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TURBO ENGINE, AND VANE CARRIER UNIT FOR TURBO ENGINE

机译:涡轮发动机和涡轮发动机叶片支架单元

摘要

PROBLEM TO BE SOLVED: To provide a vane carrier unit capable of reducing relative different motions of an inner end part and an outer end part of a guide vane member.SOLUTION: A turbo engine has an outer wall structure 11 and an inner wall structure 12; the inner wall structure 12 is arranged at an inner side position in a radial direction in respect to the outer wall structure 11; each of the wall structures 11, 12 has surfaces arranged to face to each other in a radial direction. A duct 14 is arranged between the inner wall structure 12 and the outer wall structure 11; the duct 14 has a downstream side end part in regard to a main flow direction of the working fluid of the turbo engine and a guide vane member 20 is arranged at an end part of the downstream side of the duct 14. The inner end part of the guide vane member 20 is supported by the inner wall structure 12; the outer end part of the guide vane member 20 is supported by the outer wall structure 11. The inner wall structure 12 and the outer wall structure 11 are connected to each other and arranged as a vane carrier unit 1.SELECTED DRAWING: Figure 2
机译:解决的问题:提供一种能够减少导向叶片构件的内端部和外端部的相对不同运动的叶片承载单元。解决方案:涡轮发动机具有外壁结构11和内壁结构12 ;内壁结构12相对于外壁结构11配置在径向内侧。每个壁结构11、12具有被布置为在径向方向上彼此面对的表面。在内壁结构12和外壁结构11之间布置有管道14;并且导管14在涡轮发动机的工作流体的主流方向上具有下游侧的端部,在导管14的下游侧的端部配置有导向叶片部件20。导向叶片构件20由内壁结构12支撑。导向叶片构件20的外端部分由外壁结构11支撑。内壁结构12和外壁结构11彼此连接并布置为叶片承载单元1。

著录项

  • 公开/公告号JP2017187042A

    专利类型

  • 公开/公告日2017-10-12

    原文格式PDF

  • 申请/专利权人 ANSALDO ENERGIA SWITZERLAND AG;

    申请/专利号JP20170076740

  • 发明设计人 URS BENZ;

    申请日2017-04-07

  • 分类号F01D9/04;F23R3/42;F01D9/02;F01D9/06;

  • 国家 JP

  • 入库时间 2022-08-21 14:01:48

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