FIELD: metallurgy.
SUBSTANCE: invention relates to metallurgy, namely to the methods of nitride hardening of metals and can be used for manufacturing the parts from titanium alloys working at cyclic loads. High-temperature nitride hardening is performed at 700-750°C for 30-10 min. This is followed by recovery annealing in argon at the temperature exceeding the nitride hardening temperature by 100-150°C, for as long as the time τannealing, selected from the condition: , where Knitride hardening, Kp is empirical coefficients accordingly allowing the rate of formation and the rate of dissolving of the nitride gas-saturated layer, mcm2/sec; Enitride hardening is the process activation energy controlling increase in the nitrogen concentration in the brittle nitride hardened layer J/mole; Ep - is the process activation energy controlling decrease in the nitrogen concentration in the brittle nitride hardened layer J/mole; R is gas constant, J/Kmole; Tnitride hardening is nitride hardening temperature, K; T annealing is recovery annealing temperature, K; τnitride hardening is nitride hardening time, sec.
EFFECT: reduced power inputs and enhanced cyclic endurance and durability of the titanium alloy structures.
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Authors
Dates
2009-08-27—Published
2007-12-06—Filed