摘要 |
<p>A method for making 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 and outer liners (42,44), the method comprising the steps of forming a panel (240) from a sheet of material suitable for use in a combustor liner (30), forming at least one opening (96) in the sheet of material, and applying a thermal barrier material (110) to the replacement panel (240) adjacent to the opening (96).</p> |