Turbine for an aircraft generating swirl in exhaust gases

Abstract

A turbine engine for an aircraft. The turbine engine includes a combustor, an exhaust section, and one or more swirl features. The combustor combusts a fuel and air mixture, and generates combustion gases flowing along a flow path. The exhaust section is downstream of the combustor. The exhaust section receives the combustion gases and exhausts the combustion gases from the turbine engine as exhaust gases flowing along a flow path. The one or more swirl features extend into the flow path of the combustion gases or the flow path of the exhaust gases. The one or more swirl features generate swirl in the exhaust gases to create swirl in an exhaust of the turbine engine.

Dependencies are inferred from the claim text.