A Procedure for Solution of Gas-Turbine and Other Combustion Heat-Balance Problems With Predetermined AirflowSource: Journal of Engineering for Gas Turbines and Power:;1964:;volume( 086 ):;issue: 001::page 50Author:R. W. Foster-Pegg
DOI: 10.1115/1.3675415Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The generally used boiler efficiency concept is not convenient when combustion air is not varied in direct proportion to fuel. This situation may arise, for example, if combustion is being performed in gases exhausted by a gas turbine and the flow of these gases is determined by the requirement to carry a definite load on the gas turbine. This paper outlines a method of calculation alternative to the normal boiler efficiency method whereby the heat content in effluent gases from a combustion process such as stack gases may be divided into losses associated with the combustion air and a loss proportional to fuel. Some heat-balance calculations of a hypothetical cycle are included in an Appendix to demonstrate use of the method.
keyword(s): Heat , Combustion , Air flow , Gas turbines , Gases , Fuels , Boilers , Flow (Dynamics) , Stress AND Cycles ,
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| contributor author | R. W. Foster-Pegg | |
| date accessioned | 2017-05-08T23:20:40Z | |
| date available | 2017-05-08T23:20:40Z | |
| date copyright | January, 1964 | |
| date issued | 1964 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26632#50_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/100101 | |
| description abstract | The generally used boiler efficiency concept is not convenient when combustion air is not varied in direct proportion to fuel. This situation may arise, for example, if combustion is being performed in gases exhausted by a gas turbine and the flow of these gases is determined by the requirement to carry a definite load on the gas turbine. This paper outlines a method of calculation alternative to the normal boiler efficiency method whereby the heat content in effluent gases from a combustion process such as stack gases may be divided into losses associated with the combustion air and a loss proportional to fuel. Some heat-balance calculations of a hypothetical cycle are included in an Appendix to demonstrate use of the method. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | A Procedure for Solution of Gas-Turbine and Other Combustion Heat-Balance Problems With Predetermined Airflow | |
| type | Journal Paper | |
| journal volume | 86 | |
| journal issue | 1 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3675415 | |
| journal fristpage | 50 | |
| journal lastpage | 56 | |
| identifier eissn | 0742-4795 | |
| keywords | Heat | |
| keywords | Combustion | |
| keywords | Air flow | |
| keywords | Gas turbines | |
| keywords | Gases | |
| keywords | Fuels | |
| keywords | Boilers | |
| keywords | Flow (Dynamics) | |
| keywords | Stress AND Cycles | |
| tree | Journal of Engineering for Gas Turbines and Power:;1964:;volume( 086 ):;issue: 001 | |
| contenttype | Fulltext |