CONTAINMENT CASING FOR AN AERO ENGINE
    1.
    发明申请
    CONTAINMENT CASING FOR AN AERO ENGINE 有权
    AERO发动机的集装箱

    公开(公告)号:US20110076132A1

    公开(公告)日:2011-03-31

    申请号:US12873650

    申请日:2010-09-01

    Abstract: A containment assembly for a turbo fan engine, has a casing arranged in use around a rotatable fan, to form a duct for the fan and a liner element disposed on an interior surface between the casing and blades of a rotatable fan. The liner element includes a body portion mounted in a recess in the casing and a wall portion arranged to form part of an inner wall of the duct. The wall portion and the body portion being attached and defining a containment cavity therebetween for containment of a detached fan blade fragment in use, wherein the wall portion has a moveable portion movable between a first configuration in which it lies substantially flush with the inner wall of the duct, and a second configuration in which it provides an opening through which a fan blade fragment can enter the containment cavity.

    Abstract translation: 用于涡轮风扇发动机的容纳组件具有围绕可旋转风扇布置的壳体,以形成用于风扇的管道和布置在可旋转风扇的壳体和叶片之间的内表面上的衬垫元件。 衬垫元件包括安装在壳体中的凹部中的主体部分和布置成形成管道的内壁的一部分的壁部分。 壁部分和主体部分被连接并且在其间限定了容纳空腔,用于在使用中容纳分离的风扇叶片片段,其中壁部分具有可移动部分的可移动部分,第一构造与第一构造基本上与 管道和第二构造,其中它提供了风扇叶片片段可以通过该开口进入容纳空腔的开口。

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