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Please answer the following, the final answe for part b should
be 515kW.
P2. Oxygen gas...
For a gas compressor compresses gas (Cv= 718 J/KgK and Cp= 1005 J/KgK) adiabatically from 1...
For a gas compressor compresses gas (Cv= 718 J/KgK and Cp= 1005 J/KgK) adiabatically from 1 bar and 15 ºC to 10 bar with an isentropic efficiency of 0.89. The gas flow rate is 5 kg/s. Calculate the temperature after compression and the power input
Question A.1 A schematic of a gas turbine combined cycle generating plant is shown in Figure...
Question A.1 A schematic of a gas turbine combined cycle generating plant is shown in Figure A1.1 on the next page. Exhaust gas from the gas turbine generator pass througha heat recovery steam generator (HRSG) which generates steam to drive a steam turbine generator. The following data is provided for the plant: Gas turbine 18.9:1 Pressure ratio Compressor air inlet temperature Turbine inlet temperature 15°C t 273 288 1350°C +273- 1623 588 kg/s T, T3 Exhaust gas mass flow Isentropic...
Need help for this Brayton Cycle problem. Please help me 4. (30 marks) A gas-turbine power plant operates on the simple...
Need help for this Brayton Cycle problem.
Please help me
4. (30 marks) A gas-turbine power plant operates on the simple Brayton cycle between the pressure limits of 100 kPa and 800 kPa. The T-s diagram of this cycle is shown in Fig. 2. Air enters the compressor at 30°C and leaves at 330°C at a mass flow rate of 200 kg/s. The maximum cycle temperature is 1400 K. During operation of the cycle, the net power output is measured...
please help thank you in advance In a gas turbine power plant, the gas enters the...
please help
thank you in advance
In a gas turbine power plant, the gas enters the five-stage compressor at 300 K. The overall power ratio is 20. After the compression, the gas enters a regenerator with an effectiveness of 80%. For preheating, it is further heated in a combustion chamber until it reaches a temperature of 1600 K. The heated gas expands to the first turbine stage and is reheated to 1550 K. The temperatures after the reheating processes are...
Section B – combined cycles Overview: a combined gas – steam power cycle in Sweden provides...
Section B – combined cycles Overview: a combined gas – steam power cycle in Sweden provides electricity and hot water for heating duties for a small city. The gas turbine drives an electricity generator with an efficiency of 97%. A sub-critical coal fired boiler is used as a heat recovery steam generator, as well as providing additional steam from coal during the winter months. The steam turbine drives an electricity generator with an efficiency of 95%. The plant is located...
Thermodynamics 1. Saturated liquid H20 at 16 MPa is fed into the boiler of a variant of a Carnot cycle (but simplified Rankin cycle) where the working fluid is not an ideal gas. Saturated H20 va...
Thermodynamics
1. Saturated liquid H20 at 16 MPa is fed into the boiler of a variant of a Carnot cycle (but simplified Rankin cycle) where the working fluid is not an ideal gas. Saturated H20 vapor is fed into the turbine of the same turbine. The condenser of this turbine is operated at 8 kPa. The mass flowrate of the H20 in this cycle is 7.2x103 kg/min. Draw the path of this process on T-s diagram. Estimate the thermal efficiency...
This is from a practice test and I want to be able to check my answers...
This is from a practice test and I want to be able to check my
answers so any help you can give will be greatly appreciated!
Consider the Brayton Cycle for gas-turbine heat engines as shown below. Air is compressed from P,=100kPa, T,=20°C to P2=1400 kPa. The inlet temperature to the turbine is Tz=1100°C. The compressor and turbine are both adiabatic and both have isentropic efficiencies of 80%. in Heat exchanger Wool Compressor Turbine Heat exchanger 9 out Use Cp=1.005...
Question B (15 marks) You are to analyze a combined cycle that consists of a gas (air) turbine cy...
Energy Convertion
hello, please help me quickly please please
thank you
Question B (15 marks) You are to analyze a combined cycle that consists of a gas (air) turbine cycle (top) ttom). The gas cycle has the following operating conditions: inlet pressure to compressor one bar inlet temperature-300 K operating pressure ratio-12 Maxmum allowable temperature 1150 °C adiabatic efficiency for compressor 0.83 adiabatic efficiency for turbine-0.87 - - The exhaust leaves stack at 120 °C after vaporizing water in the...
Use a simple Brayton cycle gas turbine as the baseline for the following questions. Use a...
Use a simple Brayton cycle gas turbine as the baseline for the
following questions. Use a cold-air-standard analysis (R=0.287
kJ/kg-K, k=Cp/Cv=1.40, Cp= (k/(k-1))*R = 1.0045 kJ/kg-K) with the
following specifications:
Use a simple Brayton cycle gas turbine as the baseline for the following questions. Use a cold-air-standard analysis (R=0.287 kJ/kg-K, k=Cp/Cv=1.40, Cpr (k/(k-1))*R = 1.0045 kJ/kg-K) with the following specifications: Mass Inlet Press. Pressure Turbine Isentropic Eff Neglect combustion chemistry Flowrate T p Ratio Inlet T Comp Turb Neglect minor...
