Dilution structure for gas turbine engine combustor

The present disclosure is directed to a combustor assembly for a gas turbine engine. The combustor assembly includes a liner defining a combustion chamber therewithin and a pressure plenum surroundingthe liner. The liner defines an opening. The liner includes a walled chute disposed at least partially within the opening. The walled chute defines an inner surface at least partially defining a jetdestabilizer. 本公开针对一种用于燃气涡轮发动机的燃烧器组件。燃烧器组件包括衬里和压力气室，衬里限定在其内的燃烧室，压力气室围绕衬里。衬里限定开口。衬里包括至少部分地安置在开口内的有壁槽。有壁槽限定内表面，内表面至少部分地限定射流扰乱器。