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A compressor uses 10,000 BTU/hr of power and contains Nitrogen in its gaseous form in the...
1 MPa Isentropic Efficiency of a Compressor Refrigerant-134a enters an adiabatic compressor as a saturated vapor...
1 MPa Isentropic Efficiency of a Compressor Refrigerant-134a enters an adiabatic compressor as a saturated vapor at 100kPa at a rate of 0.7 m/min and exits at 1-MPa pressure. The isentropic efficiency of the compressor is 87%. R-134a Compressor Isentropic Compressor Work hs-h 100 kPa sat. vapor Actual Compressor Work Determine the refrigerant properties at the inlet and outlet for an isentropic process. Actual 2s entropic procEss Inlet state Determine the actual isentropic enthalpy from the efficiency. (Ans: 289.71 J/kg)...
The refrigerant R134a flows through an adiabatic compressor in stationary operation. The volume at the inlet...
The refrigerant R134a flows through an adiabatic compressor in stationary operation. The volume at the inlet is 500 liters / min. At the inlet, the refrigerant is at 0 ° C and 200kPa. At the outlet, the pressure is 1MPa. The compressor has an isentropic efficiency of 85%. The environment of the compressor is at 25 ° C and 100kPa. a) Calculate the specific enthalpy at the compressor outlet (in kJ / kg). Draw a Ts diagram of the process...
A turboprop engine consists of a diffuser, compressor, combustor, turbine, and nozzle. The turbine drives a...
A turboprop engine consists of a diffuser, compressor, combustor, turbine, and nozzle. The turbine drives a propeller as well as the compressor. Air enters the diffuser with a volumetric flow rate of 63.7 m3/s at 40 kPa, 240 K, and a velocity of 180 m/s, and decelerates essentially to zero velocity. The compressor pressure ratio is 9 and the compressor has an isentropic efficiency of 85%. The turbine inlet temperature is 1240 K, and its isentropic efficiency is 85%. The...
For the helicopter gas turbine find the free turbine power for the following case: Engine mass fl...
For the helicopter gas turbine find the free turbine power for the following case: Engine mass flow rate 1.5kgs-1 Compressor pressure ratio 8:1 Compressor isentropic efficiency 0.89 Inlet temperature 300K Max cycle temperature 1100K High pressure turbine isentropic efficiency 0.93 Free turbine isentropic efficiency 0.95 275 wc--285k] kg-1, 275 v t-285k] kg. (T2s-544K, T2-574K, T4-826K, T4s-806K, P3/P4-2.9ro, p4/ps-2-668, T5s 623K, .T5-633K, wtf-200 kJ kg, W'tf-3eekw) 2 613 194 291 Note: for all calculations take Cp-1.004kJ kg-1 K-1, y-1.4
For the...
The centrifugal compressor shown here compresses air from 100 kPa, 27 °C to 600 kPa. This...
The centrifugal compressor shown here compresses air from 100 kPa, 27 °C to 600 kPa. This compressor has an isentropic efficiency of 85%. What is the air temperature at the compressor outlet and how much power does it require if the air volumetric flow rate is 9 m3/min at the compressor inlet? ideal has-hi 1 halt hasthi K- K TI OUT CH 300 =.599 Tas AR ENTERS f1technical.net .S99T25=100
Question A.1 A schematic of a gas turbine combined cycle generating plant is shown in Figure...
Question A.1 A schematic of a gas turbine combined cycle generating plant is shown in Figure A1.1 on the next page. Exhaust gas from the gas turbine generator pass througha heat recovery steam generator (HRSG) which generates steam to drive a steam turbine generator. The following data is provided for the plant: Gas turbine 18.9:1 Pressure ratio Compressor air inlet temperature Turbine inlet temperature 15°C t 273 288 1350°C +273- 1623 588 kg/s T, T3 Exhaust gas mass flow Isentropic...
A one stage axial air compressor consists of a rotor and a stator, it has a...
A one stage axial air compressor consists of a rotor and a stator, it has a mean diameter of Im for the rotor and a rotational speed of 7645 RPM. Furthermore: Mass flow rate is 50 kg/s .Inlet static temperature and pressure of Ti 276 K and Pi 85 kPa. .Inlet stagnation temperature and pressure of Toi 290 K and Poi 101.3 kPa. .Inlet absolute velocity C1 166.5 m/s Rotor exit static density (p2) equals to 1.3kg/m3 Axial component of...
ta Vew Wiadcw Helpr Home Tocls 101 2019.0.Cot QUESTION 9 In a jet engine rotor the high pressure axial compressor ro...
ta Vew Wiadcw Helpr Home Tocls 101 2019.0.Cot QUESTION 9 In a jet engine rotor the high pressure axial compressor rotates at a speed of 15000 rpm. The overall stagnation pressure ratio due to compression is 10.1, it was recorded that the air flows at a rate of 16 kg/s. The stagnation properties at the inlet are 215 kPa and 460K. The poly-tropic efficiency of the compressor is 90%. Assume the mean radius of the compressor is constant and equal...
