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Turbine bucket with platform leading edge scallop for performance and secondary flow, corresponding turbine wheel and method of controlling secondary purge air flow

机译:具有用于性能和二次流的平台前缘扇贝的涡轮机叶轮,相应的涡轮机叶轮和控制二次吹扫空气流的方法

摘要

A turbine bucket (64) includes a platform (80) and an airfoil (68). A leading edge of the platform (100) is circumferentially defined by a continuous curve forming at least one axially extending projection (102) and an adjacent recess (104), the axially-extending projection (102) located adjacent a leading edge (72) of the airfoil (68). A corresponding method of controlling secondary purge air flow is also provided.
机译:涡轮叶片(64)包括平台(80)和翼型件(68)。平台(100)的前缘由形成至少一个轴向延伸的突出部(102)和相邻的凹部(104)的连续曲线周向限定,轴向延伸的突出部(102)位于前缘(72)附近。翼型(68)。还提供了控制次级吹扫空气流量的相应方法。

著录项

  • 公开/公告号EP2586974B1

    专利类型

  • 公开/公告日2017-12-13

    原文格式PDF

  • 申请/专利权人 GENERAL ELECTRIC COMPANY;

    申请/专利号EP20120189574

  • 发明设计人 INGRAM CLINT LUIGIE;

    申请日2012-10-23

  • 分类号F01D5/14;

  • 国家 EP

  • 入库时间 2022-08-21 13:19:42

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