FUND OF ENG THERMODYN(LLF)+WILEYPLUS
9th Edition
ISBN: 9781119391777
Author: MORAN
Publisher: WILEY
expand_more
expand_more
format_list_bulleted
Question
error_outline
This textbook solution is under construction.
Students have asked these similar questions
11. The exhaust gases of a gas turbine, are used in a well insulated regenerator
(heat exchanger) to raise steam at 2 bar, which is subsequently fed to a steam
turbine in order to produce additional power. The air enters the regenerator at
758 K and exits at 350 K. The mass flow rate of the air is 3.2 kg/s. Water at
45°C and 2 bar enters the regenerator and exits as saturated steam at the same
pressure. Determine:
a) The mass flow rate of the water.
b) The rate of entropy production in the regenerator in kJ/s.
(2) Describe briefly why the following statements are wrong.
(a) "Hot cup of coffee becoming cold spontaneously is an entropy-decreasing process. So the
law of entropy increase can be violated."
(b) “Air conditioners require bulky external unit, exhausting heat to outside. With the
technology constantly advancing, external unit will be eliminated in the future."
(3).
A gas turbine unit consists of a compressor, combustion chamber, turbine
and heat exchanger. The unit has a pressure ratio of 6:1 and a maximum
cycle temperature of 600°C. The isentropic efficiencies of the compressor and
turbine are 0.8 and 0.85 respectively.
The air enters the compressor at 15°C at a rate of 17kg/s. the heat exchanger
effectiveness is 80%. If the compressor and turbine are connected by a rigid
shaft, calculate:
(a). the net power
(b). the thermal efficiency
(c). the thermal efficiency with the heat exchanger bypassed.
Knowledge Booster
Similar questions
- Air at 2.5 bar, 400 K is extracted from a main jet engine compressor for cabin cooling. The extracted air enters a heat exchanger where it is cooled at constant pressure to 350 K through heat transfer with the ambient. It then expands adiabatically to 1.0 bar through a turbine and is discharged into the cabin. The turbine has an isentropic efficiency of 80%. If the mass flow rate of the air is 2.5 kg/s, determine: (a) the power developed by the turbine, in kW. (b) the magnitude of the rate of heat transfer from the air to the ambient, in kW.arrow_forwardSteam enters the turbine of a vapor power plant at 600 lbf/in.?, 700°F and exits as a two-phase liquid-vapor mixture at 90°F. Condensate exits the condenser at 85°F and is pumped to 600 lbf/in.2 The turbine and pump isentropic efficiencies are 90 and 80%, respectively. The net power developed is 1 MW. Determine: (a) the percent steam quality at the turbine exit. (b) the percent thermal efficiency. (c) the steam mass flow rate, in Ib/h.arrow_forwardIn a gas turbine power plant, air at 10°C and I bar is compressed to a pressure of 4 bar by a compressor. The air is then heated in a 100% efficient heat exchanger and in the combustion chamber to a temperature of 700°C. heat exchanger and the combustion chamber is 0.14 bar. Calculate the power plant efficiency.arrow_forward
- ) An open type heat exchanger (feed water heater) operates at 7 bar pressure. Compressed liquid water and superheated steam at 35°C enter heat exchanger and exits as saturated liquid. As the ratio of mass flow rates of compressed liquid and superheated steam flows is 4.5/1, determine a) The temperature of superheated steam b) Entropy generation during this process in kJ/kg.pthund stam K KARIŞIM ODASI 7 bar T35°C Pe7 bar su Kızgın buhar P-7 bar su P7 bar ve x0 su n, = m, + ih, -0.222 c)arrow_forwardPlease draw the H-S diagram.arrow_forwardIn a gas turbine plant, the pressure ratio, through which air at 15°C is compressed, is 6. The same air is then heated to a maximum permissible temperature of 750°C first in a heat exchanger which is 75% efficient and then in the combustion chamber. The same air at 750 C is expanded in two stages such that expansion work is maximum. The air is reheated to 750°C after the first state. Determine the cycle thermal efficiency, the work ratio and the net shaft work per kg of air. The efficiencies may be assumed to be 80% and 85% for the compressor and turbine respectively.e) Air enters the compressor of a gas turbinearrow_forward
