HIGHTEMP1.1 Solution Heat-Treatment of the Nb-Modified MAR-M247 Superalloy

Monday, June 18, 2012: 9:00 AM
211AB (Charlotte Convention Center)
P. R. S. Azevedo e Silva , The University of Sao Paulo , Lorena, Sao Paulo, Brazil
Renato Baldan , The University of Sao Paulo , Lorena, Sao Paulo, Brazil
G. C. Coelho , The University of Sao Paulo , Lorena, Sao Paulo, Brazil
A. M. S. Costa , The University of Sao Paulo , Lorena, Sao Paulo, Brazil
Mr. Carlos Angelo Nunes , The University of Sao Paulo , Lorena, Sao Paulo, Brazil
MAR-M247 superalloy has excellent mechanical and oxidation/corrosion properties at elevated temperatures. Niobium is a refractory element normally present in the composition of nickel-based superalloys, found mainly in γ’ phase and MC carbides [1]. In general, solution heat-treatments are applied before an aging heat-treatment. The objectives of these treatments is to dissolve the γ’ phase in γ matrix and minimize segregation from non-equilibrium solidification, in order to produce a γ’ controlled re-precipitation during aging heat-treatment, an uniform and isotropic material with better properties [2,3]. The aim of this work was to find the best condition for solution heat-treatment of a MAR-M247 modified Ni-base superalloy through microstructural characterization of as-cast and heat-treated materials, comparing the results with experiments of differential thermal analysis (DTA) and Thermocalc simulations.

The conventional MAR-M247 superalloy was modified by replacing the amount of tantalum by niobium (in atomic %) and then the nominal composition of Nb-modified MAR-M247 superalloy is: 10.2 wt % Co, 10.2W, 8.5Cr, 5.6Al, 1.6Nb, 1.4Hf, 1.1Ti, 0.7Mo, 0.15C, 0.06Zr, 0.015B, Ni balance. This superalloy was produced in a vacuum induction melting furnace (VIM) via investment casting (lost-wax technique) at Açotécnica (Jandira, São Paulo, Brazil).

The samples selected to solution heat-treatments were encapsulated in quartz tube in argon atmosphere and heat-treated in a ceramic tube furnace with MoSi2 resistive element followed by air cooling. The samples were heat-treated at 1185, 1240, 1260, 1280 and 1300 oC for times of 2, 4 and 8 hours. The as-cast and heat-treated samples were prepared following conventional metallographic techniques, etched with a glyceregia solution and characterized in conventional SEM and FEG-SEM, both with EDS detector. All samples were submitted to microhardness measurements.

According to Thermocalc simulations, the window of solution heat-treatment for MAR-M247(Nb) superalloy is between 1212 oC (γ’ solvus temperature) and 1315 oC (solidus temperature).  Besides, in DTA experiments, the γ’ solvus temperature was 1238 oC and the incipient melting temperature was 1281 oC, limiting temperature of heat-treatment because segregation. The sample heat-treated at 1280 oC showed incipient melting. Therefore, Thermocalc simulations have shown a good agreement with DTA experiments.