Problem 2/2 (50%) -The gas-turbine cycle of a combined gas-steam power plant has a pressure ratio...
Problem 2/2 (50%) -The gas-turbine cycle of a combined gas-steam power plant has a pressure ratio of 12. Air enters the compressor at 310 K and the turbine at 1400 K. The combustion gases leaving the gas turbine are used to heat the steam at 12.5 MPa to 500 C in a heat exchanger. The combustion gases leave the heat exchanger at 247"C. Steam expands in a high pressure turbine to a pressure of 2.5 MPa and is reheated in...
Question A.1 A schematic of a gas turbine combined cycle generating plant is shown in Figure A1.1 on the next page. Exhaust gas from the gas turbine generator pass througha heat recovery steam generator (HRSG) which generates steam to drive a steam turbine generator. The following data is provided for the plant: Gas turbine 18.9:1 Pressure ratio Compressor air inlet temperature Turbine inlet temperature 15°C t 273 288 1350°C +273- 1623 588 kg/s T, T3 Exhaust gas mass flow Isentropic...
Need help for this Brayton Cycle problem.
Please help me
4. (30 marks) A gas-turbine power plant operates on the simple Brayton cycle between the pressure limits of 100 kPa and 800 kPa. The T-s diagram of this cycle is shown in Fig. 2. Air enters the compressor at 30°C and leaves at 330°C at a mass flow rate of 200 kg/s. The maximum cycle temperature is 1400 K. During operation of the cycle, the net power output is measured...
please help
thank you in advance
In a gas turbine power plant, the gas enters the five-stage compressor at 300 K. The overall power ratio is 20. After the compression, the gas enters a regenerator with an effectiveness of 80%. For preheating, it is further heated in a combustion chamber until it reaches a temperature of 1600 K. The heated gas expands to the first turbine stage and is reheated to 1550 K. The temperatures after the reheating processes are...
Thermodynamics
1. Saturated liquid H20 at 16 MPa is fed into the boiler of a variant of a Carnot cycle (but simplified Rankin cycle) where the working fluid is not an ideal gas. Saturated H20 vapor is fed into the turbine of the same turbine. The condenser of this turbine is operated at 8 kPa. The mass flowrate of the H20 in this cycle is 7.2x103 kg/min. Draw the path of this process on T-s diagram. Estimate the thermal efficiency...
This is from a practice test and I want to be able to check my
answers so any help you can give will be greatly appreciated!
Consider the Brayton Cycle for gas-turbine heat engines as shown below. Air is compressed from P,=100kPa, T,=20°C to P2=1400 kPa. The inlet temperature to the turbine is Tz=1100°C. The compressor and turbine are both adiabatic and both have isentropic efficiencies of 80%. in Heat exchanger Wool Compressor Turbine Heat exchanger 9 out Use Cp=1.005...
Energy Convertion
hello, please help me quickly please please
thank you
Question B (15 marks) You are to analyze a combined cycle that consists of a gas (air) turbine cycle (top) ttom). The gas cycle has the following operating conditions: inlet pressure to compressor one bar inlet temperature-300 K operating pressure ratio-12 Maxmum allowable temperature 1150 °C adiabatic efficiency for compressor 0.83 adiabatic efficiency for turbine-0.87 - - The exhaust leaves stack at 120 °C after vaporizing water in the...
Use a simple Brayton cycle gas turbine as the baseline for the
following questions. Use a cold-air-standard analysis (R=0.287
kJ/kg-K, k=Cp/Cv=1.40, Cp= (k/(k-1))*R = 1.0045 kJ/kg-K) with the
following specifications:
Use a simple Brayton cycle gas turbine as the baseline for the following questions. Use a cold-air-standard analysis (R=0.287 kJ/kg-K, k=Cp/Cv=1.40, Cpr (k/(k-1))*R = 1.0045 kJ/kg-K) with the following specifications: Mass Inlet Press. Pressure Turbine Isentropic Eff Neglect combustion chemistry Flowrate T p Ratio Inlet T Comp Turb Neglect minor...
Problem 2/2 (50%) -The gas-turbine cycle of a combined gas-steam power plant has a pressure ratio of 12. Air enters the compressor at 310 K and the turbine at 1400 K. The combustion gases leaving the gas turbine are used to heat the steam at 12.5 MPa to 500 C in a heat exchanger. The combustion gases leave the heat exchanger at 247"C. Steam expands in a high pressure turbine to a pressure of 2.5 MPa and is reheated in...
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