Isentropic Efficiency of a Compressor

Click For Summary
SUMMARY

The isentropic efficiency of a compressor is defined as the ratio of the isentropic enthalpy change to the actual enthalpy change, expressed mathematically as n=(h2s-h1)/(h2a-h1). In this discussion, the calculated isentropic efficiency was 0.37, while an alternate calculation using temperature instead of pressure yielded an efficiency of 0.72. The conversation highlights the importance of pressure as a primary variable in compressor design, emphasizing that compressors operate between specified pressures rather than temperatures. Additionally, the discussion touches on the implications of irreversibility in turbine processes, where outlet conditions differ from isentropic expectations.

PREREQUISITES
  • Understanding of thermodynamic principles, specifically isentropic processes
  • Familiarity with enthalpy and entropy calculations in thermodynamics
  • Knowledge of compressor and turbine operation principles
  • Experience with refrigerant properties and their calculations
NEXT STEPS
  • Study the calculation of isentropic efficiency in various thermodynamic systems
  • Learn about the role of pressure and temperature in compressor design
  • Explore the differences between isentropic and actual processes in turbines
  • Investigate refrigerant property tables and their application in enthalpy calculations
USEFUL FOR

Mechanical engineers, thermodynamics students, and professionals involved in the design and analysis of compressors and turbines will benefit from this discussion.

bardia sepehrnia
Messages
28
Reaction score
4
Homework Statement
The adiabatic compressor of a refrigeration system compresses saturated R-134a vapor at 0°C to 600 kPa and 50°C. What is the isentropic efficiency of this compressor?
Relevant Equations
n=(h2s-h1)/(h2a-h1)
1617229021353.png


We know that if potential and kinetic energy our negligible, the isentropic efficiency of a compressor is isentropic enthalpy change divided by actual enthalpy change: n=(h2s-h1)/(h2a-h1)
So I already answered this question and here is the answer: n1 is the isentropic efficiency of the compressor (0.37). Also h2a is the actual enthalpy value at the exit, and h2s is the isentropic enthalpy value at the exit (if process was reversible). Entropy (s1) was found as given temperature and quality value for the refrigerant. The entropy at outlet must be equal to entropy at inlet for isentropic process.

1617230341132.png

However, I'm confused about one thing. My lecturer told us that in order to find the isentropic enthalpy value at exit, the enthalpy should be found at the given specific entropy value and "pressure".

Here is my question, why can't we find the enthalpy using temperature as one of the independent properties instead of the pressure? I have calculated the isentropic efficiency using entropy and temperature instead of pressure (h2s_2), and I get a much higher efficiency. (0.72)
 

Attachments

  • 1617229114485.png
    1617229114485.png
    37 KB · Views: 364
Physics news on Phys.org
Because a compressor is designed to operate between two specified pressures, not between two specified temperatures.
 
Chestermiller said:
Because a compressor is designed to operate between two specified pressures, not between two specified temperatures.
I get that. But what if it was a turbine instead and the process was reversed. From high temperature and pressure at inlet, to low temperature and low pressure at the exit. Due to irreversibility, the temperature at the outlet would be "more" than the temperature value for an isentropic (reversible) process since some heat is generated by the turbine. But it could very well be that, the pressure at the outlet is less than the pressure value for an isentropic process at a given temperature.
 
bardia sepehrnia said:
I get that. But what if it was a turbine instead and the process was reversed. From high temperature and pressure at inlet, to low temperature and low pressure at the exit. Due to irreversibility, the temperature at the outlet would be "more" than the temperature value for an isentropic (reversible) process since some heat is generated by the turbine. But it could very well be that, the pressure at the outlet is less than the pressure value for an isentropic process at a given temperature.
Yes. So,...?
 
bardia sepehrnia said:
Here is my question, why can't we find the enthalpy using temperature as one of the independent properties instead of the pressure?
When you want to built a compressor, your objective is to increase the pressure alone. In practice, we note that there is always an increase in temperature which corresponds to a lost. The best we could do is if we did an isentropic compression. This is then the ideal situation. Therefore, we compare our compressor to the ideal one, where you still get a 600 kPa outlet pressure, but at a 24 °C instead of a 50 °C. Less heat loss; but you cannot go lower (without introducing a cooling process).

When you choose to keep the same outlet temperature for the isentropic process - while not caring about the outlet pressure - you are basically saying that you are in fact designing a heater. Your objective IS to reach 50 °C by increasing the pressure. If you were doing it isentropically, well, the temperature doesn't increase much. So you will need to reach a much higher pressure (1163 kPa instead of 600 kPa), which requires a lot more work. Therefore a very inefficient compressor is always a very efficient heater. That is normal since you have an alternative heat source (i.e. friction) that put heat in the system.
 

Similar threads

Replies
2
Views
3K
  • Poll Poll
  • · Replies 9 ·
Replies
9
Views
6K
  • · Replies 6 ·
Replies
6
Views
4K
Replies
21
Views
9K
  • · Replies 2 ·
Replies
2
Views
1K
  • · Replies 8 ·
Replies
8
Views
3K
  • · Replies 14 ·
Replies
14
Views
4K
Replies
1
Views
799
Replies
5
Views
5K
  • · Replies 1 ·
Replies
1
Views
3K