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turbinenwelle and method for cooling a turbinenwelle

机译:涡轮机井和冷却涡轮机井的方法

摘要

A turbine shaft extends along a principal axis and has an outer surface. The turbine shaft is formed by a plurality of cylindrical shaft segments which are disposed axially one behind the other and are braced together by a bracing element. An axial gap which is formed between the bracing element and at least one shaft segment is connected in terms of flow to two axially spaced radial passages. The radial passages each open at the outer surface of the turbine shaft. A method for cooling a turbine shaft is also provided.
机译:涡轮轴沿着主轴延伸并且具有外表面。涡轮轴由多个圆柱形的轴段形成,所述多个轴段在轴向上彼此相邻地布置并且通过支撑元件支撑在一起。在支撑元件和至少一个轴段之间形成的轴向间隙在流动方面与两个轴向间隔的径向通道相连。径向通道分别在涡轮轴的外表面处开口。还提供了一种用于冷却涡轮机轴的方法。

著录项

  • 公开/公告号DE59709016D1

    专利类型

  • 公开/公告日2003-01-30

    原文格式PDF

  • 申请/专利权人 SIEMENS AG;

    申请/专利号DE19975009016T

  • 发明设计人 FELDMUELLER ANDREAS;POLLAK HELMUT;

    申请日1997-05-12

  • 分类号F01D5/06;F01D5/08;F01D3/02;

  • 国家 DE

  • 入库时间 2022-08-21 23:40:24

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