NON-LINEARLY DEFLECTING BRUSH SEAL LAND
    1.
    发明公开
    NON-LINEARLY DEFLECTING BRUSH SEAL LAND 审中-公开
    NICHTLINEARER ABLENKENDEBÜRSTENDICHTUNGSFLÄCHE

    公开(公告)号:EP3055512A4

    公开(公告)日:2017-06-21

    申请号:EP14852811

    申请日:2014-09-23

    摘要: A brush seal land is disclosed. The brush seal land may comprise a first portion configured to be coupled to a turbine disc of an aircraft engine and a second portion having a contact surface. The brush seal land may comprise a concave annular structure. The second portion may deflect through a clearance area in response to contact with a brush. The second portion may not deflect in response to contact with a brush after the second portion has deflected through a clearance area in response to contact with the brush. The contact surface comprises tungsten carbide. The brush seal land may comprise INCONEL. The brush seal land may be configured to be coupled to an annular member extending from the turbine disc. The brush seal land may reduce abrasion to an annular member extending from the turbine disc by a brush.

    摘要翻译: 公开了一种刷式密封面。 刷式密封面可以包括构造成联接到飞机发动机的涡轮盘的第一部分和具有接触表面的第二部分。 刷式密封面可以包括凹形环形结构。 响应于与刷子的接触,第二部分可以偏转穿过间隙区域。 在第二部分响应于与刷子的接触而偏转通过间隙区域之后,第二部分可以不响应于与刷子的接触而偏转。 接触表面包含碳化钨。 刷式密封面可以包括INCONEL。 刷式密封件台面可构造成联接到从涡轮盘延伸的环形构件。 刷式密封面可以减少对通过刷子从涡轮盘延伸的环形构件的磨损。

    DETUNING TRAILING EDGE COMPOUND LEAN CONTOUR
    2.
    发明公开
    DETUNING TRAILING EDGE COMPOUND LEAN CONTOUR 审中-公开
    VERSTELLENDE ZUSAMMENGESETZTE SCHMALE KONTUR EINER AUSTRITTSKANTE

    公开(公告)号:EP3055507A4

    公开(公告)日:2017-06-21

    申请号:EP14851901

    申请日:2014-10-02

    IPC分类号: F01D5/14 F01D5/16

    摘要: A rotor blade comprises a blade platform and an airfoil. The airfoil comprises a blade tip, a leading edge, and a trailing edge with a stiffening compound lean contour. The blade tip is radially opposite the blade platform, and defines a blade span between the blade itself and the blade platform. The leading and trailing edges extend from the blade platform to the blade tip to define blade chords between the leading edge and the trailing edge. The compound lean contour comprises a positive lean section located at the lean tip, and extending along a lean axis to a lean end. The negative lean section is located radially inward of the positive lean section, and extends along the lean axis to the lean end.

    摘要翻译: 转子叶片包括叶片平台和翼型件。 翼型包括叶片尖端,前缘和具有加强复合物倾斜轮廓的后缘。 叶片尖端与叶片平台径向相对,并且限定叶片自身和叶片平台之间的叶片跨度。 前缘和后缘从叶片平台延伸到叶片尖端,以在前缘和后缘之间限定叶片弦。 该复合贫油轮廓包括位于贫尖端的正贫油部分,并沿着贫油轴延伸至贫油端。 负倾斜部分位于正倾斜部分的径向内侧,并且沿着倾斜轴线延伸至倾斜端部。

    NON-LINEAR BUMPER BEARINGS
    4.
    发明公开
    NON-LINEAR BUMPER BEARINGS 审中-公开
    NICHTLINEARESTOSSFÄNGERLAGER

    公开(公告)号:EP3068980A4

    公开(公告)日:2017-08-16

    申请号:EP14875971

    申请日:2014-10-10

    IPC分类号: F01D25/16 F16C17/03 F16C27/02

    摘要: A bumper bearing assembly includes a bearing housing having a level of radial spring stiffness, wherein the bearing housing defines a bearing seat. A bumper bearing is connected to the bearing housing by a spring having a level of radial spring stiffness lower than that of the bearing housing. The bumper bearing is configured to apply the level of radial spring stiffness of the spring against a rotor with the bumper bearing spaced apart from the bearing seat. The bearing housing is configured to apply the level of radial spring stiffness of the bearing housing against the rotor with the bumper bearing seated against the bearing seat.

    摘要翻译: 保险杠轴承组件包括具有径向弹簧刚度水平的轴承壳体,其中轴承壳体限定轴承座。 保险杠轴承通过具有比轴承壳体的径向弹簧刚度水平低的弹簧连接到轴承壳体。 缓冲器轴承构造成将缓冲器轴承与轴承座隔开的情况下将弹簧的径向弹簧刚度水平应用于转子。 轴承壳体构造成在保险杠轴承座靠在轴承座上时将轴承壳体的径向弹簧刚度水平应用于转子。