Design of binder jet additive manufactured co-continuous ceramic-reinforced metal matrix composites
Pablo D. Enrique, Ehsan Marzbanrad, Yahya Mahmoodkhani, Ali Keshavarzkermani, Hashem Al Momani, Ehsan Toyserkani, Norman Y. Zhou
Fig. 9. Maximum Cr3C2 shell volume fraction achievable with varying Cr concentrations in the starting powder. Values for some Ni-based alloys and the current study’s MMC are shown, with adjustments (no-fill shapes) for Mo solubility in the Cr3C2 shell.