The actual temperature entering the combustor in K. Fuel air ratio Fuel consumption in kg/s
The actual temperature entering the combustor in K. Fuel air ratio Fuel consumption in kg/s
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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Question
A 25 MW Gas Turbine power plant operating on a simple open cycle system gives the following data:
Air inlet temperature = 300 K
Air inlet pressure = 101.325 kPa
Pressure ratio = 4
Temperature after combustion = 1150 K
Compressor adiabatic efficiency = 92%
Compressor
Turbine mechanical efficiency = 80%
Generator efficiency = 96 %
Heating value = 41,680 kJ/kg
Combustion losses = 10%
For air and gas mixture, Cp = 1.005 kJ/kg – K, R = 282 J/kg-K
Determine:
- The actual temperature entering the combustor in K.
- Fuel air ratio
- Fuel consumption in kg/s
- The volume of air supplied in CFM.
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