首页> 外国专利> Gas turbine blade has platform at base with end face turned towards gas flow, smaller blade whose surface is parallel to end face being mounted under platform which is at least as wide as projection of blade width on front edge of platform

Gas turbine blade has platform at base with end face turned towards gas flow, smaller blade whose surface is parallel to end face being mounted under platform which is at least as wide as projection of blade width on front edge of platform

机译:燃气轮机叶片的底部具有平台,端面朝向气流,较小的叶片表面平行于端面,安装在平台下方,其宽度至少等于叶片宽度在平台前缘上的投影

摘要

The gas turbine blade has a platform (8) at the base with an end face (9) which is turned towards the gas flow. A smaller blade (14) whose surface is parallel to the end face is mounted under the platform and is at least as wide as the projection (b) of the blade width on the front edge of the platform.
机译:燃气涡轮机叶片在底部具有平台(8),平台(8)具有朝向气流的端面(9)。表面平行于端面的较小刀片(14)安装在平台下方,其宽度至少等于平台前边缘上刀片宽度的突出部分(b)的宽度。

著录项

  • 公开/公告号DE10064272A1

    专利类型

  • 公开/公告日2002-07-04

    原文格式PDF

  • 申请/专利权人 ALSTOM (SWITZERLAND) LTD. BADEN;

    申请/专利号DE2000164272

  • 发明设计人 BEECK ALEXANDER;EBELING WILHELM;

    申请日2000-12-22

  • 分类号F01D11/00;

  • 国家 DE

  • 入库时间 2022-08-22 00:27:17

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