Combustor liner and method for making thereof

A combustor liner is provided having first and second annular bands which define an overlapping circumferential joint area, wherein a weld is disposed in the joint area encompassing substantially all of the axial length of the joint area. A method for producing such a combustor liner is also provide...

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Bibliographic Details
Main Authors REDDEN RONALD D, DEVANE SHAUN M, GROESCHEN JAMES A, FARMER GILBERT
Format Patent
LanguageEnglish
Published 26.06.2003
Edition7
Subjects
BLASTING
CLADDING OR PLATING BY SOLDERING OR WELDING
COMBUSTION APPARATUS
COMBUSTION PROCESSES
CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING
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
PERFORMING OPERATIONS
SOLDERING OR UNSOLDERING
TRANSPORTING
WEAPONS
WELDING
WORKING BY LASER BEAM
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Summary:A combustor liner is provided having first and second annular bands which define an overlapping circumferential joint area, wherein a weld is disposed in the joint area encompassing substantially all of the axial length of the joint area. A method for producing such a combustor liner is also provided.
Bibliography:Application Number: US20010028028