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contributor authorAbdallah Bouam
contributor authorSlimane Aissani
contributor authorRabah Kadi
date accessioned2017-05-09T00:27:51Z
date available2017-05-09T00:27:51Z
date copyrightJuly, 2008
date issued2008
identifier issn1528-8919
identifier otherJETPEZ-27026#041701_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/137896
description abstractThe gas turbines are generally used for large scale power generation. The basic gas turbine cycle has low thermal efficiency, which decreases in the hard climatic conditions of operation, so the cycles with thermodynamic improvement is found to be necessary. Among several methods shown their success in increasing the performances, the steam injected gas turbine cycle (STIG) consists of introducing a high amount of steam at various points in the cycle. The main purpose of the present work is to improve the principal characteristics of gas turbine used under hard condition of temperature in Algerian Sahara by injecting steam in the combustion chamber. The suggested method has been studied and compared to a simple cycle. Efficiency, however, is held constant when the ambient temperature increases from ISO conditions to 50°C. Computer program has been developed for various gas turbine processes including the effects of ambient temperature, pressure ratio, injection parameters, standard temperature, and combustion chamber temperature with and without steam injection. Data from the performance testing of an industrial gas turbine, computer model, and theoretical study are used to check the validity of the proposed model. The comparison of the predicted results to the test data is in good agreement. Starting from the advantages, we recommend the use of this method in the industry of hydrocarbons. This study can be contributed for experimental tests.
publisherThe American Society of Mechanical Engineers (ASME)
titleCombustion Chamber Steam Injection for Gas Turbine Performance Improvement During High Ambient Temperature Operations
typeJournal Paper
journal volume130
journal issue4
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2898834
journal fristpage41701
identifier eissn0742-4795
keywordsTemperature
keywordsCombustion chambers
keywordsGas turbines
keywordsSteam AND Pressure
treeJournal of Engineering for Gas Turbines and Power:;2008:;volume( 130 ):;issue: 004
contenttypeFulltext


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