Question

In: Mechanical Engineering

A gas turbine used for power generation is producing 57MW of power. The turbine’s exhaust temperature...

A gas turbine used for power generation is producing 57MW of power. The turbine’s exhaust temperature is 541°C at a mass flow rate of 132.8 kg/s and is currently emitted to the atmosphere.

Your task is to design a heat exchanger that recovers the waste heat from the exhaust. The recovered heat is to be used to heat water from 40°C to 60°C for use in a closed-loop hydronic heating system for an office building. The heat exchanger is to be placed between the gas turbine’s exhaust and the attached power generator. To not interfere with the power generator, the pressure drop across the hot flow path should not exceed 600Pa. The maximum gas mass flow rate possible through the heat exchanger has been restricted to 4% of the exhaust gas flow rate of the turbine.

QUESTIONS

1.DO LMTD CALCULATION

2. TEMPERATURE CORRECTION FACTOR CALCULATION

Solutions

Expert Solution


Related Solutions

I want a report on ‏)Gas Turbine Power Plant as are being used as standby plants...
I want a report on ‏)Gas Turbine Power Plant as are being used as standby plants for hydro-electric)
1. Power generation by natural gas or other petroleum productfired steam power plant is the...
1. Power generation by natural gas or other petroleum product fired steam power plant is the most comment way of producing energy in most parts of the worlda. Sketch steam power plant and discuss the function of each unit Operation in the process(b. What are the major operational and safety challenges in steam power plants )c. Pumps are the most important fluid movers in process industries, discuss the various types of Pumps you find in steam power plant and their...
How can the temperature of the incoming air affect the effect of the gas turbine? Describe...
How can the temperature of the incoming air affect the effect of the gas turbine? Describe this by drawing a T-s diagram. Also draw a T-s diagram for how the compression ratio affects the effect and a T-s diagram for how the combustion temperature affects the effect.
. Air enters the compressor of a gas turbine power plant operating on Brayton cycle at...
. Air enters the compressor of a gas turbine power plant operating on Brayton cycle at 14.5 psia and 540° R. The pressure ratio across the turbine and compressor is same, which is equal to 6. Assume that the compressor work as 0.4 times the turbine work. Take K=1.4 a) Draw the T-S diagram of the cycle. [2] b) Calculate the maximum temperature in the cycle. [3] c) Calculate the cycle efficiency
In a gas turbine of a thermoelectric plant a regenerator is used that preheats the air...
In a gas turbine of a thermoelectric plant a regenerator is used that preheats the air before it enters the combustion chamber. You have the options of a backflow heat exchanger or a shell heat exchanger and two tube passages. The air leaves the compressor at a temperature of 350 C and the exhaust gases have a temperature of 700 C. The mass flow in both cases is 5 kg / sec. The overall transfer coefficient is 75 w /...
A combined gas turbine–vapor power plant has a net power output of 200 MW. Air enters...
A combined gas turbine–vapor power plant has a net power output of 200 MW. Air enters the compressor of the gas turbine at 300 kPa, 1200 K, and is compressed to 1000 kPa. The pressure ratio of the gas turbine cycle is 11. Steam leaving the turbine of the vapor power cycle are used to heat the steam at 6 MPa to 350C in a heat exchanger. The combustion gases leave the heat exchanger at 420 K. An open feedwater...
A gas turbine unit has a pressure ratio of 5/1 and a maximum cycle temperature of...
A gas turbine unit has a pressure ratio of 5/1 and a maximum cycle temperature of 550⁰C. The turbine drives the compressor and an electric generator., the mechanical efficiency of the drive being 97%. The ambient temperature is 20⁰C and the isentropic efficiencies of the compressor and turbine are 0.8 and 0.83 respectively. Calculate the power output in kilowatts for an airflow of 15kg/s. Calculate also the thermal efficiency and the work ratio. Neglect changes in kinetic energy, and the...
a gas turbine power plant operating on brayton cycle with a fuel compressor isentropic efficiency of...
a gas turbine power plant operating on brayton cycle with a fuel compressor isentropic efficiency of 80 and turbine isentropic efficiency of 85 percent and it has a pressure ratio of rp. The gas temperature is 300K at a compressor inlet and 1300K at the turbine inlet. Heat is received from a source of 1700K. Utilizing the air-standard assumption (Hot Assumption) and for pressure ratio rp which varies from 3 to 10, determine: a) The gas temperature at the exits...
A gas-turbine power plant operates on the simple Brayton cycle with air as the working fluid...
A gas-turbine power plant operates on the simple Brayton cycle with air as the working fluid and delivers 32 MW of power. The minimum and maximum temperatures in the cycle are 310 and 900 K, and the pressure of air at the compressor exit is 8 times the value at the compressor inlet. Assuming an isentropic efficiency of 80% for the compressor and 86% for the turbine, determine the mass flow rate of air through the cycle. Account for the...
A gas turbine power plant operates on a Brayton cycles has a pressure ratio of 7....
A gas turbine power plant operates on a Brayton cycles has a pressure ratio of 7. Air enters the compressor at 300 K. The energy in the form of heat is transferred to the air in the amount of 950 kJ/kg. Using a variable specific heat for air and assuming the compressor isentropic efficiency is 83 percent and turbine isentropic efficiency is 85 percent. Determine the followings: (i) The highest temperature in the cycle [5 marks] (ii) The net work...
ADVERTISEMENT
ADVERTISEMENT
ADVERTISEMENT