Faceted dome assemblies for gas turbine engine combustors

Details Faceted dome assemblies for gas turbine engine combustors Faceted dome assemblies for gas turbine engine combustors

F - Mech Eng,Light,Heat,Weapons

23

R

F23R 3/42 (2006.01) F02C 7/24 (2006.01)

Patent

CA 2637090

A dome assembly for a gas turbine engine includes a plurality of faceted segments and a plurality of openings. The plurality of faceted segments are coupled together to form a dome structure that is configured to be disposed between an inner liner and an outer liner that circumscribes the inner liner. The plurality of openings are each opening formed within a respective faceted segment, and are configured to at least partially house an atomizer therein. Each faceted segment is at least substantially flat.

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