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Rotationally symmetrical part for a turbine engine rotor, and related turbine engine rotor, turbine engine module, and turbine engine

机译:用于涡轮发动机转子的旋转对称部件,以及相关的涡轮发动机转子,涡轮发动机模块和涡轮发动机

摘要

A rotationally symmetrical part, such as a disk, for a turbine engine rotor. The part has a rotational axis (A) and includes, an annular row of teeth defining grooves therebetween for therein holding fir tree-shaped rotor blade roots. Each tooth includes a first side flank, having at least two projecting portions for holding a blade root and separated from each other by a hollow portion, and a second side flank including at least two projecting portions for holding an adjacent blade root and separated from each other by a hollow portion. Each tooth has, on substantially the entire longitudinal dimension thereof, a lack of symmetry in relation to a substantially radial median longitudinal plane. At least one of the circumferences of the projecting portions of the second flank is located between the circumferences of the projecting portions of the first flank and is radially shifted from the circumferences.
机译:用于涡轮发动机转子的旋转对称部件,例如盘。该部件具有旋转轴(A),并且包括环形齿排,环形齿排之间限定了用于在其中保持杉树形转子叶片根部的凹槽。每个齿包括第一侧面,其具有至少两个用于保持叶片根部并由中空部分彼此隔开的突出部,以及第二侧面包括至少两个用于保持相邻叶片根部并彼此分开的突出部。其他由空心部分组成。每个齿在其基本上整个纵向尺寸上相对于基本上径向的中间纵向平面缺乏对称性。第二侧面的突出部分的圆周中的至少一个位于第一侧面的突出部分的圆周之间,并且从该圆周径向偏移。

著录项

  • 公开/公告号US10436043B2

    专利类型

  • 公开/公告日2019-10-08

    原文格式PDF

  • 申请/专利权人 SAFRAN AIRCRAFT ENGINES;

    申请/专利号US201515128095

  • 发明设计人 NICOLAS TRAPPIER;

    申请日2015-03-11

  • 分类号F01D5/30;

  • 国家 US

  • 入库时间 2022-08-21 12:15:08

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