Question No.5: With help of T-s diagram, explain the effects of variables on efficiency of the Rankine cycle
Question No.6: State various methods to improve efficiency of Brayton cycle. With suitable diagrams, explain any two of them


Question No.5
The variable which affect the efficiency of rankine cyle are
1.condensor pressure 2. Superheating of steam 3. boiler pressure
This is explained in comparison with the simple Rankine cycle (Fig 1)
1. Refer fig 2 By lowering the condensor pressure, the temperature at which the heat is rejected also lowered. Thus the amount of heat transfer increases (that can be see in the figure - shaded portion ) . Thus the effect is increase in the thermal efficiency of the cycle.
2. Refer fig 3 Super heating the steam from the boiler increases the temperature of steam without changing the boiler pressure. This will add the heat energy to the steam and increases the thermal efficiency. This dcreases the moisture content in the steam during the expansion.
3. Refer fig 4 , by increasing the operating pressure of boiler, the temperature at which boiling takes place also increases. This increases the heat added to the steam and increases the thermal efficiency of the cycle.
Question No.6
The various methods to improve efficiency of Brayton cycle are
1. Regeneration 2. Increasing the pressure ratio 3. Inter cooling 4. Reheating
Intercooling
Refer figure 6
Inter cooling can be done with staged compression. The compression is divided in to two stages. Air is compressed in the first stage , is cooled to initial temperature in the intercooler, then compressed further in the second stage. 1-2'-5-6 is the ideal cycle without intercooling. 1-2-3-4-5-6 is the cycle with intercooling. The cycle 2-3-4-2' is added to the basic cycle. We can see that there is more work capacity (included area is more), there is more heat supply also. So the efficiency of the cycle can be increased by intercooling.
Reheat
Refer fig 7
In this the expansion in the turbine is done in two stages. In between reheat is provided (4-5-6-4' is added to the basic cycle due to reheat). The work capacity and heat supply also increases. The efficiency can be increased.
Question No.5: With help of T-s diagram, explain the effects of variables on efficiency of the...
3: Consider the Rankine power cycle using vapor and liquid. a: Explain what kinds of problems the Carnot Vapor Cycle has. b: Draw a T-s diagram for the ideal Rankine cycle and label each process explicitly c: There is a method to lower the condenser pressure (or to decrease the average low temperature) in order to improve the efficiency of the ideal Rankine cycle. Explain its advantages and disadvantages explicitly. d: Name the gas power cycle which uses the same...
solve in detail please
10-21 The net work output and the thermal efficiency for the Carnot and the simple ideal Rankine cycles with steam as the working fluid are to be calculated and compared. Steam enters the turbine in both cases at 5 MPa as a saturated vapor, and the condenser pressure is 50 kPa. In the Rankine cycle. the condenser exit state is saturated liquid and in the Carnot cycle, the boiler inlet state is saturated liquid. Draw the...
PA AQi T =Th AQ19 2 4 3 AQout T= Te V Figure 1: Pressure-volume diagram of the Stirling cycle. (a) A Stirling cycle consists of two isothermal processes and two isochoricprocesses as shown in Fig. J. The hot reservoir is at temperature T and the cold-reservoir AS at temperaturé T)You may assume that the working fluid is anideal gas with Llegrees of freedom. The compression ratio V2/Vi)i.e. the ratio of the volume of the gas at state 2 to...
please solve the problem, it is thermo-design problem,
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Combustor Gas turbine :Compressor- Turbine Air inlet- 7 Heat-recovery steam generator Turbine Vapor cycle W) Pump Condenser Cooling water Figure 1: Combined gas turbine-vapor power plant Consider Figure 1 above. The following information is given a. p- 14.7 psia, T 540 °R b. P/p1 12.0 С. Т,-2500,"R d, P,-14.7 psia, Ts-700. "R (Rankine) e. P 1000. psia f. P 1.00 psia, x>0.85 or superheated The isentropic...
please help thermodynamics
a) Explain the methods that can be adopted to increase the thermal efficiency of a vapor power cycle. You may use a T-s diagram to explain your reasons. b) A steam regenerative cycle, shown below, is delivering 100 MW of power. Steam from the boller is supplied to the turbine at 8 MPa. 400°C. After expanding isentropically in the 1st stage turbine to a pressure of 1 MPa, steam is taken to the reheater where Its temperature...
please solve the problem, it is thermo-design problem,
please do in details, thank you
Combustor Gas turbine :Compressor- Turbine Air inlet- 7 Heat-recovery steam generator Turbine Vapor cycle W) Pump Condenser Cooling water Figure 1: Combined gas turbine-vapor power plant Consider Figure 1 above. The following information is given a. p- 14.7 psia, T 540 °R b. P/p1 12.0 С. Т,-2500,"R d, P,-14.7 psia, Ts-700. "R (Rankine) e. P 1000. psia f. P 1.00 psia, x>0.85 or superheated The isentropic...
Need help for this Brayton Cycle problem.
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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...
4. An Ideal diesel engine has a compression ratio of 20 and uses air as the working fluid. The state of air at the beginning of the compression process is 95kPa and 20°C. If the maximum temperature in the cycle is not to exceed 2200K, determine a) the thermal efficiency and b) the mean effective pressure. Assume constant specific heats for air at room temperature. 5. An aircraft engine operates on a simple ideal Brayton cycle with a pressure ratio...
a) 15 pts Trace the T-s diagram of an ideal turbojet with afterburner, labeling each point. Do not show thoe equations of the various processes, but make sure that both shape and lengths of the different segments of the cycle are as close as possible to those of an ideal engine. b) 5 pts Find an expression for 7a starting from the free-stream conditions c) 10 pts Derive an expression for Tis as a function of the free-stream conditions and...
the question(5.) the answer please in meters. SI
units.
the Taeal gas model Tol alr aiia Hegligible potential energy effects. a. Determine the temperature of the air at the exit of the diffuser, in K b. Ifthe air would undergo an isentropic process as It fows through the diffuser, determine the pressure of the air at the diffuser exit. in kPa. c. Ie friction were present would the pressure of the air at the diffuser exit be greater than. less...