The schematic of a single-flash geothermal power plant with state numbers is given in Fig. P10–69. Geothermal resource exists as saturated liquid at 230°C. The geothermal liquid is withdrawn from the production well at a rate of 230 kg/s and is flashed to a pressure of 500 kPa by an essentially isenthalpic flashing process where the resulting vapor is separated from the liquid in a separator and is directed to the turbine. The steam leaves the turbine at 10 kPa with a moisture content of 5 percent and enters the condenser where it is condensed; it is routed to a reinjection well along with the liquid coming off the separator. Determine (a) the power output of the turbine and the thermal efficiency of the plant, (b) the exergy of the geothermal liquid at the exit of the flash chamber, and the exergy destructions and the second-law efficiencies for (c) the turbine and (d) the entire plant.
FIGURE P10–69
(a)
The temperature of the steam after the flashing process and the power output from the turbine if the pressure of the steam at the exit of flash chamber is
Answer to Problem 69P
The power output turbine is
The thermal efficiency of the plant is
Explanation of Solution
Draw schematic diagram of single flash geothermal power plant as shown in Figure 1.
Write the general energy rate balance equation.
Here, the rate of total energy in is
Consider the system operates at steady state. Hence, the rate of change in net energy of the system becomes zero.
The Equation (I) is reduced as follows.
Refer Figure 1.
The flash chamber is nothing but the expansion valve. At expansion valve, the enthalpy kept constant.
Express the energy balance equation for the flash chamber.
Express the energy balance equation for the separator.
Express the energy balance equation for the turbine.
At state 1:
The geothermal water is extracted at the state of saturated liquid at the temperature of
The enthalpy and entropy at state 1 is as follows.
Refer Table A-4, “Saturated water-Temperature table”
The enthalpy
Refer Table A-1, “Molar mass, gas constant, and critical-point properties”.
At state 2:
The exit pressure of the flash chamber is
The geothermal steam is flashed at constant enthalpy. The exit steam of the flash chamber is at the quality of
Here, the fluid enthalpy is
Refer Table A-5, “Saturated water-Pressure table”.
Obtain the following corresponding to the pressure of
The entropy
Write the formula for mass flow rate of vapor at entering the turbine.
Here, the mass flow rate is
At state 3:
There is no pressure drop in the separator. The separator separates vapor and liquid form the flashed steam, and the separated vapor alone sent to the turbine.
The enthalpy
Refer Table A-5, “Saturated water-Pressure table”.
The enthalpy
At state 4:
The steam is at the state of saturated mixture at the pressure of
The quality at state 4 is as follows.
The enthalpy
Refer Table A-5, “Saturated water-Pressure table”.
Obtain the following corresponding to the pressure of
At state 6:
The saturated water only exits at the bottom of the separator. The enthalpy
Refer Table A-5, “Saturated water-Pressure table”.
The enthalpy
Write the formula for net energy input of the plant.
Write the formula for thermal efficiency.
Consider, the surrounding temperature is
The surrounding enthalpy
Refer Table A-4, “Saturated water-Temperature table”.
The enthalpy
Conclusion:
Substitute
Substitute
Substitute
Substitute
Equation (VII).
Substitute
Substitute
Equation (III).
Thus, the power output turbine is
Substitute
Equation (IX).
Substitute
Thus, the thermal efficiency of the plant is
(b)
The exergy of the geothermal liquid at the exit of the flash chamber, and the exergy destructions.
Answer to Problem 69P
The exergy of the geothermal liquid at the exit of the flash chamber, and the exergy destruction is
Explanation of Solution
Write the formula for exergy of the steam at their respective process state.
Here, the enthalpy is
Write the formula for rate of exergy destruction at the exit of flash chamber (state 6).
Here, the rate of exergy destruction at state 6 is
Conclusion:
For process state 1:
Substitute
For process state 2:
Substitute
For process state 3:
Substitute
For process state 4:
Substitute
For process state 6:
Substitute
The mass flow rate of water at the bottom exit of separator (state 6) is expressed as follows.
