Combustor for gas turbine engine

摘要

A gas turbine engine has a combustor module (10) including an annular combustor having a liner assembly that defines an annular combustion chamber. The liner assembly includes an inner liner (32) and an outer liner (34) that circumscribes the inner liner (32). The inner liner (32) has a plurality of first combustion air admission holes (66) passing therethrough and the second liner (34) has a plurality of second combustion air admission holes (68) passing therethrough. Each of the first and the second combustion air admission holes (66,68) has a swirler (70,80) disposed therein.