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    • 7. 发明专利
    • DE602005002866D1
    • 2007-11-29
    • DE602005002866
    • 2005-04-27
    • DAIDO STEEL CO LTDMITSUBISHI HEAVY IND LTD
    • UETA SHIGEKINODA TOSHIHARUYAMAMOTO RYUICHIKADOYA YOSHIKUNIMAGOSHI RYOTARONISHIMOTO SHIN
    • C22F1/10C22C19/03C22C19/05C22F1/00
    • The present invention provides a method for producing a low thermal expansion Ni-base superalloy, which includes: preparing an alloy including, by weight%, C: 0.15% or less, Si: 1% or less, Mn: 1% or less, Cr: 5 to 20%, at least one of Mo, W and Re, which satisfy the relationship Mo + 1/2(W + Re): 17 to 27%, Al: 0.1 to 2%, Ti: 0.1 to 2%, Nb and Ta, which satisfy the relationship Nb + Ta/2: 1.5% or less, Fe: 10% or less, Co: 5% or less, B: 0.001 to 0.02%, Zr: 0.001 to 0.2%, a reminder of Ni and inevitable components; subjecting the alloy to a solution heat treatment under the condition of at a temperature of 1000 to 1200°C; subjecting the alloy to either a carbide stabilizing treatment for making aggregated carbides on grain boundaries and stabilizing the carbides under the conditions of at a temperature of not less than 850°C and less than 1000°C and for 1 to 50 hours, or a carbide stabilizing treatment for making aggregated carbides on grain boundaries and stabilizing the carbides by cooling from the temperature in the solution heat treatment to 850°C at a cooling rate of 100°C or less per hour; subjecting the alloy to a first aging treatment for precipitating y' phase under the conditions of at a temperature of 720 to 900°C and for 1 to 50 hours; and subjecting the alloy to a second aging treatment for precipitating A 2 B phase under the conditions of at a temperature of 550 to 700°C and for 5 to 100 hours.
    • 9. 发明专利
    • AT376077T
    • 2007-11-15
    • AT05009211
    • 2005-04-27
    • DAIDO STEEL CO LTDMITSUBISHI HEAVY IND LTD
    • UETA SHIGEKINODA TOSHIHARUYAMAMOTO RYUICHIKADOYA YOSHIKUNIMAGOSHI RYOTARONISHIMOTO SHIN
    • C22F1/10C22C19/03C22C19/05C22F1/00
    • The present invention provides a method for producing a low thermal expansion Ni-base superalloy, which includes: preparing an alloy including, by weight%, C: 0.15% or less, Si: 1% or less, Mn: 1% or less, Cr: 5 to 20%, at least one of Mo, W and Re, which satisfy the relationship Mo + 1/2(W + Re): 17 to 27%, Al: 0.1 to 2%, Ti: 0.1 to 2%, Nb and Ta, which satisfy the relationship Nb + Ta/2: 1.5% or less, Fe: 10% or less, Co: 5% or less, B: 0.001 to 0.02%, Zr: 0.001 to 0.2%, a reminder of Ni and inevitable components; subjecting the alloy to a solution heat treatment under the condition of at a temperature of 1000 to 1200°C; subjecting the alloy to either a carbide stabilizing treatment for making aggregated carbides on grain boundaries and stabilizing the carbides under the conditions of at a temperature of not less than 850°C and less than 1000°C and for 1 to 50 hours, or a carbide stabilizing treatment for making aggregated carbides on grain boundaries and stabilizing the carbides by cooling from the temperature in the solution heat treatment to 850°C at a cooling rate of 100°C or less per hour; subjecting the alloy to a first aging treatment for precipitating y' phase under the conditions of at a temperature of 720 to 900°C and for 1 to 50 hours; and subjecting the alloy to a second aging treatment for precipitating A 2 B phase under the conditions of at a temperature of 550 to 700°C and for 5 to 100 hours.