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THERMAL BARRIER PLACED DIRECTLY ON SINGLE-CRYSTAL SUPERALLOYS

2025-06-18 06:591530下载
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The process for depositing a thermal barrier on a monocrystalline superalloy (10) that is useful in a part of turbine blade of a turbomachine, comprises directly depositing zirconium on the superalloy. Independent claims are included for : (1) a part having the monocrystalline superalloy; and (2) a turbine blade.


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