Gas turbine engine and combustor therefor

Abstract

A combustor for a turbine engine including a dome wall; a combustor liner extending from the dome wall; a combustion chamber at least partially defined by the dome wall and the combustor liner; a fuel cup disposed at a dome wall section of the dome wall, the fuel cup comprising a fuel cup centerline; a set of air tubes extending at least partially through the dome wall section to direct air into the combustion chamber; and a set of cooling holes extending through the dome wall section.

Dependencies are inferred from the claim text.