Section B – combined cycles Overview: a combined gas – steam power cycle in Sweden provides...
Section B – combined cycles Overview: a combined gas – steam power cycle in Sweden provides electricity and hot water for heating duties for a small city. The gas turbine drives an electricity generator with an efficiency of 97%. A sub-critical coal fired boiler is used as a heat recovery steam generator, as well as providing additional steam from coal during the winter months. The steam turbine drives an electricity generator with an efficiency of 95%. The plant is located...
Problem 1 (15 pts) A gas turbine cycle operates with a compressor pressure ratio of 12...
Problem 1 (15 pts) A gas turbine cycle operates with a compressor pressure ratio of 12 and a mass flow rate of 5.0 kg/s. Air enters the compressor at 1 bar, 290 K. The maximum cycle temperature is 1600 K. For the compressor, the isentropic efficiency is 85%, and for the turbine the isentropic efficiency is 90%. Using an air-standard analysis with air as ideal gas with constant specific heats, calculate: a) the volumetric flow rate of air entering the...
1 MPa Isentropic Efficiency of a Compressor Refrigerant-134a enters an adiabatic compressor as a saturated vapor at 100kPa at a rate of 0.7 m/min and exits at 1-MPa pressure. The isentropic efficiency of the compressor is 87%. R-134a Compressor Isentropic Compressor Work hs-h 100 kPa sat. vapor Actual Compressor Work Determine the refrigerant properties at the inlet and outlet for an isentropic process. Actual 2s entropic procEss Inlet state Determine the actual isentropic enthalpy from the efficiency. (Ans: 289.71 J/kg)...
For the helicopter gas turbine find the free turbine power for the following case: Engine mass flow rate 1.5kgs-1 Compressor pressure ratio 8:1 Compressor isentropic efficiency 0.89 Inlet temperature 300K Max cycle temperature 1100K High pressure turbine isentropic efficiency 0.93 Free turbine isentropic efficiency 0.95 275 wc--285k] kg-1, 275 v t-285k] kg. (T2s-544K, T2-574K, T4-826K, T4s-806K, P3/P4-2.9ro, p4/ps-2-668, T5s 623K, .T5-633K, wtf-200 kJ kg, W'tf-3eekw) 2 613 194 291 Note: for all calculations take Cp-1.004kJ kg-1 K-1, y-1.4
For the...
The centrifugal compressor shown here compresses air from 100 kPa, 27 °C to 600 kPa. This compressor has an isentropic efficiency of 85%. What is the air temperature at the compressor outlet and how much power does it require if the air volumetric flow rate is 9 m3/min at the compressor inlet? ideal has-hi 1 halt hasthi K- K TI OUT CH 300 =.599 Tas AR ENTERS f1technical.net .S99T25=100
Question A.1 A schematic of a gas turbine combined cycle generating plant is shown in Figure A1.1 on the next page. Exhaust gas from the gas turbine generator pass througha heat recovery steam generator (HRSG) which generates steam to drive a steam turbine generator. The following data is provided for the plant: Gas turbine 18.9:1 Pressure ratio Compressor air inlet temperature Turbine inlet temperature 15°C t 273 288 1350°C +273- 1623 588 kg/s T, T3 Exhaust gas mass flow Isentropic...
A one stage axial air compressor consists of a rotor and a stator, it has a mean diameter of Im for the rotor and a rotational speed of 7645 RPM. Furthermore: Mass flow rate is 50 kg/s .Inlet static temperature and pressure of Ti 276 K and Pi 85 kPa. .Inlet stagnation temperature and pressure of Toi 290 K and Poi 101.3 kPa. .Inlet absolute velocity C1 166.5 m/s Rotor exit static density (p2) equals to 1.3kg/m3 Axial component of...
ta Vew Wiadcw Helpr Home Tocls 101 2019.0.Cot QUESTION 9 In a jet engine rotor the high pressure axial compressor rotates at a speed of 15000 rpm. The overall stagnation pressure ratio due to compression is 10.1, it was recorded that the air flows at a rate of 16 kg/s. The stagnation properties at the inlet are 215 kPa and 460K. The poly-tropic efficiency of the compressor is 90%. Assume the mean radius of the compressor is constant and equal...
Problem 1 (15 pts) A gas turbine cycle operates with a compressor pressure ratio of 12 and a mass flow rate of 5.0 kg/s. Air enters the compressor at 1 bar, 290 K. The maximum cycle temperature is 1600 K. For the compressor, the isentropic efficiency is 85%, and for the turbine the isentropic efficiency is 90%. Using an air-standard analysis with air as ideal gas with constant specific heats, calculate: a) the volumetric flow rate of air entering the...
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