General Electric Company

Kamil Bazyli Kaczorowski

John Carl Jacobson

Joseph Douglas Monty

Aureen Cyr Currin

Mariusz Grzegorz Karpinski

Damian Strzelec

Andrzej Jacek Radlicz

Various embodiments include methods of reinforcing apertures in turbomachine combustors, and related combustors. In various particular embodiments, a method of reinforcing an existing turbomachine combustor aperture includes: broaching the existing aperture to modify an initial profile of the existing aperture and form a modified profile, where the modified profile protrudes radially outwardly from an outer surface of the turbomachine combustor; and welding a combustor ring along an inner surface of the modified profile, where the modified profile enhances bonding between the existing aperture and the combustor ring.

Methods of reinforcing combustor aperture and related combustor

A method for fabricating a dome assembly for a gas turbine engine combustor includes forming an annular dome plate including a plurality of substantially circular eyelets circumferentially spaced thereon, coupling a seal plate to the dome plate at each eyelet such that an opening defined in each seal plate is aligned substantially concentrically with respect to a respective eyelet, coupling a baffle to each seal plate such that an opening defined in each baffle is aligned substantially concentrically with respect to a respective eyelet, and coupling a swirler assembly having an integrally formed swirler and flare cone to each seal plate such that the flare cone extends at least partially through the baffle opening, and such that cooling air may be directed towards the flare cone through openings formed in the assembly.

Methods and apparatus for fabricating gas turbine engine combustors

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Warsaw, Poland

Kamil Bazyli Kaczorowski