Refrigerant vapor enters into the compressor of a standard vapor compression cycle at 10°C (h= 402 kJ/kg) and leaves the compression at 50°C(h= 432 kJ/kg). It leaves the condenser at 30°C (h= 237 kJ/kg). The COP of the cycle is
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- An ideal diesel engine has a compression ratio of 20 and uses air as the working fluid. The state of air at the beginning of the compression process is 95 kPa and 20°C. If the maximum temperature in the cycle is not to exceed 2200 K, determine the net work of the system as a function of compression ratio, r.Consider an ideal gas-turbine cycle with two stages of compression and two stages of expansion. The pressure ratio across each stage of the compressor and turbine is 3. The air enters each stage of the compressor at 300 K and each stage of the turbine at 1200 K. Determine the back work ratio and the thermal efficiency of the cycle, assuming no regenerator is used.An ideal diesel engine has a compression ratio of 20 and uses air as the working fluid. The state of air at the beginning of the compression process is 95 kPa and 20°C. If the maximum temperature in the cycle is not to exceed 2200 K, determine the thermal efficiency.
- An ideal diesel engine has a compression ratio of 20 and uses air as the working fluid. The state of air at the beginning of the compression process is 95 kPa and 20°C. If the maximum temperature in the cycle is not to exceed 2200 K, determine the mean effective pressure. Assume constant specific heats for air at room temperature.1.An ideal Otto cycle has a compression ratio of 8. At the beginning of the compression process, air is at 105 kPa and 28 °C, and 850 kJ/kg of heat is transferred to air during the constant-volume heat-addition process. Taking into account the variation of specific heats with temperature, determine (i) the pressure and temperature at the end of the heat addition process, (ii) the net work output, (iii) the thermal efficiency, and (iv) the mean effective pressure for the cycle.Steam at 2000 psia and 1000°F enters the high-pressure turbine of a reheat cycle and is expanded adiabatically and reversibly to 200 psia. The steam is then passed through the superheater, from where it exits at the 950°F temperature. The low-pressure turbine expands the steam reversibly and adiabatically to 1 psia. If 7 lbm/s of steam is used and the circulating pump is assumed to operate ideally, the power produced, the added heat rate, and the cycle efficiency are: a) 7049,76 hp ; 12124,5 Btu/s ; 42,2% b) 7400,77 hp ; 11553,7 Btu/s ; 45,1% c) 8350,08 hp ; 13089,6 Btu/s ; 49,8% d) 7944,76 hp ; 11834,2 Btu/s ; 47,6%
- Otto cycle operating under air standard condition has a compression ratio of 8.0. If the heat added on the cycle amounts to 3500kJ/kg of working substance, determine the peak temperature of the cycle.In an ideal gas turbine cycle with two-stage compression and expansion, the pressure ratio in both stages of the compressor and turbine is 3.8. The air enters both stages of the compressor at 300 K and both stages of the turbine at 1069 K. What will be the thermal efficiency of the cycle if a regenerator with 75% efficiency is used.A steam turbine cycle running on a Rankin cycle between a condenser pressure of 10 kPa and a boiler pressure of 20 MPa, the steam enters the high pressure turbine at a temperature of 600 ° C. The average turbine expands to 800 kPa and then enters the boiler again to be reheated to 500 ° C. The steam leaves the boiler to a low pressure turbine, where it expands to the condenser pressure. If the expansion and compression in the turbine and the pump is isotropic, and the addition of heat is constant pressure, find the efficiency of the cycle. Note point # 1 at the vapor exit region of the condenser
- An air-standard Carnot cycle is executed in a closed system between the temperature limits of 350 and 1200 K. The pressures before and after the isothermal compression are 150 and 300 kPa, respectively. If the net work output per cycle is 0.5 kJ, determine the maximum pressure in the cycle.Air enters the compressor of a regenerative gasturbine engine at 310 K and 100 kPa, where it is compressed to 900 kPa and 650 K. The regenerator has an effectiveness of 80 percent, and the air enters the turbine at 1400 K. For a turbine efficiency of 90 percent, determine the thermal efficiency. Assume variable specific heats for air.A gas turbine cycle with two stage of compression and two stage of expansion, the overall pressure ratio is 9, air enters each stage of compression at 298 K and each stage of turbine at 1200 K. Determine the thermal efficiency of the cycle under the following conditions:- 1- no heat exchanger is used. 2- ideal regenerator is used