High temperature corrosion resistant alloy, thermal barrier coating material, and gas turbine using high temperature corrosion resistant alloy

   
   

A high temperature corrosion resistant alloy composition comprising, in addition to Ni, 0.1 to 12% by weight of Co, 10 to 30% by weight of Cr, 4 to 15% by weight of Al, 0.1 to 5% by weight of Y, and 0.5 to 10% by weight of Re. The high temperature corrosion resistant alloy composition has an excellent oxidation resistance and ductility and is suitable for use in a bonding layer of a thermal barrier coating material.

Состав сплава высокой корозии температуры упорный состоя из, в дополнение к ni, 0.1 к 12% by weight of co, от 10 до 30% by weight of cr, от 4 до 15% by weight of al, от 0.1 до 5% by weight of ы, и от 0.5 до 10% by weight of re. Состав сплава высокой корозии температуры упорный имеет превосходные сопротивление и дуктильность оксидации и целесообразн для пользы в слое bonding материала теплоизолирующей прокладки покрывая.

 
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