ENDWALL CONTOURING
    1.
    发明申请
    ENDWALL CONTOURING 审中-公开
    端到端

    公开(公告)号:WO2014070280A3

    公开(公告)日:2014-06-26

    申请号:PCT/US2013054953

    申请日:2013-08-14

    Abstract: An airfoil array is disclosed. The airfoil array may include an endwall, and a plurality of airfoils radially projecting from the endwall. Each airfoil may have a first side and an opposite second side extending axially in chord between a leading edge and a trailing edge. The airfoil array may further include a convex profiled region extending from the endwall adjacent the first side of at least one of said plurality of airfoils and near the leading edge of the at least one of said plurality of airfoils. The airfoil array may further include a concave profiled region in the endwall adjacent the first side of said at least one of said plurality of airfoils and aft of the convex profiled region.

    Abstract translation: 公开了一种翼型阵列。 翼型阵列可以包括端壁和从端壁径向突出的多个翼型件。 每个翼型件可以具有在前缘和后缘之间沿弦向轴向延伸的第一侧和相对的第二侧。 翼型阵列还可以包括从邻近所述多个翼型中的至少一个翼型件的第一侧的端壁延伸并且在所述多个翼型中的至少一个翼型件的前缘附近的凸形轮廓区域。 翼型阵列还可包括邻近所述多个翼型件中的所述至少一个翼型件的第一侧和凸形轮廓区域的后端的端壁中的凹形轮廓区域。

    LOW LOSS AIRFOIL PLATFORM TRAILING EDGE
    3.
    发明申请
    LOW LOSS AIRFOIL PLATFORM TRAILING EDGE 审中-公开
    低损失航空平台行驶边

    公开(公告)号:WO2013130181A3

    公开(公告)日:2015-06-11

    申请号:PCT/US2013020962

    申请日:2013-01-10

    CPC classification number: F01D5/143 F05D2240/80 F05D2260/60 Y02T50/673

    Abstract: An airfoil platform comprises a leading edge portion and a trailing edge portion. The trailing edge portion comprises a first region having a convex flowpath contour, a second region having an intermediate flowpath contour extending downstream from the convex flowpath contour, and a third region having a concave or linear flowpath contour extending downstream from the intermediate flowpath contour to a downstream end of the trailing edge portion of the platform.

    Abstract translation: 翼型平台包括前缘部分和后缘部分。 后缘部分包括具有凸形流路轮廓的第一区域,具有从凸形流路轮廓的下游延伸的中间流路轮廓的第二区域以及具有从中间流路轮廓向下延伸的凹或线性流路轮廓的第三区域 平台的后缘部分的下游端。

    ENDWALL CONTOURING
    5.
    发明申请
    ENDWALL CONTOURING 审中-公开
    端到端

    公开(公告)号:WO2014074190A3

    公开(公告)日:2014-07-17

    申请号:PCT/US2013054944

    申请日:2013-08-14

    Abstract: An airfoil array is disclosed. The airfoil array may include an endwall, and a plurality of airfoils radially projecting from the endwall. Each airfoil may have a first side and an opposite second side extending axially in chord between a leading edge and a trailing edge. The airfoils may be circumferentially spaced apart on the endwall thereby defining a plurality of flow passages between adjacent airfoils. The airfoil array may further include a convex profiled region extending from the endwall adjacent to the first side of at least one of said plurality of airfoils near the leading edge of the at least one of said plurality of airfoils, and a concave profiled region in the endwall and extending across said at least one of said plurality of flow passages.

    Abstract translation: 公开了一种翼型阵列。 翼型阵列可以包括端壁和从端壁径向突出的多个翼型件。 每个翼型件可以具有在前缘和后缘之间以弦状轴向延伸的第一侧和相对的第二侧。 翼型件可以在端壁上周向间隔开,从而在相邻翼型之间限定多个流动通道。 翼型阵列还可以包括凸出的轮廓区域,该凸形轮廓区域从靠近所述多个翼型件中的至少一个的前缘的所述多个翼型件中的至少一个的第一侧面的端壁延伸,并且在所述多个翼型件中的凹形轮廓区域 并且延伸穿过所述多个流动通道中的所述至少一个。

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