| 摘要 |
<p>A method for repairing a combustor 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 removing a portion of a combustor liner (140) to form a deficit in the liner (140); providing a replacement panel (240) having at least one opening (96) and a thermal barrier material (110) applied to the replacement panel (240) adjacent to the opening (96), and installing the replacement panel (240) in the deficit.</p> |