Substitute
Thus, the exergy of the geothermal liquid at the exit of the flash chamber, and the exergy destruction is
(c)
The exergy destruction and second law of efficiency for the turbine.
Answer to Problem 69P
The exergy destruction and second law of efficiency for the turbine is
Explanation of Solution
Write the formula for rate of exergy destruction of the turbine.
Write the formula for second law of efficiency of the turbine.
Conclusion:
Substitute
Substitute
Thus, the exergy destruction and second law of efficiency for the turbine is
(d)
The exergy destruction and second law of efficiency for the entire plant.
Answer to Problem 69P
The exergy destruction and second law of efficiency for the plant is
Explanation of Solution
Write the formula for rate of exergy input of the plant.
Write the formula for rate of exergy destruction of the plant.
Write the formula for second law of efficiency of the plant.
Conclusion:
Substitute
Substitute
Substitute
Thus, the exergy destruction and second law of efficiency for the plant is
Want to see more full solutions like this?
Chapter 10 Solutions
CONNECT FOR THERMODYNAMICS: AN ENGINEERI
- Q Derive (continuity equation)? I want to derive clear mathematics.arrow_forwardmotor supplies 200 kW at 6 Hz to flange A of the shaft shown in Figure. Gear B transfers 125 W of power to operating machinery in the factory, and the remaining power in the shaft is mansferred by gear D. Shafts (1) and (2) are solid aluminum (G = 28 GPa) shafts that have the same diameter and an allowable shear stress of t= 40 MPa. Shaft (3) is a solid steel (G = 80 GPa) shaft with an allowable shear stress of t = 55 MPa. Determine: a) the minimum permissible diameter for aluminum shafts (1) and (2) b) the minimum permissible diameter for steel shaft (3). c) the rotation angle of gear D with respect to flange A if the shafts have the minimum permissible diameters as determined in (a) and (b).arrow_forwardFirst monthly exam Gas dynamics Third stage Q1/Water at 15° C flow through a 300 mm diameter riveted steel pipe, E-3 mm with a head loss of 6 m in 300 m length. Determine the flow rate in pipe. Use moody chart. Q2/ Assume a car's exhaust system can be approximated as 14 ft long and 0.125 ft-diameter cast-iron pipe ( = 0.00085 ft) with the equivalent of (6) regular 90° flanged elbows (KL = 0.3) and a muffler. The muffler acts as a resistor with a loss coefficient of KL= 8.5. Determine the pressure at the beginning of the exhaust system (pl) if the flowrate is 0.10 cfs, and the exhaust has the same properties as air.(p = 1.74 × 10-3 slug/ft³, u= 4.7 x 10-7 lb.s/ft²) Use moody chart (1) MIDAS Kel=0.3 Q3/Liquid ammonia at -20°C is flowing through a 30 m long section of a 5 mm diameter copper tube(e = 1.5 × 10-6 m) at a rate of 0.15 kg/s. Determine the pressure drop and the head losses. .μ= 2.36 × 10-4 kg/m.s)p = 665.1 kg/m³arrow_forward
- 2/Y Y+1 2Cp Q1/ Show that Cda Az x P1 mactual Cdf Af R/T₁ 2pf(P1-P2-zxgxpf) Q2/ A simple jet carburetor has to supply 5 Kg of air per minute. The air is at a pressure of 1.013 bar and a temperature of 27 °C. Calculate the throat diameter of the choke for air flow velocity of 90 m/sec. Take velocity coefficient to be 0.8. Assume isentropic flow and the flow to be compressible. Quiz/ Determine the air-fuel ratio supplied at 5000 m altitude by a carburetor which is adjusted to give an air-fuel ratio of 14:1 at sea level where air temperature is 27 °C and pressure is 1.013 bar. The temperature of air decreases with altitude as given by the expression The air pressure decreases with altitude as per relation h = 19200 log10 (1.013), where P is in bar. State any assumptions made. t = ts P 0.0065harrow_forward36 2) Use the method of MEMBERS to determine the true magnitude and direction of the forces in members1 and 2 of the frame shown below in Fig 3.2. 300lbs/ft member-1 member-2 30° Fig 3.2. https://brightspace.cuny.edu/d21/le/content/433117/viewContent/29873977/Viewarrow_forwardCan you solve this for me?arrow_forward
