首页> 外国专利> Platform for use between fan blades mounted on rotor disk of blower of e.g. turbojet, has assembly supports, where one support is arranged with position in portion of downstream end, and third assembly support located between supports

Platform for use between fan blades mounted on rotor disk of blower of e.g. turbojet, has assembly supports, where one support is arranged with position in portion of downstream end, and third assembly support located between supports

机译:用于安装在鼓风机转子盘上的风扇叶片之间的平台,例如涡轮喷气发动机,具有组件支架,其中一个支架在下游端的一部分位置定位,而第三组件支架位于支架之间

摘要

The platform (110) has a body part that is intended to be arranged face to face with regard to a rotor disk of a blower. An axially central portion of a seam part (111) is made a seam wall (111a). The body part includes a set of assembly supports (112a, 112b) that extends from the seam part in an internal radial direction. One of the assembly supports is arranged with a position in a portion of downstream end of the seam part. A third assembly support (112c) is located between the set of assembly supports. An independent claim is also included for a turboshaft engine blower.
机译:平台(110)具有旨在相对于鼓风机的转子盘面对面布置的主体部分。接缝部分(111)的轴向中心部分制成接缝壁(111a)。主体部分包括在内部径向方向上从接缝部分延伸的一组组件支撑件(112a,112b)。组件支撑件中的一个布置成在接缝部分的下游端的一部分中具有位置。第三组件支撑件(112c)位于该组组件支撑件之间。涡轮轴发动机鼓风机也包含独立索赔。

著录项

  • 公开/公告号FR2988427A1

    专利类型

  • 公开/公告日2013-09-27

    原文格式PDF

  • 申请/专利权人 SNECMA;

    申请/专利号FR20120052475

  • 申请日2012-03-20

  • 分类号F01D5/22;F04D29/34;

  • 国家 FR

  • 入库时间 2022-08-21 16:20:54

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