Methods for repairing combustor liners
AssigneeGeneral Electric Company
InventorEdward John Emilianowicz
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Abstract
A method for repairing a combustor liner for a gas turbine engine combustor, the combustor having a combustion zone formed by inner and outer liners, the method comprising the steps of removing a portion of a combustor liner to form a deficit in the liner; providing a replacement panel having at least one opening and a thermal barrier material applied to the replacement panel adjacent to the opening, and installing the replacement panel in the deficit.
Claims6
A method for repairing a combustor liner for a gas turbine engine combustor, the combustor having a combustion zone formed by inner and outer liners, said method comprising the steps of:
- removing a portion of a combustor liner to form a deficit in said liner;
- providing a replacement panel having at least one opening and a thermal barrier material applied to said replacement panel adjacent to said opening;
- and
- installing said replacement panel in said deficit.
Dependencies are inferred from the claim text.