首页> 外国专利> METHOD OF DETAILS CLEANING FROM HEAT-RESISTANT ALLOYS ON BASIS OF NICKEL OF GAS TURBINE ENGINE FROM PRODUCTS OF HIGH-TEMPERATURE OXIDATION AND SULPHIDE CORROSION

METHOD OF DETAILS CLEANING FROM HEAT-RESISTANT ALLOYS ON BASIS OF NICKEL OF GAS TURBINE ENGINE FROM PRODUCTS OF HIGH-TEMPERATURE OXIDATION AND SULPHIDE CORROSION

机译:基于高温氧化和硫化物腐蚀的燃气轮机镍的耐热合金的清洁方法

摘要

FIELD: metallurgy.;SUBSTANCE: invention relates to treatment of details of gas turbine engines of nickel heat-resistant alloys and can be used in aircraft motor building, energetics and other pertinent art, where there are used gas turbine engines, and during the maintenance. Cleaning method includes treatment of details in melt of fluoride salts at the temperature from 320 up to 370°C and further treatment of details in aqueous alkaline solution under pressure from 20 up to 24 MPa at the temperature from 350 up to 450°C in blanket of inert gas, herewith in the capacity of alkaline solution it is used queous alkalines solution KOH or NaOH, or its mixture.;EFFECT: increasing of efficiency of details cleaning of heat-resistant alloys on the basis of nickel of gas turbine engine from high-temperature oxidation products and sulphide corrosion.;1 ex
机译:技术领域本发明涉及镍耐热合金的燃气涡轮发动机的细节的处理,并且可以用于飞机发动机制造,高能学和其他相关领域中,其中使用了燃气涡轮发动机,并且在维护期间。清洁方法包括在320至370°C的温度下在氟化物熔盐中处理细节,并在温度范围从350至450°C的温度下在20至24 MPa的压力下在碱性水溶液中进一步处理细节。惰性气体,因此以碱性溶液的形式使用碱性水溶液KOH或NaOH或其混合物。效果:提高了基于燃气涡轮发动机镍的耐热合金的细节清洁效率,从高温开始氧化产物和硫化物腐蚀; 1 ex

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