METHODS FOR REPAIRING COMBUSTOR LINERS

METHODS FOR REPAIRING COMBUSTOR LINERS 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) t...

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Bibliographische Detailangaben
1. Verfasser:	EMILIANOWICZ, EDWARD JOHN
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING COMBINED OPERATIONS COMBUSTION APPARATUS COMBUSTION PROCESSES GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MACHINE TOOLS MECHANICAL ENGINEERING METAL-WORKING NOT OTHERWISE PROVIDED FOR OTHER WORKING OF METAL PERFORMING OPERATIONS TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION TECHNICAL SUBJECTS COVERED BY FORMER USPC TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TRANSPORTING UNIVERSAL MACHINE TOOLS WEAPONS
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Zusammenfassung:	METHODS FOR REPAIRING COMBUSTOR LINERS 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.