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Gas Turbine Blade and Manufacturing Method Thereof 发明申请

2023-02-25 2590 622K 0

专利信息

申请日期 2025-06-26 申请号 US12107796
公开(公告)号 US20100266418A1 公开(公告)日 2010-10-21
公开国别 US 申请人省市代码 全国
申请人 IMANO SHINYA; ICHIKAWA KUNIHIRO; DOI HIROYUKI; TANAKA KATSUMI
简介 In a gas turbine blade where a part of the γ′ phase precipitation strengthened type Ni-based alloy base material is composed of a weld metal, the weld metal is a Ni-based alloy containing Ta from 4.8 to 5.3 wt. %, Cr from 18 to 23 wt. %, Co from 12 to 17 wt. %, W from 14 to 18 wt. %, C from 0.03 to 0.1 wt. %, Mo from 1 to 2 wt. %, and Al of 1 wt. % or less, in which the oxygen content is 0 to 30 ppm, the Ti content from 0 to 0.1 wt. %, and the Re content from 0 to 0.5 wt. %. A blade base metal is manufactured by the step of stripping, the step of solution heat treatment where the γ′ phase is dissolved again, the step of welding in an inert gas chamber by a TIG method using a welding wire where the weld metal can be obtained, the step of HIP treatment at 1100° C. to 1150° C., and the step of an aging treatment at 835° C. to 855° C.


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