GAS TURBINE SHROUD WITH CERAMIC ABRADABLE COATINGS

摘要

There is provided a gas turbine shroud including a ceramic abradable coating used as a gap adjusting component that can reduce a fluid leakage from a gap and increase turbine efficiency. A gas turbine ceramic abradable coating includes a bond layer (2), a thermal barrier ceramic layer (3), and a porous ceramic abradable layer (4) (hardness may be RC15Y: 80±3). A slit groove (5) is provided in the porous ceramic abradable layer (4) by machining. A width of a rectangular section of the ceramic abradable layer (4) divided by the slit groove (5) may be set to a range of 2 to 7 mm.