Engine propulsion system and methods of assembling the same
    1.
    发明授权
    Engine propulsion system and methods of assembling the same 有权
    发动机推进系统及其组装方法

    公开(公告)号:US08205821B2

    公开(公告)日:2012-06-26

    申请号:US11610077

    申请日:2006-12-13

    IPC分类号: B64C27/22

    摘要: A method for exhausting gas from an aircraft engine assembly is provided. The method includes coupling a first exhaust duct in fluid communication only to a first engine. The first exhaust duct includes a primary outlet and a secondary outlet. The method further includes coupling a second exhaust duct in fluid communication only to a second engine. The second exhaust duct includes a primary outlet and a secondary outlet. The method also includes aligning a portion of the first engine secondary outlet concentrically within a portion of the second engine secondary outlet.

    摘要翻译: 提供了一种从飞行器发动机组件排出气体的方法。 该方法包括将仅与流体连通的第一排气管连接到第一发动机。 第一排气管道包括主出口和次级出口。 该方法还包括将仅与流体连通的第二排气管连接到第二发动机。 第二排气管道包括主出口和次级出口。 该方法还包括将第一发动机次级出口的一部分同心地对准在第二发动机次级出口的一部分内。

    ENGINE PROPULSION SYSTEM AND METHODS OF ASSEMBLING THE SAME
    2.
    发明申请
    ENGINE PROPULSION SYSTEM AND METHODS OF ASSEMBLING THE SAME 有权
    发动机推进系统及其组装方法

    公开(公告)号:US20080141653A1

    公开(公告)日:2008-06-19

    申请号:US11610077

    申请日:2006-12-13

    IPC分类号: F02K9/00

    摘要: A method for exhausting gas from an aircraft engine assembly is provided. The method includes coupling a first exhaust duct in fluid communication only to a first engine. The first exhaust duct includes a primary outlet and a secondary outlet. The method further includes coupling a second exhaust duct in fluid communication only to a second engine. The second exhaust duct includes a primary outlet and a secondary outlet. The method also includes aligning a portion of the first engine secondary outlet concentrically within a portion of the second engine secondary outlet.

    摘要翻译: 提供了一种从飞行器发动机组件排出气体的方法。 该方法包括将仅与流体连通的第一排气管连接到第一发动机。 第一排气管道包括主出口和次级出口。 该方法还包括将仅与流体连通的第二排气管连接到第二发动机。 第二排气管道包括主出口和次级出口。 该方法还包括将第一发动机次级出口的一部分同心地对准在第二发动机次级出口的一部分内。