COMBUSTOR COMPRISING PANELS WITH SKEWED SIDE WALLS

A combustor of a gas turbine engine including a first forward liner panel (72A-1, 74A-1). The forward liner panel including a liner panel forward edge (130), a liner panel aft edge (132) opposite of the liner panel forward edge, and a first liner panel side edge (134) between the liner panel aft edg...

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Bibliographic Details
Main Authors QUACH, San, KARANIAN, Caroline, STYBORSKI, Jeremy
Format Patent
LanguageEnglish
French
German
Published 30.08.2023
Subjects
BLASTING
CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FORCOMBUSTION CHAMBERS, e.g. FIREBRIDGES
COMBUSTION APPARATUS
COMBUSTION PROCESSES
DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDEDFOR
DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS INCOMBUSTION CHAMBERS
GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
HEATING
LIGHTING
MECHANICAL ENGINEERING
SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTIONAPPARATUS
WEAPONS
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Summary:A combustor of a gas turbine engine including a first forward liner panel (72A-1, 74A-1). The forward liner panel including a liner panel forward edge (130), a liner panel aft edge (132) opposite of the liner panel forward edge, and a first liner panel side edge (134) between the liner panel aft edge and the liner panel forward edge. The first liner panel side edge is non-perpendicular to the liner panel forward edge and oriented at an angle about perpendicular to a swirl flow (I, O) in the combustor.
Bibliography:Application Number: EP20230160757