B
Our gas turbine is a GE MS5002D model, designed to run three centrifugal compressors BCL in series (gas compression process).
My question is: if the discharge pressure of the load increase what will happen to the engine (the speed of LP shaft). I mean the turbine request more energy or less.
for example my machine was running at 99%TNL, and the discharge pressure of the header was 220 barg.
if the pressure in the header will be 250, what will happen to the speed TNL?
thank you in advance
My question is: if the discharge pressure of the load increase what will happen to the engine (the speed of LP shaft). I mean the turbine request more energy or less.
for example my machine was running at 99%TNL, and the discharge pressure of the header was 220 barg.
if the pressure in the header will be 250, what will happen to the speed TNL?
thank you in advance