Combustor with dilution opening

A gas turbine engine includes a compressor section and a combustion section in a serial flow arrangement along an engine centerline, the combustion section having a combustor liner, a dome wall coupled to the combustor liner and a dome inlet in the dome wall, a fuel injector fluidly coupled to the dome inlet, a combustion chamber fluidly coupled to the fuel injector and at least partially defined by the combustor liner and the domed wall, and at least one set of dilution openings in the domed wall and fluidly coupled to the combustion chamber. 一种燃气涡轮发动机，包括沿着发动机中心线处于串行流动布置的压缩机区段和燃烧区段，燃烧区段具有燃烧器衬里，联接到燃烧器衬里的圆顶壁和位于圆顶壁中的圆顶入口，流体联接到圆顶入口的燃料喷射器，流体联接到燃料喷射器并且至少部分由燃烧器衬里和圆顶壁限定的燃烧室，以及位于圆顶壁中并且流体联接到燃烧室的至少一组稀释开口。