FAN BLADE COMPOSITE RIBS
    31.
    发明公开

    公开(公告)号:EP3063378A4

    公开(公告)日:2017-11-15

    申请号:EP14876029

    申请日:2014-10-09

    Abstract: A fan blade has a blade body, a composite rib and a cover. The blade body extends from a blade root to an opposed blade tip along a longitudinal axis. The blade body defines a leading edge and a trailing edge. A first airfoil surface extends from the leading edge to the trailing edge A pocket is defined between the leading edge, the trailing edge, the blade root, and the blade tip. The pocket has a bottom surface that opposes the first airfoil surface across the blade body. The composite rib is disposed in the pocket. The cover is mounted to the composite rib and the blade body to form a second airfoil surface opposed to the first airfoil surface.

    COVERS FOR CAVITIES IN AIRCRAFT FAN BLADES
    38.
    发明公开
    COVERS FOR CAVITIES IN AIRCRAFT FAN BLADES 有权
    飞机叶片空心室的盖子

    公开(公告)号:EP2964892A4

    公开(公告)日:2016-11-09

    申请号:EP13877424

    申请日:2013-11-08

    Abstract: Hollow fan blades for gas turbine engines are disclosed. The hollow fan blades include a body having a convex side and a concave side wherein the convex side has a cavity formed therein. The cavity is covered by two covers including an inner cover that may be adhered to the body of the fan blade assembly and an outer cover that may be adhered to the inner cover and/or the body of the fan blade assembly. The covers may be made of titanium, more than two covers may be employed and more than one cavity may be employed.

    Abstract translation: 公开了用于燃气涡轮发动机的中空风扇叶片。 中空风扇叶片包括具有凸侧和凹面的主体,其中凸侧具有形成在其中的空腔。 空腔由两个盖子覆盖,其中包括可以粘附到风扇叶片组件的主体的内盖和可以附着到风扇叶片组件的内盖和/或主体的外盖。 盖可以由钛制成,可以使用多于两个的盖,并且可以使用多于一个的空腔。

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