| 摘要 |
<p>A replacement panel (240) for repairing a liner (140) for a gas turbine engine combustor (30), the combustor (30) having a combustion zone (36) formed by inner (42) and outer (44) liners, the replacement panel (240) comprising a sheet of material suitable for use in a combustor liner (140), at least one opening (96) in the sheet of material, a thermal barrier material (110) applied to the sheet of material adjacent the at least one opening (96); and a peripheral edge (245) free of thermal barrier material (110).</p> |
