Page 19 - PR 2014 2016 10 Materials and Nanotechnology
P. 19

Materials and Nanotechnology | Progress Report  295




               Mechanical Properties                          at 300°C for 5 h. Preliminary results show the

                                                              occurrence of DSA in the (b) and (c) conditions.
               Fracture mechanics and mechanical
               properties of metals, alloys and               A fracture mechanics analysis of flaws in grind-
               composites                                     ing balls mills for mining plants was undertak-

                                                              en and the theoretical values of growth rate
               An elastic-plastic fracture mechanics study    of those defects were compared with actual
               of the application of Leak-Before-Break (LBB)   values obtained through periodic inspections
               concept in a relatively small-diameter (273    performed in this component. The cracks nu-
               mm diameter) high-energy nuclear reactor       cleation was caused by lack of lubrication in
               coolant line was done, where it is proposed    the trunnion bearings, generating circumfer-
               AISI 316LN type stainless steel to be used as   ential thermal stresses and the estimated tem-
               base material welded with AISI 316L coat-      perature of the trunnion and bushing contact
               ed electrode. Results show a well-defined      reached 150°C. During the analyzed period,
               mechanical behavior where base material        the results obtained by the BS7910 standard
               has a high toughness, weld region has a low    proved to be closer to the actual values than
               toughness, and HAZ shows intermediate          the ASME Section XI standard.
               properties. For the load limit analysis, the
               lowest critical crack size was found for base   A study of the influence of solution heat treat-
               material presenting circumferential cracks.    ment temperature on the hardness response in
               For J-integral analysis, it was demonstrated   incoloy 945 was done. Incoloy 945 is a hybrid
               that tearing instability leading to failure    Ni-Fe-Cr based superalloy with a mechanical
               would not occur.                               strength and corrosion resistance comparable
                                                              to those of Inconel 718 and Incoloy 925, respec-
               A preliminary draft version of a surveillance   tively, with minimum yield strength reaching
               program for the materials presented in the     860 MPa. The heat treatment at 1000°C causes
               nucleus of Brazilian Multipurpose Reactor      a hardness reduction around 61%, reaching
               (RMB) was developed. The surveillance pro-     63% at the temperature of 1020°C. The reasons
               gram is needed to confirm and determine        for the reductions are the dissolution of the
               the effects of radiation on the mechanical     gamma prime hardening phase and a slight
               properties of the core reactor materials: its   grain growth (ASTM 7). Above this temperature,
               effects on the tensile properties (strength and   the hardness loss is negligible, however, grain
               ductility), fracture toughness, radiation-in-  growth is more pronounced reaching a ASTM
               duced growth and corrosion.                    2 grain size in the specimens treated at 1050°C.


               The mechanical behavior of high strength       Aluminum alloys for automotive
               aluminum alloys of the 7075 series is under    applications
               investigation, to study the occurrence of dy-
               namic strain aging (DSA: Portevin-Le Chat-     Automobile parts made of steel/cast iron have
               ellier effect) on tensile specimens, submitted   been replaced with those made with alumi-
               to different heat-treatment conditions: (a)    num alloys to not only reduce weight, but also
               solution heat treated then artificially aged,   to reduce fuel consumption the emission of
               T6, (b) T6 then solution heat treated at 485°C   pollutants. Structural materials require not
               for 5 hours, (c) T6 then solution heat treated   only high strength/weight ratio, besides rea-
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