ScottyUK
Electrical
- May 21, 2003
- 12,915
Looking for a few ideas:
We have a fleet of eight Mitsubishi MW-701DA turbines. The 701 is essentially a 50Hz variant of the Westinghouse 501.
One of our units suffered a baseload trip while running on distillate in the past week. We are having tremendous problems igniting the machine on natural gas where normally we would expect a first time start. The turbine uses dual igniters in adjacent combuster cans at the approximate 5 o'clock position. Igniters are known to be working. Fuel valves are known to be working. The engine is reaching the normal cranking speed of 650rpm.
We are able to detect gas flow into the engine by measuring the DP developed between the fuel manifold and the combuster shell. The DP is about 14kPa which is the typical lightoff value for this engine design. We can't verify fuel flow to individual cans, so a blocked or damaged nozzle would not be detected by this method. We've tried a slightly lean and slightly rich gas mix relative to normal conditions with no success.
I'm inclined toward thinking we have suffered combuster damage as a result of the trip, but am being fought by others who would like to avoid an internal inspection. I think we have checked everything which is likely to affect ignition - is there anything else I have forgotten to check? Can anyone familiar with the internal design of these machines - or the 501 - offer any other ideas, or either lend support to or discount my theory of internal damage to the combuster?
Thanks.
----------------------------------
I don't suffer from insanity. I enjoy it...
We have a fleet of eight Mitsubishi MW-701DA turbines. The 701 is essentially a 50Hz variant of the Westinghouse 501.
One of our units suffered a baseload trip while running on distillate in the past week. We are having tremendous problems igniting the machine on natural gas where normally we would expect a first time start. The turbine uses dual igniters in adjacent combuster cans at the approximate 5 o'clock position. Igniters are known to be working. Fuel valves are known to be working. The engine is reaching the normal cranking speed of 650rpm.
We are able to detect gas flow into the engine by measuring the DP developed between the fuel manifold and the combuster shell. The DP is about 14kPa which is the typical lightoff value for this engine design. We can't verify fuel flow to individual cans, so a blocked or damaged nozzle would not be detected by this method. We've tried a slightly lean and slightly rich gas mix relative to normal conditions with no success.
I'm inclined toward thinking we have suffered combuster damage as a result of the trip, but am being fought by others who would like to avoid an internal inspection. I think we have checked everything which is likely to affect ignition - is there anything else I have forgotten to check? Can anyone familiar with the internal design of these machines - or the 501 - offer any other ideas, or either lend support to or discount my theory of internal damage to the combuster?
Thanks.
----------------------------------