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The combustion can is located on top of the turbine casing and seen on the opposite side of the turbine casing in the picture. The foreground of the picture contains the air relief valve and the connection of the air to the atomizing air supply header.
The combustor fuel nozzles located on the top of the combustion can are set up for liquid fuel operation. Due to the low 4:1 pressure ratio of the machine, any liquid can be burned as long as it can be pumped.
The combustion system requires annual maintenance and more so than the rest of the turbine generator skid. Access in the floor of the upper container allows for access to disassemble the combustor and also the turbine section of the machine where the compressor and turbine impellers can be accessed for the tri-annual hot gas path inspections. A beam is installed in the upper box with a trolley that allows for rigging of components in the lower container. |