GAS TURBINE ENGINE COMBUSTOR WITH DILUTION PASSAGES

A combustor including an annular liner (206, 208), a dome wall (202), a combustion chamber, at least one fuel cup (204) and at least one dilution passage (212). The fuel cup (204) being provided on the dome wall (202) and being fluidly coupled to the combustion chamber. The fuel cup (204) defining a fuel cup centerline (210). The at least on dilution passage (212) terminating in at least on slot (214) opening onto the dome wall (202), with the slot (214) having a longitudinal body axis (216).