In view of their outstanding intrinsic properties, notably the high melting point (approaching 2000°C) and, thus, the very good mechanical properties and creep strength at elevated temperatures, refractory metal (RM) silicide alloys are considered first choice replacements for Ni-base superalloys with the aim of increasing the (thermodynamic) efficiency of gas turbine engines. [1] Hence, the main objective of work on RM silicide alloys is to manufacture a composite material that takes advantage of (i) the beneficial oxidation resistance of the silicides and (ii) the outstanding mechanical properties of molybdenum. Nowotny et al, [2] first pointed out that alloys in the ternary system Mo-Si-B might be able to fulfil the above requirements. Later on, Berczik [3,4] followed up on this work and patented alloy compositions in the Mo-rich corner which were proved to possess balanced properties regarding high temperature creep strength, room temperature toughness and oxidation resistance. However, in his approach two manufacturing steps have appeared to be at least problematic to obtain sound material in sufficient quantities at reasonable costs: (1) Berczik employed a rapid solidification (RS) step via Helium gas atomization to obtain a matrix of Mo solid solution for adequate fracture toughness and ductility at temperatures below 600°C with embedded intermetallic compounds Mo 3 Si and Mo 5 SiB 2 (the T2 phase) for oxidation resistance due to the formation of a dense borosilicate glass layer on the metal surface, and (2) he also reported that for sound wrought processing temperatures above 1700°C were needed which makes industrial up-scaling hardly feasible.In order to overcome the above limitation (2) we suggested a powder-metallurgical manufacturing route with mechanical alloying (MA) as the technique replacing the (costly) RS gas atomization step to economically obtain large quantities of three phase Mo-Si-B material with a nearly continuous Mo solid solution matrix. [5] This material beneficially proved superplastic tensile deformation at temperatures as low as 1300°C, exhibiting an ultrafine microstructure with extraordinary thermal stability.Besides the above mentioned requirements applications as high temperature structural materials, for example as guide vanes in a turbine environment, also require the knowledge about the temperature dependent elastic properties and their dependence on microstructure. It is, therefore, the object of the present paper to combine an experimental and numerical approach for predicting the elastic properties of Mo-Si-B composite materials with varying microstructures.
Experimental and Numerical Approach
Microstructural characterizationThe microstructures of the samples were characterized by scanning electron microscopy (SEM) combined with energy dispersive X-ray microanalysis (JEOL 6400 SEM and FEI XL30 FEG equipped with EDX and EBSD). Three different alloy compositions and manufacturing routes were considered for subsequent modelling: while two cast alloys, Mo12Si8.5B and Mo12Si10...