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Bearing support which allows to keep a turbofan engine functioning after the appearance of an imbalance

机译:轴承支撑,可在出现不平衡现象后使涡轮风扇发动机保持运转

摘要

The method involves maintaining at least one bearing (15,18) on a support (17,19) having at least two levels of stiffness (35,36) agreed at the level of the normal stiffness corresponding to the correct rotor mode at a speed above a given level where the engine is throttled back during flight, and a lower level of stiffness corresponding to a mode suitable for a level below this speed. Play is provided (E) at least equal to the radial displacement (D) of the rotor at the first speed, under the effect of a maximum pre-established imbalance with the bearing support at a lower level. The bearing support is moved from a normal level to a lower level after the appearance of an imbalance at least equal to the pre established level.
机译:该方法包括将至少一个轴承(15,18)保持在具有至少两个刚度水平(35,36)的支撑件(17,19)上,所述至少两个刚度水平在对应于正确转子模式的正常刚度水平下以一定速度一致。高于给定水平,在飞行过程中发动机会被节流,而较低的刚度则对应于低于该速度的模式。在最大预先建立的不平衡与轴承座处于较低水平的情况下,在第一速度下提供的游隙(E)至少等于转子的径向位移(D)。在出现至少等于预定水平的不平衡之后,轴承支撑件从正常水平移动到较低水平。

著录项

  • 公开/公告号EP0814236B1

    专利类型

  • 公开/公告日2002-03-13

    原文格式PDF

  • 申请/专利权人 SNECMA MOTEURS;

    申请/专利号EP19970401324

  • 发明设计人 GEREZ VALERIO;

    申请日1997-06-12

  • 分类号F01D25/16;F01D21/04;

  • 国家 EP

  • 入库时间 2022-08-22 00:36:08

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