Mixer assembly for a gas turbine engine

摘要

A mixer assembly (200) for a gas turbine engine is provided, including a main mixer (220) with fuel injection holes (226) located between at least one radial swirler (240) and at least one axial swirler (230), wherein the fuel injected into the main mixer (220) is atomized and dispersed by the air flowing through the radial swirler (240) and the axial swirler (230).