The invention discloses a method for printing a
combustion chamber lining by using GRCop-42 spherical
powder. The GRCop-42
alloy spherical
powder comprises the following chemical components in percentage by weight: 2-4wt% of Cu, 2-4wt% of Cr and Nb. The method comprises the following steps of: 1) heating the spherical
powder in vacuum, cooling the spherical powder along with a furnace, then performing
ultrasonic vibration, screening the spherical powder and preparing to
discharge the spherical powder into the furnace; 2) establishing a process model of a part, and
slicing the model in
layers to form a
laser scanning path of each layer; 3) setting process parameters of powder laying and printing equipment, placing a rear bottom plate substrate, and fully laying the GRCop-42 spherical powderin a powder cylinder; 4) starting the equipment and starting printing and forming; 5) after
laser scans one layer, descending a forming cylinder by one layer, then ascending the powder cylinder by one layer, laying a layer of
copper powder on the processed layer surface by using the powder in the powder cylinder through a scraper, then descending the powder cylinder, and repeating the steps on each layer until the printing of the structure is finished; 6) performing annealing treatment; and 7)
cutting and separating the structure from the substrate, and performing
sand blasting on the surfaceof the structure. The method solves the problem of domestic application of
advanced materials, and meets the preparation requirement of an
aerospace copper alloy structure.