system for reducing wear on a gas turbine combustion system, method for reducing wear on a gas turbine combustion system and wear resistant solid material

摘要

system and method for reducing wear in a gas turbine combustion system. The invention relates to systems and methods for providing wear reduction of a gas turbine combustion system. the wear reduction system includes at least one substantially h-shaped block (202), the substantially h-shaped block (202) being configured to secure a transition piece (10) of a gas turbine combustor to a support piece; a first insert including tungsten carbide in a first metal matrix, the metal matrix is selected from a group including cobalt and nickel; and a brazing material that is used for welding the first insert and the at least one substantially h-shaped block (202) at at least one location on the inner wear surface of the at least one substantially h-shaped block (202) .