Recently our Frame6B gas turbine in boroscopic inspection we found first stage turbine nozzle tip damaged & fuel nozzle crack. the reason is one of the combuster liner lock plate broke and that piece entered the turbine. later we replaced the first stage nozzles, fuel nozzles and throughly inspected the other stages too. After the installation when we started the gas turbine we are facing high spread only on base load in both fuels, we checked bleed valves , thermocouple tips, sealing air but we have not found any defect in any of them. the thermocouples which are low and high are adjacent thermocouples i.e TTXD1_3 and 4 second highest is TTXD1_16 which always almost equal to first highest.
why spread going high only at baseload or near base load only?
what could be the reason of the adjacent thermocouples showing such a high variation?
Any sort of ideas are very valuable for us... will be waiting for ur valuable ideas
TY
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