Turbine fan fairing platform with protective surface

    公开(公告)号:US11268396B2

    公开(公告)日:2022-03-08

    申请号:US16746229

    申请日:2020-01-17

    Abstract: A turbine fan fairing platform is disclosed. The turbine fan fairing platform includes a platform body including a first side portion arranged to abut a first fan blade, a second side portion arranged to abut a second fan blade, and a central portion extending between the first side portion and the second side portion. A seal member is disposed over the platform body. The seal member includes a first side portion over the platform body first side portion, a central portion over the platform body the central portion, and a second side portion over the platform body second side portion. An erosion protection layer is disposed over the seal member over the central portion of the platform body.

    TURBINE ENGINE CASE ATTACHMENT AND A METHOD OF USING THE SAME

    公开(公告)号:US20200182153A1

    公开(公告)日:2020-06-11

    申请号:US16730497

    申请日:2019-12-30

    Abstract: The present disclosure relates generally to a turbine engine case assembly, the turbine engine case assembly including a fan case including an outer frame encircling an axis, the outer frame including an outer frame exterior surface and an outer frame interior surface, at least two mounts disposed on the outer frame exterior surface, wherein the at least two mounts are circumferentially spaced along the outer frame exterior surface, and a compliant attachment device operably coupled to the at least two mounts.

    Ground handling system for a composite fan case and a method of using the same

    公开(公告)号:US10202866B2

    公开(公告)日:2019-02-12

    申请号:US14958548

    申请日:2015-12-03

    Inventor: Darin S. Lussier

    Abstract: The present disclosure relates generally to a system for handling a gas turbine engine fan case. The system includes a composite fan containment case including a case outer surface, a case inner surface, and at least one main case aperture extending from the case outer surface through the case inner surface, and at least one shear puck, the at least one shear puck including a shear puck protrusion; wherein the shear puck protrusion of each of the at least one shear pucks is disposed within a respective one of each of the at least one main case apertures.

    CO-MOLDED METALLIC FAN CASE CONTAINMENT RING
    26.
    发明申请
    CO-MOLDED METALLIC FAN CASE CONTAINMENT RING 审中-公开
    CO模具金属风扇箱包装环

    公开(公告)号:US20160369812A1

    公开(公告)日:2016-12-22

    申请号:US15185573

    申请日:2016-06-17

    Abstract: A method of fabricating a fan case for a gas turbine engine defines a metallic ring including an outer surface and an inner surface. A first composite material is assembled about the outer surface of the metallic ring. A second composite material is assembled about the first composite material. The first composite material and the second material are cured about the metallic ring within a tool to form a first subassembly. The first subassembly is removed from the tool. A fan case assembly for a gas turbine engine and a gas turbine engine are also disclosed.

    Abstract translation: 制造用于燃气涡轮发动机的风扇壳体的方法限定了包括外表面和内表面的金属环。 围绕金属环的外表面组装第一复合材料。 围绕第一复合材料组装第二复合材料。 第一复合材料和第二材料围绕工具中的金属环固化以形成第一子组件。 第一个子组件从工具中移除。 还公开了一种用于燃气涡轮发动机和燃气涡轮发动机的风扇壳体组件。

    TURBINE ENGINE CASE ATTACHMENT AND A METHOD OF USING THE SAME
    27.
    发明申请
    TURBINE ENGINE CASE ATTACHMENT AND A METHOD OF USING THE SAME 审中-公开
    涡轮发动机附件及其使用方法

    公开(公告)号:US20160201510A1

    公开(公告)日:2016-07-14

    申请号:US14874049

    申请日:2015-10-02

    Abstract: The present disclosure relates generally to a turbine engine case assembly, the turbine engine case assembly including a fan case including an outer frame encircling an axis, the outer frame including an outer frame exterior surface and an outer frame interior surface, at least two mounts disposed on the outer frame exterior surface, wherein the at least two mounts are circumferentially spaced along the outer frame exterior surface, and a compliant attachment device operably coupled to the at least two mounts.

    Abstract translation: 本发明总体上涉及一种涡轮发动机壳体组件,涡轮发动机壳体组件包括风扇壳体,该风扇壳体包括围绕轴线的外框架,外框架包括外框架外表面和外框架内表面,至少两个安装件设置 在所述外框架外表面上,其中所述至少两个安装件沿着所述外框架外表面沿圆周间隔开,以及柔性附接装置,其可操作地联接到所述至少两个安装件。

    Turbine engine case attachment and a method of using the same

    公开(公告)号:US10519863B2

    公开(公告)日:2019-12-31

    申请号:US14874049

    申请日:2015-10-02

    Abstract: The present disclosure relates generally to a turbine engine case assembly, the turbine engine case assembly including a fan case including an outer frame encircling an axis, the outer frame including an outer frame exterior surface and an outer frame interior surface, at least two mounts disposed on the outer frame exterior surface, wherein the at least two mounts are circumferentially spaced along the outer frame exterior surface, and a compliant attachment device operably coupled to the at least two mounts.

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