GAS TURBINE ENGINE INNER CASE INCLUDING NON-SYMMETRICAL BLEED SLOTS
    3.
    发明公开
    GAS TURBINE ENGINE INNER CASE INCLUDING NON-SYMMETRICAL BLEED SLOTS 审中-公开
    GASTURBINENMOTOR-INNENGEHÄUSEMIT UNSYMMETRISCHENENTLÜFTUNGSSCHLITZEN

    公开(公告)号:EP2935804A4

    公开(公告)日:2016-08-17

    申请号:EP13865842

    申请日:2013-03-05

    Abstract: A compressor of a gas turbine engine includes a plurality of rotors rotatable about a central longitudinal axis, a plurality of stators, and a circumferential inner case wall located outwardly of the plurality of rotors and the plurality of stators. The inner case wall includes a plurality of first slots located in a first section of the circumferential inner case wall and a plurality of second slots located in at least one second section of the circumferential inner case wall. A first area of each of the first slots is greater than a second area of each of the second slots. A circumferential manifold is located outwardly of the inner case wall including a port. At least one of the plurality of second slots is located proximate to the port.

    Abstract translation: 燃气涡轮发动机的压缩机包括可围绕中心纵轴线旋转的多个转子,多个定子以及位于多个转子和多个定子外侧的周向内壳体壁。 内壳壁包括位于周向内壳壁的第一部分中的多个第一槽和位于周向内壳壁的至少一个第二部分中的多个第二槽。 每个第一槽的第一区域大于每个第二槽的第二区域。 圆周歧管位于包括端口的内壳壁的外侧。 多个第二槽中的至少一个位于端口附近。

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