ROTOR AIRFOILS TO CONTROL TIP LEAKAGE FLOWS
    1.
    发明申请
    ROTOR AIRFOILS TO CONTROL TIP LEAKAGE FLOWS 审中-公开
    转子空气控制提升泄漏流量

    公开(公告)号:WO1996014494A2

    公开(公告)日:1996-05-17

    申请号:PCT/US1995013402

    申请日:1995-10-23

    CPC classification number: F01D5/20 F01D5/141 F01D5/145

    Abstract: A rotor blade (24) for a gas turbine engine includes a bowed surface (43) on a tip region (40) of the suction side (32) thereof. The curvature of the bowed surface (43) progressively increases toward the tip (36) of the blade (24). The bowed surface (43) results in a reduction of tip leakage through a tip clearance (50) from the pressure side (30) to the suction side (32) of the blade (24) and reduces mixing loss due to tip leakage.

    Abstract translation: 用于燃气涡轮发动机的转子叶片(24)包括在其吸力侧(32)的尖端区域(40)上的弯曲表面(43)。 弯曲表面(43)的曲率朝着刀片(24)的尖端(36)逐渐增加。 弯曲表面(43)导致通过尖端间隙(50)从叶片(24)的压力侧(30)到吸力侧(32)的尖端泄漏减少,并且减少由于尖端泄漏引起的混合损失。

    ROTOR AIRFOILS TO CONTROL TIP LEAKAGE FLOWS
    2.
    发明公开
    ROTOR AIRFOILS TO CONTROL TIP LEAKAGE FLOWS 失效
    转子叶片形用于减少间隙损耗

    公开(公告)号:EP0792410A1

    公开(公告)日:1997-09-03

    申请号:EP95938269.0

    申请日:1995-10-23

    IPC: F01D5

    CPC classification number: F01D5/20 F01D5/141 F01D5/145

    Abstract: A rotor blade (24) for a gas turbine engine includes a bowed surface (43) on a tip region (40) of the suction side (32) thereof. The curvature of the bowed surface (43) progressively increases toward the tip (36) of the blade (24). The bowed surface (43) results in a reduction of tip leakage through a tip clearance (50) from the pressure side (30) to the suction side (32) of the blade (24) and reduces mixing loss due to tip leakage.

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