GEARED TURBOFAN ARCHITECTURE FOR IMPROVED THRUST DENSITY
    212.
    发明公开
    GEARED TURBOFAN ARCHITECTURE FOR IMPROVED THRUST DENSITY 审中-公开
    GETTREBETURBOLÜFTERARCHITEKTURFÜRVERBESSERTE SCHUBDICHTE

    公开(公告)号:EP2820264A4

    公开(公告)日:2015-11-18

    申请号:EP13790528

    申请日:2013-02-22

    CPC classification number: F01D25/162 F02C3/107 F02K3/072 F05D2260/40311

    Abstract: A turbine engine includes a fan, a compressor section having a low pressure compressor section and a high pressure compressor section, a combustor in fluid communication with the compressor section and a turbine section in fluid communication with the combustor. The turbine section includes a low pressure turbine section and a high pressure turbine section. The low pressure compressor section, the low pressure turbine section and the fan rotate in a first direction whereas the high pressure compressor section and the high pressure turbine section rotate in a second direction opposite the first direction.

    Abstract translation: 涡轮发动机包括风扇,具有低压压缩机部分和高压压缩机部分的压缩机部分,与压缩机部分流体连通的燃烧器和与燃烧器流体连通的涡轮部分。 涡轮部分包括低压涡轮部分和高压涡轮部分。 低压压缩机部分,低压涡轮部分和风扇沿第一方向旋转,而高压压缩机部分和高压涡轮部分沿与第一方向相反的第二方向旋转。

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