发明名称 PRODUCTION OF HIGHHTEMPERATURE GAS TURBINE BLADE
摘要 PURPOSE:To produce the captioned blade which will not cause cracking and peeling and has superior thermal barrier effect by depositing the Ni-plated layer co-deposited with ceramic powder on the surface of turbine blade blank and spraying ceramics thereon. CONSTITUTION:The surface of the gas tubine blade bland 1 composed of superalloy of Ni- or Co-base or the like is degreased, pickled and rinsed, after which it is put in the Ni plating bath containing ceramic powder of Al2O3, ZrO2, TiO2, etc. to apply Ni plating, whereby the Ni-plated layer 2 co-deposited with ceramic powder 3 is formed on the blank 1 surface. After the plating, the surface is rounghened by blasting, thence a ceramic layer 4 is formed on the Ni-plated layer 2 surface by a spraying method.
申请公布号 JPS55115972(A) 申请公布日期 1980.09.06
申请号 JP19790021415 申请日期 1979.02.27
申请人 TOKYO SHIBAURA ELECTRIC CO 发明人 YOSHIMOTO KAZUNORI;HAGIWARA MITSUHARU;SUZUKI KAZUO
分类号 F01D5/18;C23C2/04;C23C4/02;C23C4/10;C23C28/00;C25D15/02 主分类号 F01D5/18
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