ADDITIVE MANUFACTURED NON-ROUND, SEPTUM TIED, CONFORMAL HIGH PRESSURE TUBING
    27.
    发明申请
    ADDITIVE MANUFACTURED NON-ROUND, SEPTUM TIED, CONFORMAL HIGH PRESSURE TUBING 审中-公开
    添加剂制造的非圆形,均匀的高压管道

    公开(公告)号:US20160333790A1

    公开(公告)日:2016-11-17

    申请号:US15112468

    申请日:2015-01-20

    Abstract: A septum-tied tube pack is provided that includes a first outer wall formed by a multiple of first connected radiuses. A second outer wall is formed by a multiple of second connected radiuses. A first end radius connects the first outer wall and the second outer wall. A second end radius connects the first outer wall and the second outer wall. A multiple of septum elements extend between the first outer wall and the second outer wall. A gas turbine engine is also provided that includes an engine case structure and a fluid conduit mounted to the engine case structure. The fluid conduit includes a septum-tied tube pack section.

    Abstract translation: 提供了隔膜束管,其包括由多个第一连接半径形成的第一外壁。 第二外壁由多个第二连接半径形成。 第一端半径连接第一外壁和第二外壁。 第二端半径连接第一外壁和第二外壁。 多个隔膜元件在第一外壁和第二外壁之间延伸。 还提供了一种燃气涡轮发动机,其包括发动机壳体结构和安装到发动机壳体结构的流体导管。 流体导管包括隔膜束管部分。

    CERAMIC COVERED TURBINE COMPONENTS
    28.
    发明申请
    CERAMIC COVERED TURBINE COMPONENTS 审中-公开
    陶瓷覆盖涡轮组件

    公开(公告)号:US20160326892A1

    公开(公告)日:2016-11-10

    申请号:US15108613

    申请日:2015-01-05

    Abstract: A component for a gas turbine engine comprises an underlying substrate. A plurality of ceramic panels have intermediate thermal expansion joints bonded by a bond layer to the underlying substrate. The thermal expansion joints are formed of a material having a greater coefficient of expansion than a material forming the ceramic panels. The ceramic panels and the thermal expansion joints are positioned to define an outer surface for the component. A gas turbine engine and a component for a gas turbine engine are also disclosed.

    Abstract translation: 用于燃气涡轮发动机的部件包括下面的基板。 多个陶瓷板具有通过接合层与下面的基底结合的中间热膨胀接头。 热膨胀接头由比形成陶瓷板的材料膨胀系数大的材料形成。 陶瓷板和热膨胀接头被定位以限定用于部件的外表面。 还公开了一种燃气涡轮发动机和用于燃气涡轮发动机的部件。

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