FAN AXIAL CONTAINMENT SYSTEM
    8.
    发明公开
    FAN AXIAL CONTAINMENT SYSTEM 有权
    EINSCHLUSSSYSTEMFÜREINENLÜFTER

    公开(公告)号:EP2971676A4

    公开(公告)日:2016-11-16

    申请号:EP14769463

    申请日:2014-03-13

    发明人: MCCUNE MICHAEL E

    摘要: A gas turbine engine (20) and method for containing a fan inside an engine after a fan thrust bearing assembly failure. The engine (20) may comprise a fan (42), a housing (100) including a compartment (102), a fan shaft (104) inside the compartment (102) and comprising a bowl (108), a support structure (110) inside the compartment (102), a speed sensor pickup (114) mounted on the outer surface (120) of the bowl (108), a speed sensor (112) mounted on the support structure (110), and a fan thrust bearing assembly (41) disposed forward of the bowl (108). The fan thrust bearing assembly (41) including a bearing (126). The speed sensor (112) and the sensor pickup (114) define a defining a sensor gap (116). The bearing (126) and the outer surface (120) defining a fan thrust bearing gap (130), wherein the sensor gap (116) is less than the fan thrust bearing gap.

    摘要翻译: 一种燃气涡轮发动机(20)以及在风扇推力轴承组件发生故障后在发动机内容纳风扇的方法。 发动机(20)可以包括风扇(42),包括隔室(102)的壳体(100),隔室(102)内的风扇轴(104),并且包括碗(108),支撑结构(110) ),安装在所述碗(108)的外表面(120)上的速度传感器拾取器(114),安装在所述支撑结构(110)上的速度传感器(112),以及风扇推力轴承 组件(41)布置在碗(108)的前方。 风扇推力轴承组件(41)包括轴承(126)。 速度传感器(112)和传感器拾取器(114)限定了传感器间隙(116)。 轴承(126)和外表面(120)限定了风扇推力轴承间隙(130),其中传感器间隙(116)小于风扇推力轴承间隙。