- 5670 mm The apartment in the ground floor of three floors building in Fig. in Baghdad city. The details of walls, roof, windows and door are shown. The window is a double glazing and air space thickness is 1.3cm Poorly Fitted-with Storm Sash with wood strip and storm window of 0.6 cm glass thickness. The thickness of door is 2.5 cm. The door is Poor Installation. There are two peoples in each room. The height of room is 280 cm. assume the indoor design conditions are 25°C DBT and 50 RH, and moisture content of 8 gw/kga. The moisture content of outdoor is 10.5 gw/kga. Calculate heat gain for living room : الشقة في الطابق الأرضي من مبنى ثلاثة طوابق في مدينة بغداد يظهر في مخطط الشقة تفاصيل الجدران والسقف والنوافذ والباب. النافذة عبارة عن زجاج مزدوج وسمك الفراغ الهوائي 1.3 سم ضعيف الاحكام مع ساتر حماية مع إطار خشبي والنافذة بسماكة زجاج 0.6 سم سماكة الباب 2.5 سم. الباب هو تركيب ضعيف هناك شخصان في كل غرفة. ارتفاع الغرفة 280 سم. افترض أن ظروف التصميم الداخلي هي DBT25 و R50 ، ومحتوى الرطوبة 8…arrow_forwardHow do i solve this problem?arrow_forwardQ4/ A compressor is driven motor by mean of a flat belt of thickness 10 mm and a width of 250 mm. The motor pulley is 300 mm diameter and run at 900 rpm and the compressor pulley is 1500 mm diameter. The shaft center distance is 1.5 m. The angle of contact of the smaller pulley is 220° and on the larger pulley is 270°. The coefficient of friction between the belt and the small pulley is 0.3, and between the belt and the large pulley is 0.25. The maximum allowable belt stress is 2 MPa and the belt density is 970 kg/m³. (a) What is the power capacity of the drive and (b) If the small pulley replaced by V-grooved pulley of diameter 300 mm, grooved angle of 34° and the coefficient of friction between belt and grooved pulley is 0.35. What will be the power capacity in this case, assuming that the diameter of the large pulley remain the same of 1500 mm.arrow_forward
- You are tasked with designing a power drive system to transmit power between a motor and a conveyor belt in a manufacturing facility as illustrated in figure. The design must ensure efficient power transmission, reliability, and safety. Given the following specifications and constraints, design drive system for this application: Specifications: Motor Power: The electric motor provides 10 kW of power at 1,500 RPM. Output Speed: The output shaft should rotate at 150 rpm. Design Decisions: Transmission ratio: Determine the necessary drive ratio for the system. Shaft Diameter: Design the shafts for both the motor and the conveyor end. Material Selection: Choose appropriate materials for the gears, shafts. Bearings: Select suitable rolling element bearings. Constraints: Space Limitation: The available space for the gear drive system is limited to a 1-meter-long section. Attribute 4 of CEP Depth of knowledge required Fundamentals-based, first principles analytical approach…arrow_forward- | العنوان In non-continuous dieless drawing process for copper tube as shown in Fig. (1), take the following data: Do-20mm, to=3mm, D=12mm, ti/to=0.6 and v.-15mm/s. Calculate: (1) area reduction RA, (2) drawing velocity v. Knowing that: ti: final thickness V. Fig. (1) ofthrearrow_forwardA direct extrusion operation produces the cross section shown in Fig. (2) from an aluminum billet whose diameter 160 mm and length - 700 mm. Determine the length of the extruded section at the end of the operation if the die angle -14° 60 X Fig. (2) Note: all dimensions in mm.arrow_forward
- Principles of Heat Transfer (Activate Learning wi...Mechanical EngineeringISBN:9781305387102Author:Kreith, Frank; Manglik, Raj M.Publisher:Cengage Learning