Mixer Assembly for a Gas Turbine Engine

Dai, Zhongtao [Inventor]Cohen, Jeffrey M [Inventor]Fotache, Catalin G [Inventor]Smith, Lance L [Inventor]Hautman, Donald J [Inventor]

关键词: MIXERS;    GAS TURBINE ENGINES;    FUEL INJECTION;    HOLES (MECHANICS);    AIR FLOW;    SWIRLING;    COMPRESSORS;    COMBUSTION;    ATOMIZING;    PATENTS;    ELECTRICITY;   

RP-ID  :  US-Patent-9,920,932, US-Patent-Appl-SN-14/593,877

学科分类：航空航天科学

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来源: NASA Technical Reports Server

【 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.