Fundamentals Of Engineering Thermodynamics
9th Edition
ISBN: 9781119391388
Author: MORAN, Michael J., SHAPIRO, Howard N., Boettner, Daisie D., Bailey, Margaret B.
Publisher: Wiley,
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For a given Rankine Cycle, the ideal pump work involves an isentropic compression process.
O True
O False
Specific pump work input for an ideal Rankine cycle can be approximated with which of the following equations (where state 1 is the liquid into the pump and state 2 is the liquid coming out of the pump)?
v1(p1 - p2)
v2(p2 - p1)
v1(h2 - h1)
v2(p1 - p2)
v1(p2 - p1)
Consider the operation of an actual turbine in a gas turbine engine. The mass flow rate is 50 lbm/s. The turbine inlet temperature is 2040 deg F. The pressure ratio in the compressor is 18.15. The turbine efficiency is 0.91. Assume variable specific heats. The turbine exit temperature is approximately
Group of answer choices
1320 deg R
1220 deg R
1200 deg R
1090 deg R
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- A gas turbine has continuous combustion with constant pressure receives air from atmosphere at 15 °Cand compresses it to five time the intake pressure in a compressor with efficiency of 80%. The compressed air then passes through a regenerator with effectiveness of 60%. From the regenerator, the air passes through the combustion chamber at constant pressure in which temperature is raised to 800 °C. From the combustion chamber the air expand through a turbine to atmospheric pressure. The isentropic efficiency of the turbine is 82%. The flow air through the gas turbine is at rate of 2.5 kg/s. Neglect the mass of fuel and take n =1.4 and cp=1.005 kJ/kg K. Evaluate;i.The net power output of the gas turbineii.The temperature of the air leaving the regenerator to combustion chamberiii.The thermal efficiency of the gas turbineiv.Discussone method of improving the thermal efficiency ofthis gas turbine.arrow_forwardCompare the thermal efficiency of a two-stage gas turbine with regeneration, reheating, and intercooling to that of a three-stage gas turbine with the same equipment when all components operate ideally.arrow_forwardA Carnot cycle has been chosen as a candidate for the ideal vapor power cycle. The pump inlet is a saturated liquid and the minimum and maximum pressures are set. The minimum pressure is 10 kPa and the maximum pressure is 10 MPa. Check all that will are correct Group of answer choices The minimum pump work will be about 5 kJ/kg The efficiency of the Carnot cycle will be greater than the efficiency of a Rankine cycle with the same minimum and maximum pressures The difference between the maximum and minimum temperature will be small and the thermal efficiency will be low. The minimum pump work will be about 10 kJ/kgarrow_forward
- A water feed pump operates with a mass flow rate of 464 kg/s. The inlet pressure is 689 kPa and the outlet pressure is 26 MPa. Water enters the pump at 422 K. Assuming an isentropic efficiency of 85%, estimate the power required to drive the pump.arrow_forwardIn a Rankine Cycle, real work required by the pump is less that the isentropic work. True Falsearrow_forwardFor a Rankine cycle, decreasing minimum pressure while holding all other parameters constant will allow an engineer to make the following statements Group of answer choices The quality at the turbine exit will decrease increasing liquid water content and back stage turbine damage, Turbine net work output will increase due to the reduced pressure at the exit The quality at the turbine exit will increase improving turbine reliability The average temperature at which heat is rejected will increase increasing thermal efficiencyarrow_forward
- A steady-flow system operating on the ideal Ericsson cycle can achieve the Carnot efficiency. One of the salient features of this cycle is the isothermal expansion through a heated turbine, as shown in Fig. a. Heat is added to the turbine such that the outlet temperature is equal to the inlet temperature, i.e. T₁=T₂, and the overall pressure ratio for this process is rₚ=P₁/P₂. However, an isothermal expansion through a heated turbine is very difficult to achieve in practical engineering applications. An alternate approach is two use a multi-stage expansion process with reheating. In this approach, the gas expansion process is carried out in multiple stages with reheating in between each stage. Consider the two-stage turbine expansion with reheating shown in Fig. b. The gas enters the first stage of the turbine at state A1, is expanded isentropically to an intermediate pressure Pₐ₂, is reheated at constant pressure to state B1, and is expanded in the second stage isentropically to the…arrow_forwardA steady-flow system operating on the ideal Ericsson cycle can achieve the Carnot efficiency. One of the salient features of this cycle is the isothermal expansion through a heated turbine, as shown in Fig. a. Heat is added to the turbine such that the outlet temperature is equal to the inlet temperature, i.e. T₁=T₂, and the overall pressure ratio for this process is rₚ=P₁/P₂. However, an isothermal expansion through a heated turbine is very difficult to achieve in practical engineering applications. An alternate approach is two use a multi-stage expansion process with reheating. In this approach, the gas expansion process is carried out in multiple stages with reheating in between each stage. Consider the two-stage turbine expansion with reheating shown in Fig. b. The gas enters the first stage of the turbine at state A1, is expanded isentropically to an intermediate pressure Pₐ₂, is reheated at constant pressure to state B1, and is expanded in the second stage isentropically to the…arrow_forwardWhat are the practical limitations to maximum work being able to be done from an engine when all the processes ard reversible.arrow_forward
- 19arrow_forwardIf the turbine in a Rankine cycle operated with a second law efficiency less than 100%, how would the actual exiting quality compare to the ideal exiting quality?arrow_forwardan ideal Rankine cycle (fluid flow rate is 8 kg/s) operating between upper and lower pressures of 5 and 10,000 kPa. Draw a schematic of the components of this cycle. Draw the cycle on a P-v phase diagram and a T-s diagram. Find the power output of the turbine, the power input needed for the pump, and the overall cycle thermal efficiency.arrow_forward
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