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Program computes fuel input, combustion temperature

Journal Article · · Power Eng.; (United States)
OSTI ID:6945242
Supplementary fuel firing of turbine exhaust gases is frequently utilized in combined cycle and cogeneration projects to generate additional steam from heat recovery boilers. Typical turbine exhaust has 14-16% free oxygen before entering the combustion system. Part or all of it may be utilized to increase the final combustion temperature to desired levels. Duct burners typically raise the exhaust gas temperature to approximately 1700 F maximum. In furnace-fire heat recovery boilers the final combustion temperature could be as high as adiabatic combustion temperature, which is the temperature obtained by consuming all of the free oxygen in the exhaust gas. Natural gas is the most widely used fuel. In order to analyze the performance of the burner system and the boiler--and to calculate the cycle efficiency--the following data are required: 1. Fuel required to raise the temperature of the incoming turbine exhaust gas to a particular value. Sometimes fresh air is used instead of turbine exhaust gas; 2. Given a particular fuel input, the combustion temperature (reverse of case 1) that results; and 3. Fuel data such as density and heating value in Btu/lb and Btu/scf.
OSTI ID:
6945242
Journal Information:
Power Eng.; (United States), Journal Name: Power Eng.; (United States) Vol. 90:7; ISSN POENA
Country of Publication:
United States
Language:
English