发明申请
US20120186256A1 MIXER ASSEMBLY FOR A GAS TURBINE ENGINE 有权
燃气轮机发动机混合器总成

MIXER ASSEMBLY FOR A GAS TURBINE ENGINE
摘要:
A mixer assembly for a gas turbine engine is provided, including a main mixer with fuel injection holes located between at least one radial swirler and at least one axial swirler, wherein the fuel injected into the main mixer is atomized and dispersed by the air flowing through the radial swirler and the axial swirler.
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