发明申请
- 专利标题: HIGH-TEMPERATURE RESISTANT COMPONENT AND GAS TURBINE HOT PART
- 专利标题(中): 耐高温组件和气体涡轮机热部件
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申请号: US12822208申请日: 2010-06-24
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公开(公告)号: US20100330391A1公开(公告)日: 2010-12-30
- 发明人: Hideyuki Arikawa , Akira Mebata , Yoshitaka Kojima , Kunihiro Ichikawa , Hiroshi Haruyama
- 申请人: Hideyuki Arikawa , Akira Mebata , Yoshitaka Kojima , Kunihiro Ichikawa , Hiroshi Haruyama
- 专利权人: Hitachi, Ltd.
- 当前专利权人: Hitachi, Ltd.
- 优先权: JP2009-154526 20090630
- 主分类号: B32B5/18
- IPC分类号: B32B5/18
摘要:
A high-temperature resistant component for a gas turbine hot part and so on is provided, which has durability and reliability enough to withstand a corrosive environment with use of the low-grade oil. The high-temperature resistant component includes an alloy substrate containing Ni, Co, or Fe as the principal component, and a thermal barrier coating formed over the surface of the substrate via a bond coat. The thermal barrier coating includes a porous thermal-barrier layer made of ceramic and an environmental barrier layer with corrosion resistance. An impregnated layer is provided between the environmental barrier layer and the thermal barrier layer. In the impregnated layer, the thermal barrier layer is impregnated with a part of the environmental barrier layer. The thermal barrier layer is made of a porous zirconia layer, and the environmental barrier layer includes silica as the principal component. The porous zirconia layer has pores impregnated with the part of the environmental barrier layer. As a result, the high-temperature resistant component has excellent corrosion resistance and excellent heat resistance.
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