davefitz
Mechanical
- Jan 27, 2003
- 2,927
We have several large combustion gas turbines located in Florida, USA. The gas pipeline company indicates that the source of gas will shift to imported rich LNG in 2007-2008. The new fuel gas will have 1.2% butane and 2.75% propane.
According to technical papers based on lab tests of model combustors, the increase in butane and propane will increase the exhaust levels of CO and unburned hydrocarbons, and these unburned hydrocarbons will form radicals HO2 and O which will oxidize NO to NO2. However, I am not able to find any reports of actual field test data from operating gas turbines that burn rich LNG.
Can anyone advise if they have access to test data of gas turbines that burn rich LNG ( Japan, Korea, Spain), if so, what is the expected increase in exhaust NO2 levels?
If the NO2 level exceeds 13 ppm in a simple cycle turibne, the exhaust will exhibit a visible "yellow plume". If the ratio of NO2/NO exceeds 1:1, then the SCR performance will suffer.
According to technical papers based on lab tests of model combustors, the increase in butane and propane will increase the exhaust levels of CO and unburned hydrocarbons, and these unburned hydrocarbons will form radicals HO2 and O which will oxidize NO to NO2. However, I am not able to find any reports of actual field test data from operating gas turbines that burn rich LNG.
Can anyone advise if they have access to test data of gas turbines that burn rich LNG ( Japan, Korea, Spain), if so, what is the expected increase in exhaust NO2 levels?
If the NO2 level exceeds 13 ppm in a simple cycle turibne, the exhaust will exhibit a visible "yellow plume". If the ratio of NO2/NO exceeds 1:1, then the SCR performance will suffer.