| 摘要 |
A method of coating a corner interface 14 of a turbine system includes placing a mesh assembly 18 proximate the corner interface 14. The method also includes depositing a coating 16 onto and through the mesh assembly 18 and into the corner interface 14, wherein the mesh assembly 18 dampens a kinetic energy of the coating 16 and secures the coating 16 proximate the corner interface 24. |
