AAWSAP DIRD, Metallic Glasses for Aerospace Applications, December 2009
DOW-UAP-D117 · page 21 of 30
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UNCLASSIFIED//P'OR OP'P'l@IAL WS& &Nia¥ Figure 8. Microstructure of In Situ Metallic Glass Matrix Composite. With ductile crystalline dendrites. (a) Scanning electron micrograph showing the dendrites (light gray) in the glassy matrix (dark gray). (b) Composite after plastic deformation; note the multiplicity of slip steps, indicating extensive interaction of shear bands with the dendrltes.33 The key limitation of these in situ composites is that not every alloy system is capable of forming them. While any alloy will form crystalline phases at elevated temperatures, usually the crystalline phases that form are brittle intermetallics that degrade rather than enhance the mechanical properties. To be effective in controlling shear bands, the precipitated phase needs to be ductile, have a shear modulus lower than that of the glassy matrix, and (preferably) form as dendrites. To date, the only published reports of systems that satisfy these criteria concern alloys based on early transition metals, notably zirconium and titanium. Whether in situ composites can be developed in other alloy systems remains to be seen. MECHANICAL PROPERTIES OF COMPOSITES The ability to produce mixed amorphous-crystalline microstructure provides the ability to control the formation and propagation of shear bands. The resulting materials can have good fracture and fatigue resistance while retaining the high strength and processing flexibility associated with metallic glasses. The origin of these effects is related to the development of a region of plastic deformation at the tip of an advancing crack. For a crack opening under tensile loading, the size of the plastic region is approximately given by: (Equation 1) where Kie is the plane-strain fracture toughness (mentioned above) and crv is the yield strength. The size of the plastic zone varies from ~ 1 µm for "intrinsically brittlle" metallic glasses to ,.., 1 mm for glasses capable of some plastic deformation. 34 If the material has structure on this length scale (or if the sample itself is of this size), then 15 UNCLASSIFIED//FQB OFFICIO! 1!&'Ii QNLY