Fundamentals Of Thermodynamics
10th Edition
ISBN: 9781119494966
Author: Borgnakke, C. (claus), Sonntag, Richard Edwin, Author.
Publisher: Wiley,
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Steam at 6.2 MPa and 480°C is received by a regenerative engine. Extractions for feedwaterheating occurs at 3 MPa and again at. 1.4 MPa,with the remaining steam expanding to0.0065 MPa. For the ideal engine with a throttla flow of 54,500 kg/h, find the hourlyquantities of steam ex-tracted, the turbine work in kW, and the thermal efficiency. For an ideal cycle through the same states, calculate Q and e。
A Steam power plant uses a Rankine cycle to produce electrical power. The boiler pressure is 2 MPa and the temperature at the turbine inlet is 300C. The pump inlet pressure is 0.025 MPa and the entropy is 0.8931 kJ/kg-k. The turbine gives 1MW of work to the generator. Find the dryness of the steam at turbine exit, Wp, Qa, Qr, Wt, Wnet, efficiency, SR, and mass flow rate of steam. (84.65%, 2.0143 kJ/kg, 2749.56 kJ/kg, 1986.15 kJ/kg, 765.42 kJ/kg, 763.41 kJ/kg, 27.76%, 4.7157 kg/kWh, 1.3064 kg/s)
-Draw the T-S diagram with properly labelled points and solve the problems. Show your COMPLETE solution
- Use the Steam Table provided if necessary.
The turbine section in a jet engine receives gas (assume air) at 1200 K,
800 kPa with an ambient atmosphere at 80 kPa The turbine is followed
by a nozzle open to the atmosphere and all the turbine work drives a
compressor receiving air at 85 kPa, 270 K with the same flow rate Find
the turbine exit pressure P. so the nozzle has an exit velocity of 800
m/s.
Lutfen birini seçin.
a 341 kPa
b. 400 KPa
C 382 KPa
d 254 KPa
e 300 kPa
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- In a reheat cycle steam at 550°C expands in an h.p. turbine till it is saturated vapour. It is reheated at constant pressure to 450°C and then expands in a I.p. turbine to 40°C. If the maximum moisture content at turbine exhaust is limited to 10%, find (a) the reheat pressure, (b) the boiler pressure, c) the net specific work output,plss give info as much as possiblearrow_forwardA gas turbine power plant operating on Brayton cycle shown in figure. The air enters the compressor at 300 K and exits at 700 K. The pressure ratio for compressor is 7. The gas enters the turbine at 1600 K, 600 kPa and exits at 1050 K, 100 kPa. Fuel T₂ = 700k. p=7 Compressor T₁ = 300k Fresh air Combustion Chamber Turbine Find Work T3 = 1600 K P3=600 кра Exhaust gas In put work efficiency we net =1050 K P4=100 kPaarrow_forwardUPVOTE WILL BE GIVEN FOR FAST ANSWERS WRITE LEGIBLY THANKSarrow_forward
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