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  • ISSN: 0577-6686

Journal of Mechanical Engineering ›› 2025, Vol. 61 ›› Issue (4): 107-115.doi: 10.3901/JME.2025.04.107

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Preparation and Stiffness Property of Cf/Mg Composite Special-shaped Thin Parts Fabricated by Liquid-solid Extrusion Following Vacuum Pressure Infiltration

CHEN Baolin1, LU Zhuqing2, ZHOU Jiming1,3, JU Luyan1, QI Lehua1,3   

  1. 1. School of Mechanical Engineering, Northwestern Polytechnical University, Xi'an 710072;
    2. Western Superconducting Technologies Co., Ltd., Xi'an 710018;
    3. Shaanxi Key Laboratory of Fiber Reinforced Light Composite Materials, Xi'an 710072
  • Received:2024-02-06 Revised:2024-07-11 Published:2025-04-14

Abstract: The carbon fiber reinforced magnesium matrix (Cf/Mg) composites exhibit light weight, high specific strength and modulus as well as excellent dimensional stability, which means more potential for engineering applications such as in aeronautic/astronautic equipment, light armaments, and railway traffic equipment. Due to the poor wettability and the high-temperature reaction between the carbon fiber and magnesium alloy, especially the forming thin parts with the thin wall and complex shapes, the incomplete filling or the nonuniform infiltration of liquid magnesium at variable cross-section is prone to occur. These challenges increase the difficulty of the preparation, which limits the practical applications of Cf/Mg composites. The liquid-solid extrusion following vacuum pressure infiltration mainly includes the following steps. Firstly, the molten metal infiltrates partially into the fiber preform under a vacuum environment. Then, the preform is fully infiltrated by a hydraulic pressure. When the metal solidifies into a liquid-solid state, a high pressure is applied to further restrict the shrinkage and increase the densification. The process can improve the overall performance of composite parts. Taking the preparation of an electronic mounting plate of the missile as a typical example, the process steps, process parameters, tensile properties and integral stiffness of the composite plate are studied in detail. The result shows that the fabricated Cf/Mg thin parts can meet the requirements of practical applications. When the extrusion temperature is 600 ℃ and the circulating cooling system is installed, the preform is completely and uniformly infiltrated by the molten magnesium alloy. The detrimental interfacial reaction between the fiber and magnesium alloy is decreased by the designed circulating cooling system, which further improves the mechanical properties of Cf/Mg thin parts. The ultimate tensile strength and elastic modulus reach up to 328 MPa and 68 GPa, respectively, which are 24% and 6% higher than those of uncirculated cooling parts, and are 139% and 79% higher than those of magnesium alloy parts. The overall load-bearing capacity of the parts was tested. The deformation of the circulated cooling parts under the 700 N pressure is only 0.313 mm, which is reduced by 2/3 of that of magnesium alloy parts. The objective of this study is to lay a foundation for the preparation and application of Cf/Mg composite structural parts.

Key words: magnesium matrix composites, liquid-solid extrusion following vacuum pressure infiltration, carbon fibers, special-shaped thin parts, integral stiffness

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