Turbine blade inner end attachment structure
    1.
    发明授权
    Turbine blade inner end attachment structure 失效
    涡轮叶片内端附件结构

    公开(公告)号:US5131814A

    公开(公告)日:1992-07-21

    申请号:US505121

    申请日:1990-04-03

    CPC分类号: F01D5/3007 Y02T50/671

    摘要: A gas turbine engine having an outer annular turbine rotor, which is counterrotatable relative to an inner annular turbine rotor, includes attachment structure for attaching turbine blades in circumferential rows to the inner rotor. The attachment structure includes first and second male members of hook-like configurations spaced axially along and circumferentially extending about the rotor, and first and second grooves defined by flanges attached to the rotor and axially spaced along and circumferentially extending about the rotor. The grooves open in a common axial direction for receiving in mated relation respectively and concurrently the hook-like configured first and second male members. The attachment structure also includes several different locking arrangements for locking the male members in mated relation with the grooves to thereby restrain the turbine blade against radial and axial movements relative to the rotor. Some locking arrangements are adapted for locking all of the blades but a last or final one thereof in a circumferential row around the rotor. Other locking arrangements are adapted for locking all of the blades in the circumferential row. Still other locking arrangements are adapted for locking only the last or final blade to complete the circumferential row of blades.

    摘要翻译: 具有外环形涡轮机转子的燃气涡轮发动机,其相对于内环形涡轮机转子可逆地旋转,包括用于将周向行中的涡轮叶片附接到内转子的附接结构。 附接结构包括钩状构造的第一和第二阳构件,所述第一和第二阳构件沿轴向并沿着转子周向延伸,以及由附接到转子并由轴向间隔开并围绕转子周向延伸的凸缘限定的第一和第二槽。 所述凹槽在共同的轴向方向上打开以分别接合并且同时形成钩状配置的第一和第二阳构件。 附接结构还包括几个不同的锁定装置,用于将阳构件与凹槽配合关系锁定,从而约束涡轮叶片抵抗相对于转子的径向和轴向运动。 一些锁定装置适用于锁定所有叶片,但是围绕转子的圆周排锁定其最后的或最后的叶片。 其他锁定装置适于锁定圆周排中的所有叶片。 还有其它锁定装置适于仅锁定最后的刀片或最终刀片以完成圆周排的刀片。

    Turbine blade outer end attachment structure
    2.
    发明授权
    Turbine blade outer end attachment structure 失效
    涡轮叶片外端附件结构

    公开(公告)号:US5131813A

    公开(公告)日:1992-07-21

    申请号:US505118

    申请日:1990-04-03

    摘要: A gas turbine engine having an outer annular turbine rotor, which is counterrotatable relative to an inner annular turbine rotor, includes attachment structure for attaching turbine blades in circumferential rows to the outer rotor. The attachment structure includes first and second male members spaced axially along and circumferentially extending about the rotor, and first and second grooves spaced axially along and extending circumferentially about the rotor being defined by flanges attached to the rotor. Each male member has a first portion attached to an end of a turbine blade and extending therefrom in a radial direction. The first male member has a second portion attached to its first portion and extending therefrom in an axial direction to define the first male member with an overall hook-like cross-sectional configuration. The first groove is cross-sectionally shaped for receiving in mated relation the second portion of the first male member. The second groove is cross-sectionally shaped for receiving in mated relation in the second groove a lock segment of the locking assembly and the first portion of the second male member to lock the male members in the respective grooves and thereby lock the turbine blade against radial and axial movements relative to the rotor.

    摘要翻译: 具有外环形涡轮机转子的燃气涡轮发动机,其相对于内部环形涡轮机转子可反转,包括用于将涡轮机叶片以周向排附接到外转子的附接结构。 附接结构包括沿着转子轴向间隔开并在周向上延伸的第一和第二阳构件,并且围绕转子沿轴向间隔开并且围绕转子周向延伸的第一和第二槽由连接到转子的凸缘限定。 每个阳构件具有附接到涡轮叶片的端部并且沿径向方向从其延伸的第一部分。 第一阳构件具有附接到其第一部分的第二部分并且在轴向方向上从第二部分延伸以限定具有整体钩状横截面构造的第一阳构件。 第一槽是横截面形状的,用于以配合的关系接收第一阳构件的第二部分。 第二凹槽是横截面形状的,用于在第二凹槽中以配合关系接收锁定组件的锁定段和第二阳构件的第一部分,以将阳构件锁定在相应的凹槽中,从而将涡轮叶片锁定在径向 和相对于转子的轴向移动。