Hello everyone. I would love to get some insight on why IGVs closing on a gas turbine increases its exhaust temperature.
Reading manuals, posts on forums, and O&M manuals, I've gotten to this so far: Reducing the airflow through the axial compressor on a gas turbine changes the air-to-fuel ratio (reduces air), enriching the mixture. However, according to my research, rich mixtures tend to burn at lower temperatures.
Am I on the right track here? Or am I missing something? I am by no means a combustion specialist/engineer. I'm just trying to understand what's going on in our gas turbine for some fine HRSG steam temperature control fine-tuning.
Thanks in advance!
Reading manuals, posts on forums, and O&M manuals, I've gotten to this so far: Reducing the airflow through the axial compressor on a gas turbine changes the air-to-fuel ratio (reduces air), enriching the mixture. However, according to my research, rich mixtures tend to burn at lower temperatures.
Am I on the right track here? Or am I missing something? I am by no means a combustion specialist/engineer. I'm just trying to understand what's going on in our gas turbine for some fine HRSG steam temperature control fine-tuning.
Thanks in advance!
