrifugal Impellers | |
type | Journal Paper | |
journal volume | 127 | |
journal issue | 3 | |
journal title | Journal of Engineering for Gas Turbines and Power | |
identifier doi | 10.1115/1.1806450 | |
journal fristpage | 505 | |
journal lastpage | 513 | |
identifier eissn | 0742-4795 | |
keywords | Flow (Dynamics) | |
keywords | Compressors | |
keywords | Impellers | |
keywords | Gas turbines | |
keywords | Heat exchangers | |
keywords | Turbines | |
keywords | Cycles | |
keywords | Turbomachinery | |
keywords | Temperature | |
keywords | Fluids | |
keywords | Engines | |
keywords | Space stations AND Steady state | |
tree | Journal of Engineering for Gas Turbines and Power:;2005:;volume( 127 ):;issue: 003 | |
contenttype | Fulltext |