Case study
An assessment of the effects of a solid fuel on the stationary inlet blades of a gas turbine was undertaken. This included combustion of the solid fuel to determine actual size of the flyash and the gas and particulate distribution and velocities. Suitability of the fuel for gas turbine operations was also assessed.
A specification for grinding size of the solid fuel was developed.
The use of modelling software in the preliminary phase, avoided the need for expensive pilot scale testing. |