Nickel-based superalloys [1] are key materials in airplane and turbine disks due to their outstanding properties such as high tensile strength and excellent creep deformation resistance. With the increasing requirements of the modern aerospace industry on the performance of materials, traditional nickel alloys are gradually unable to meet the demands of high properties. Thus, selecting the nanoreinforcement phase to construct metal matrix composites (MMCs) is one of the simple and easy ways to improve the performance of materials. [2] The MMC materials [3] not only possess excellent performance of the metal matrix, but also combine several advantages such as high tensile properties, good thermal expansion, low thermal expansion coefficient, and good wear resistance originating from the reinforcement phase. Graphene [4,5] and its related derivative materials (such as graphene oxide (GO), [6] multilayer graphene, [7] graphene nanosheets (GNS), [8] graphene nanoflakes (GNFs) [9]) are a series of 2D materials with unique layered hexagonal honeycomb structure. It is considered to be an ideal reinforcement phase for MMCs due to its unique structure and extraordinary electronic, mechanical, and thermal properties. In the reported literature, graphene-reinforced MMCs (Al, [10] Cu, [11] Ti, [9,12] Ni, [13,14] etc.) have been successfully prepared by hot isostatic pressing (HIP), [15] spark plasma sintering (SPS), [16] laser additive manufacturing (LAM), [17] and so on. These graphene-reinforced MMCs show impressive strength and toughness. A small amount of added graphene can greatly improve the mechanical properties of the MMCs, such as tensile properties and wear resistance. Regarding the mechanical properties of graphene-reinforced MMCs, the uniform graphene dispersion, the bonding interface between graphene and the matrix, and the arrangement of graphene in the matrix are still the main factors influencing the large-scale applications of graphene-reinforced MMCs. [18] The dispersion and arrangement of graphene in the matrix are the basic factors affecting the MMCs. The poor dispersion and disordered arrangement will result in agglomeration of graphene and weakly bonded interfaces between reinforcement and matrix phases. These defects lead to crack initiation and propagation, [19] which ultimately weakens the reinforcing effect of graphene. Therefore, improving the properties of MMCs by structural design to change the spatial distribution pattern of the micro-/ nanograde reinforcement phase in the matrix has become urgent in current research.