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we have a GE gas turbine of frame 9E. if we start the unit at distillate fuel the exhaust spread reaches allowable at fsnl.
The exhaust temperatures shows a cold spot in TC. from 11 to 17 with 250c as average at 10mw. The fqlm1 gives a value of 2.7 kg/s at 10mw which is a high value and a yellow smoke from the stack. the fuel command and feedback is maching.
The LFBV LVDT has been calibrated and magnetic speed pickups at flow divider also have been calibrated. atomizing air pressure at firing moment is 0.5bar. flow divider pressures are similar.
Is there are possibility of un-flamed combustion chambers in the respective cold spot area, and how to check that?
kindly note that starting at gas fuel is normal with reasonable exhaust spreads.
The exhaust temperatures shows a cold spot in TC. from 11 to 17 with 250c as average at 10mw. The fqlm1 gives a value of 2.7 kg/s at 10mw which is a high value and a yellow smoke from the stack. the fuel command and feedback is maching.
The LFBV LVDT has been calibrated and magnetic speed pickups at flow divider also have been calibrated. atomizing air pressure at firing moment is 0.5bar. flow divider pressures are similar.
Is there are possibility of un-flamed combustion chambers in the respective cold spot area, and how to check that?
kindly note that starting at gas fuel is normal with reasonable exhaust spreads.
