首页> 外国专利> A contra-angle insertion for a turbomachine blade in a cooling by air and the blade thus obtained

A contra-angle insertion for a turbomachine blade in a cooling by air and the blade thus obtained

机译:涡轮机叶片在空气冷却中的反角插入,由此获得了叶片

摘要

The impingement baffle insert of a turbomachinery blade is provided with a collar around a portion thereof, the collar having a chamfered surface on the radially inner end and adapted to be frictionally engaged by a damper which also surrounds a portion of the insert and which tends to move radially outward over the beveled surface when acted on by centrifugal forces caused by rotation of the blade. The damper is thus wedged between the insert and the blade inner wall to reduce or prevent relative movement therebetween which is normally caused by thermal and vibrational forces. The integrity of the combination is thus improved to reduce the incidence of insert and turbine blade failure.
机译:涡轮机械叶片的冲击挡板插件在其一部分周围设有轴环,该轴环在径向内端具有倒角表面,并适于通过阻尼器摩擦接合,该阻尼器也围绕插件的一部分,并且趋向于当受到叶片旋转产生的离心力作用时,在倾斜表面上径向向外移动。因此,阻尼器楔入插件和叶片内壁之间,以减小或防止它们之间的相对运动,该相对运动通常是由热力和振动力引起的。因此,改进了组合的完整性,以减少插入件和涡轮叶片故障的发生。

著录项

  • 公开/公告号FR2286276B3

    专利类型

  • 公开/公告日1978-05-05

    原文格式PDF

  • 申请/专利权人 GENERAL ELECTRIC CY;

    申请/专利号FR19750029340

  • 发明设计人

    申请日1975-09-25

  • 分类号F01D5/18;

  • 国家 FR

  • 入库时间 2022-08-22 21:48:50

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