发明名称 ROTOR BLADE OF GAS-TURBINE UNIT COMPRESSOR
摘要 A blade of compressor of gas-turbine unit is made of alloy based on titanium with protective coating and comprises a blade root and a fin rigidly connected to each other. Two layers of vacuum-plasma coating are applied to the blade root as well.
申请公布号 UA88405(U) 申请公布日期 2014.03.11
申请号 UA20130012905U 申请日期 2013.11.06
申请人 VOLODYMYR DAL EASTERN UKRAINIAN NATIONAL UNIVERSITY 发明人 ASHYKHMINA OLENA ANATOLIIVNA;KORSUNOV KOSTIANTYN ANATOLIIOVYCH
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