HEAT TREATMENT METHOD OF DISC-TYPE PARTS OF GAS-TURBINE ENGINES FROM HEAT-RESISTANT POWDER NICKEL ALLOYS Russian patent published in 2011 - IPC C22F1/10 

Abstract RU 2433202 C1

FIELD: metallurgy.

SUBSTANCE: heat treatment method of parts like discs of gas-turbine engines from heat-resistant powder nickel alloys is proposed. Method involves heating to hardening temperature, and ageing. Cooling from hardening temperature is performed in salt bath with temperature that is by 350-500°C lower than complete dissolution temperature of γ' - phase during 8-16 hours.

EFFECT: increasing heat resistance, reducing the duration of heat treatment, improving the process efficiency at low level of residual stresses.

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RU 2 433 202 C1

Authors

Eremenko Vasilij Ivanovich

Fatkullin Oleg Khikmetovich

Furashov Aleksej Sergeevich

Fatkullin Stanislav Igorevich

Shchukarev Anatolij Konstantinovich

Dates

2011-11-10Published

2010-04-16Filed