How does the pressure ratio affect the efficiency of a gas turbine?

  • Thread starter Thread starter Sunfire
  • Start date Start date
  • Tags Tags
    Cycle Efficiency
Click For Summary
SUMMARY

The efficiency of a gas turbine is fundamentally determined by the Brayton cycle and is significantly influenced by the pressure ratio (ε). A high compression ratio can enhance efficiency only if the high-pressure gas is directly supplied to the turbine. If a pressure regulator is used to reduce the gas pressure before it enters the turbine, the efficiency will decrease. Additionally, increasing the turbine inlet temperature and employing methods such as intercooling and regenerators can further improve Brayton cycle efficiency.

PREREQUISITES
  • Understanding of the Brayton cycle in thermodynamics
  • Knowledge of gas turbine operation and components
  • Familiarity with pressure regulation techniques
  • Basic principles of thermodynamic efficiency
NEXT STEPS
  • Research the impact of turbine inlet temperature on Brayton cycle efficiency
  • Study the design and implementation of intercooling in gas turbines
  • Explore the use of regenerators in enhancing gas turbine performance
  • Investigate the limitations and challenges of high-pressure gas turbine components
USEFUL FOR

Engineers, thermodynamics students, and professionals involved in gas turbine design and optimization will benefit from this discussion.

Sunfire
Messages
221
Reaction score
4
Hello,

In http://www.aerostudents.com/files/gasTurbines/gasTurbinesFullVersion.pdf it is shown that the efficiency of a gas turbine is determined by the Brayton cycle and it depends on the pressure ratio ε.

ε is the compression ratio before fossil fuel burning invests further energy into the gas.

I want to be sure that my thinking is correct -

If I build a reservoir and perform a very high compression (high ε), efficiency will be high ONLY if the high-pressure gas is supplied to the turbine, which will now be extracting work from the high pressure gas, correct?

But if I am to build a reservoir and perform a very high compression (high ε), but use a pressure regulator to drop the gas pressure before the gas enters the turbine, the efficiency should drop, correct?

It seems to me that the high ε and high efficiency has to do with the area inside the Brayton cycle curve, e.g. high pressure drops utilize better the internal energy of the supplies gas, correct?
 
Engineering news on Phys.org
Sunfire said:
Hello,

In http://www.aerostudents.com/files/gasTurbines/gasTurbinesFullVersion.pdf it is shown that the efficiency of a gas turbine is determined by the Brayton cycle and it depends on the pressure ratio ε.

The document details how the efficiency of a turbine can be calculated when the Brayton cycle is employed. The efficiency of all gas turbines is not determined by the Brayton cycle.

Engineering very high pressure components is not practical and leads to thick walled vessels, very expensive turbine casings, very expensive pumps, etc ... The other ways to increase the Brayton cycle efficiency is to increase the turbine inlet temperature to the maximum possible that the blade materials can safely operate at. Adding a regenerator and using intercooling between the compressor stages and reheating between the turbine stages can also increase the cycle efficiency.

The second law must be considered because the cycle is only internally reversible. External irreversibility has to be considered.
 
CFDFEAGURU said:
The other ways to increase the Brayton cycle efficiency is to increase the turbine inlet temperature

Could you elaborate on this point? Thank you for your reply.
 

Similar threads

Replies
5
Views
2K
Replies
8
Views
3K
Replies
2
Views
2K
  • · Replies 6 ·
Replies
6
Views
3K
  • · Replies 4 ·
Replies
4
Views
779
  • · Replies 3 ·
Replies
3
Views
3K
  • · Replies 10 ·
Replies
10
Views
5K
  • · Replies 13 ·
Replies
13
Views
5K
  • · Replies 1 ·
Replies
1
Views
2K
  • · Replies 1 ·
Replies
1
Views
3K