RI 6920 Bureau Of Mines Coal-Fired Gas Turbine Research Project - Test Of New Turbine Blade Design

New turbine blades designed to resist ash erosion were tested by the Bureau of Mines in a pilot-scale coal-fired gas turbine. After a total of 1,963 hours, the rotor blades were only slightly eroded; and they had an estimated useful life of 20,000 to 30,000 hours. Changes in aerodynamic design of the blades successfully concentrated the ash at the outer casing, but stepped sidewalls for the rotor drum and wear strips at the bases of the rotor blades are still needed to minimize wear at these points. Stepped sidewalls and wear strips did not adequately protect the stator blades. Ash slightly eroded their leading edges, above the inserts, and cut notches into their trailing edges near the bases. Stator blade life was estimated at 5,000 to 7,500 hours. Blade erosion in these tests was less severe than with previous designs, but more efficient combustors and ash separators are required to reduce the amount and size of ash entering the turbine, to achieve acceptable blade life for commercial operation.