Completely solve and provide the diagram. Box the final answers. Use 4 decimals in all instances. Problem: 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% %3D Compressor mechanical efficiency = 87% 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 %3D Determine: a. The actual temperature entering the combustor in K b. Fuel air ratio c. Fuel consumption in kg/s d. The volume of air supplied in CFM
Completely solve and provide the diagram. Box the final answers. Use 4 decimals in all instances. Problem: 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% %3D Compressor mechanical efficiency = 87% 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 %3D Determine: a. The actual temperature entering the combustor in K b. Fuel air ratio c. Fuel consumption in kg/s d. The volume of air supplied in CFM
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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Completely solve and provide the diagram. Box the final answers. Use 4 decimals in all instances. PLEASE WRITE LEGIBLY OR TYPEWRITE THE SOLUTIONS.
![Completely solve and provide the diagram. Box the final answers. Use 4 decimals
in all instances.
Problem: 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 mechanical efficiency = 87%
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:
a. The actual temperature entering the combustor in K
b. Fuel air ratio
c. Fuel consumption in kg/s
d. The volume of air supplied in CFM](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F1e7ffa2a-23a3-47c5-b016-ba17b777fedf%2F4a1b6ab8-81a8-44f5-bd54-73e5857b03f7%2Fnjb85ok_processed.png&w=3840&q=75)
Transcribed Image Text:Completely solve and provide the diagram. Box the final answers. Use 4 decimals
in all instances.
Problem: 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 mechanical efficiency = 87%
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:
a. The actual temperature entering the combustor in K
b. Fuel air ratio
c. Fuel consumption in kg/s
d. The volume of air supplied in CFM
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