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Vane, gas turbine, ring segment, remodeling method for vane, and remodeling method for ring segment

机译:叶片,燃气轮机,环段,叶片的改型方法和环段的改型方法

摘要

A vane (18) has an airfoil section (19) that extends in a radial direction and an outer shroud (20) that is disposed on the radially outward side of the airfoil section (19), and is supported inside a casing by means of a vane support member (24). The outer shroud (20) has a shroud body (31), radial protrusions (36, 37), and a hook section (32) including the radial protrusions (36, 37) and engaging parts (39, 40). A recessed part (50), which is recessed in an axial direction or in the radial direction, is provided in at least a part of the circumference of the hook section (32). The engaging part (39) has a sealing surface that continues along the entire circumference thereof, the sealing surface coming into contact with the vane support member (24) in the radial direction.
机译:叶片( 18 )具有沿径向方向延伸的翼型截面( 19 )和布置在其上的外罩( 20 )翼型部分( 19 )的径向外侧,并通过叶片支撑部件( 24 )支撑在壳体内。外罩( 20 )具有罩体( 31 ),径向突起( 36、37 )和钩形部分( 32 ),包括径向突起( 36、37 )和接合部分( 39、40 )。在钩部( 32 )的圆周的至少一部分上设有在轴向或径向上凹陷的凹陷部( 50 )。 )。接合部( 39 )具有沿着其整个圆周连续的密封表面,该密封表面在径向上与叶片支撑构件( 24 )接触。 。

著录项

  • 公开/公告号US10724404B2

    专利类型

  • 公开/公告日2020-07-28

    原文格式PDF

  • 申请/专利权人 MITSUBISHI HITACHI POWER SYSTEMS LTD.;

    申请/专利号US201515324777

  • 发明设计人 KEITA TAKAMURA;

    申请日2015-06-29

  • 分类号F01D9/04;F01D25/24;F01D11;

  • 国家 US

  • 入库时间 2022-08-21 11:28:57

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