- 专利标题: BLADE, GAS TURBINE INCLUDING THE SAME, AND BLADE MANUFACTURING METHOD
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申请号: US15743909申请日: 2016-09-08
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公开(公告)号: US20180200783A1公开(公告)日: 2018-07-19
- 发明人: Keita TAKAMURA , Satoshi HADA , Hidekatsu ATSUMI , Tomofumi SHINTANI
- 申请人: Mitsubishi Hitachi Power Systems, Ltd.
- 优先权: JP2015-181691 20150915
- 国际申请: PCT/JP2016/076496 WO 20160908
- 主分类号: B22C9/04
- IPC分类号: B22C9/04 ; F02C7/18 ; F01D5/18 ; B22C9/10 ; B22D29/04 ; B22D25/02 ; B23H9/10 ; B23H9/14
摘要:
A blade (50) has a blade, passage (71) extending in a blade height direction (Dwh), a platform passage (81) formed inside a platform (60), and a communication passage (75) leading from an outer surface (93) of a shaft-mounted part (90) through the platform passage (81) to the blade passage (71). An inner surface defining an inflow passage portion (82) of the platform passage (81) includes a shaft-side inner surface (88) that faces a gas path side. The shaft-side inner surface (88) spreads in a direction having more of a component of a blade thickness direction (Dwt) than a component of the blade height direction (Dwh). An inner surface defining the communication passage (75) joins to the shaft-side inner surface (88).
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