Thermodynamics lecture 13
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Transcript of Thermodynamics lecture 13
BITS PilaniBITS PilaniPilani Campus
Lecture 13 FIRST LAW ANALYSIS FORLecture 13 – FIRST- LAW ANALYSIS FOR A CONTROL VOLUME
Compressor
A compressor receives 0.1 kg/s R-134a at 150gkPa, -10oC and delivers it at 1000 kPa, 40oC.The power input is measured to be 3 kW. The
h h t t f t i t 100 kPcompressor has heat transfer to air at 100 kPacoming in at 20oC and leaving at 25oC. Howmuch is the mass flow rate of air?much is the mass flow rate of air?
BITS Pilani, Pilani Campus
Mixing Chamber
In engineering applications, thesection where the mixingprocess takes place iscommonly referred to as aymixing chamber
The T elbow of an ordinary shower serves as the
BITS Pilani, Pilani Campus
The T-elbow of an ordinary shower serves as the mixing chamber for the hot- and the cold-water streams.
Thermal Power PlantEquipments Involved with simple Thermal Power
Thermal Power Plant
Plant• Boiler• Turbine• Condenser• Pump
BITS Pilani, Pilani Campus
Thermal Power Plant
BITS Pilani, Deemed to be University under Section 3 of UGC Act, 1956
Thermal Power Plant
BITS Pilani, Deemed to be University under Section 3 of UGC Act, 1956
Thermal Power Plant
BITS Pilani, Deemed to be University under Section 3 of UGC Act, 1956
Thermal Power Plant
Boiler
BITS Pilani, Deemed to be University under Section 3 of UGC Act, 1956
Boiler
Multi component systems
BITS Pilani, Deemed to be University under Section 3 of UGC Act, 1956
Multi component systems
BITS Pilani, Deemed to be University under Section 3 of UGC Act, 1956
Multi component systems
A modern jet engine has a temperature afterb ti f b t 1500 K t 3200 kP it tcombustion of about 1500 K at 3200 kPa as it enters
the turbine section, see state 3 Fig. P.6.100. Thecompressor inlet is 80 kPa 260 K state 1 and outletcompressor inlet is 80 kPa, 260 K state 1 and outletstate 2 is 3300 kPa, 780 K; the turbine outlet state 4into the nozzle is 400 kPa, 900 K and nozzle exit,state 5 at 80 kPa, 640 K. Neglect any heat transferand neglect kinetic energy except out of the nozzle.Find the compressor and turbine specific work termsand the nozzle exit velocity.
BITS Pilani, Deemed to be University under Section 3 of UGC Act, 1956
Multi component systems
BITS Pilani, Deemed to be University under Section 3 of UGC Act, 1956
Refrigerator
Equipments Involved with Refrigerator
• Evaporator• Compressor• Condenser• Throttling Valve
BITS Pilani, Pilani Campus
Refrigerator
BITS Pilani, Pilani Campus
Refrigerator
BITS Pilani, Pilani Campus
Refrigerator
A R-410a heat pump cycle (refrigerator) shown in Fig. P6.99 has a R-410a flow rate of 0.05 kg/s with 5 kW into the compressor. The following data are given
Calculate the heat transfer from the compressor, the heat transfer from the R-410a in the condenser and the heat transfer to the R-410a in the evaporator
BITS Pilani, Pilani Campus
transfer to the R 410a in the evaporator.
Refrigerator
BITS Pilani, Pilani Campus