Corrosion-resistant material for large propeller blade and preparation method
A corrosion-resistant material and technology for propellers, which are applied in the field of corrosion-resistant materials and preparation for large-scale propeller blades, can solve problems such as the strength and corrosion resistance of copper alloys, the corrosion resistance of propellers, and the inability to replace copper alloys. , to achieve the effect of improving corrosion resistance and prolonging service life
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Embodiment 1
[0075] The corrosion-resistant material for large-scale propeller blades according to the present invention, the chemical composition contained in the material and its mass percentage are as follows: copper is used as the main raw material, and Fe iron: 3.5% to 10.5%; Sr strontium: 1.5% to 1.7% ;Si silicon: 0.01%~1.2%; B boron: 0.003%~0.048%; Mn manganese: 2.3%~4.1%; Ni nickel: 3.5%~7.5%; Mo molybdenum: 0.3%~0.9%; %~0.15%; Zn Zinc: 0~1.5%.
[0076] On this basis, a method for preparing a corrosion-resistant material for large propeller blades is also provided, comprising the following steps:
[0077] (1) Preparation of materials: weigh each component material required, the proportion is qualified, and add according to the weight ratio;
[0078] (2) First add 3.5-10.5 parts of iron, 0.3-0.9 parts of molybdenum, 0.01-1.2 parts of silicon and 0.003-0.048 parts of boron, heat to 2200-2400 degrees Celsius, and fully stir to obtain a mixture;
[0079] When the temperature reaches ...
Embodiment 2
[0085]Corrosion-resistant materials for large propeller blades. The chemical composition and mass percentage of the material are as follows. Copper is the main raw material. Among other materials, the weight ratio of Si and B in the percentage content is: (0.02-0.4): (0.005 -0.04).
[0086] Further, the Si / B ratio of the elements Si and B by weight has a minimum value of 0.5 and a maximum value of 10, which can ensure the improvement of alloy performance.
Embodiment 3
[0088] A corrosion-resistant material for large propeller blades, the components of which include by weight percentage: Fe iron: 5.2% to 10.1%; Sr strontium: 1.3% to 1.65%; Si silicon: 0.26% to 0.94%; B boron: 0.014% %~0.026%; Mn manganese: 2.35%~3.63%; Ni nickel: 4.8%~6.6%; Mo molybdenum: 0.44%~0.79%; P phosphorus: 0.008%~0.091%; Zn zinc: 0.83%~1.25%; The remainder is Cu and unavoidable impurities.
[0089] On this basis, a method for preparing a corrosion-resistant material for large propeller blades is also provided, comprising the following steps:
[0090] (1) Preparation of materials: weigh each component material required, the proportion is qualified, and add according to the weight ratio;
[0091] (2) First add Fe: 5.2% to 10.1%, Mo: 0.44% to 0.79%, silicon 0.26% to 0.94% and boron 0.014% to 0.026%, heat to 2200-2400 degrees Celsius, and fully stir to obtain mixture;
[0092] When the temperature reaches between 650°C and 950°C, perform at least one thermoforming ope...
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