- 3. In a gas turbine power plant, the air is preheated by the exhaust gases in a heat exchanger called a regenerator. Air enters at 1 MPa, 550 K, and the mass flow rate of 900 kg / min. Heat is transferred to the air with a rate of 3500 kJ / s. While the exhaust gas enters the regenerator at 150 kPa, 800 K and leaves at 130 kPa and 600 K. Assuming the air and the exhaust gases are ignoring kinetic and potential energy effects, determine the a) the air temperature at the outlet b) the exhaust gas flow rate [Assuming that air and exhaust gas has the same Cp = 1.005 kJ/kg.K]arrow_forwardREFRIGERATION ENGINEERING ACTUAL VCRSarrow_forwardSteamenters the turbine of a vapor power plant at 600 lbf/in., 1000°F and exits as a two-phase liquid-vapor mixture at 100°F. Condensate exits the condenser at 95°F and is pumped to 600 Ibf/in.? The turbine and pump isentropic efficiencies are 90 and 80%, respectively. The net power developed is 1 MW. Determine: (a) the percent steam quality at the turbine exit. (b) the percent thermal efficiency. (c) the steam mass flowrate, in Ib/h.arrow_forward
- Problem 1 In a Rankine Thermodynamic cycle, steam leaves the boiler and enters the turbine at 600 psia, 800 °F. The condenser pressure is 1 psia. After presenting a schematic of the problem in addition to clearly labeled and explained T-s and h-s diagrams, you are asked to determine the following: (a) Pump work required per Ibm of working fluid. Quality of fluid at turbine inlet. Work output of turbine per lbm of working fluid. Energy input to the boiler per lbm of working fluid. Heat rejection by the condenser per Ibm of working fluid. Determine the cycle thermal efficiency. (d) (e) (f)arrow_forwardSuppose that the regenerative heat exchanger is only 80% efficient, i.e., only 80% of theheat exhausted in step (B) is absorbed in step (D). For an ideal gas working fluid (Cv = 5/2 R, R = 8.3145 J/mol K) operating with the heat reservoirs at Th = 400 K and Tc = 300 K, determine how much work per mol of working fluid is needed to supplement the regenerative heat exchanger in step (D) and ensure that the cycle is completed. What is the new ηcycle in light of this additional work requirement? (the answer does not need to be numeric)arrow_forwardA power plant using a Rankine power generation cycle and steam operates at a temperature of 81.25°C in the condenser, a pressure of 5 MPa in the boiler and a maximum boiler temp of 775°C. The cycle operates at steady state with a mass flow rate of 2.5kg/s. Use the steam tables in the appendix of Sandler (p. 917 to 925). a.) Draw out the cycle, calculate the work required for the pump, the work output by the turbine, the heat into the boiler, and the heat out of the condenser. b.) What is the efficiency of this power plant? c.) If the turbine was only 89% efficient but still adiabatic (only generates 89% of the calculated work from part b), what is the overall efficiency of the cycle?arrow_forward
arrow_back_ios
SEE MORE QUESTIONS
arrow_forward_ios
Recommended textbooks for you
- Elements Of ElectromagneticsMechanical EngineeringISBN:9780190698614Author:Sadiku, Matthew N. O.Publisher:Oxford University PressMechanics of Materials (10th Edition)Mechanical EngineeringISBN:9780134319650Author:Russell C. HibbelerPublisher:PEARSONThermodynamics: An Engineering ApproachMechanical EngineeringISBN:9781259822674Author:Yunus A. Cengel Dr., Michael A. BolesPublisher:McGraw-Hill Education
- Control Systems EngineeringMechanical EngineeringISBN:9781118170519Author:Norman S. NisePublisher:WILEYMechanics of Materials (MindTap Course List)Mechanical EngineeringISBN:9781337093347Author:Barry J. Goodno, James M. GerePublisher:Cengage LearningEngineering Mechanics: StaticsMechanical EngineeringISBN:9781118807330Author:James L. Meriam, L. G. Kraige, J. N. BoltonPublisher:WILEY
Elements Of Electromagnetics
Mechanical Engineering
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Oxford University Press
Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:9780134319650
Author:Russell C. Hibbeler
Publisher:PEARSON
Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:9781259822674
Author:Yunus A. Cengel Dr., Michael A. Boles
Publisher:McGraw-Hill Education
Control Systems Engineering
Mechanical Engineering
ISBN:9781118170519
Author:Norman S. Nise
Publisher:WILEY
Mechanics of Materials (MindTap Course List)
Mechanical Engineering
ISBN:9781337093347
Author:Barry J. Goodno, James M. Gere
Publisher:Cengage Learning
Engineering Mechanics: Statics
Mechanical Engineering
ISBN:9781118807330
Author:James L. Meriam, L. G. Kraige, J. N. Bolton
Publisher:WILEY