Pouring and polishing process for propeller and copper alloy formula for propeller
A propeller, copper alloy technology, applied in propellers, manufacturing tools, metal processing equipment and other directions, can solve the problems of poor anti-cavitation erosion performance of propellers, low mechanical strength of propellers, and easy to be eroded by seawater, etc. Performance, the overall connection strength will not be damaged, the effect of improving the overall mechanical properties
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Embodiment 1
[0040] A copper alloy for manufacturing propellers, the copper-aluminum alloy is composed of the following components in weight ratio: 7% aluminum, 8% manganese, 4% iron, 1% nickel, 1% zinc, and 0.1% titanium , chromium is 0.1%, cobalt is 0.010%, and the rest is copper.
[0041] A propeller pouring and grinding process, comprising the following steps:
[0042] The first step: copper alloy melting
[0043] S101. Rough smelting: put the copper alloy described in the above formula into the melting furnace for heating and melting; at the same time, place a nitrogen blowing device on the melting furnace to blow nitrogen at low pressure and small flow rate;
[0044] S102. Refining: After rough refining, add ice crystal powder to the metal solution, the amount of ice crystal powder is 0.1% of the alloy mass; heat the furnace to 1000 degrees, and then add copper alloy refining slag removal agent with a mass fraction of 0.4% ;
[0045] Step Two: Pouring
[0046] S201. Inject the re...
Embodiment 2
[0099] Embodiment 2 differs from Embodiment 1 in that it is a copper alloy for manufacturing propellers, and the copper-aluminum alloy is composed of the following components in weight ratio: 8% of aluminum, 15% of manganese, 5% of iron, and 5% of nickel. 2%, 3% zinc, 0.2% titanium, 0.1% chromium, 0.02% cobalt, and the rest is copper.
[0100] The propeller made of the manufacturing materials produced in this case has been tested and has the following properties: the yield point of the propeller is 320N / mm2, the tensile strength is ≥660N / mm2, and the elongation is 18.5%, which is higher than the mechanical properties of the existing nickel-aluminum-bronze propeller . The performance index of the existing nickel-aluminum-bronze propeller: yield point 245N / mm2, tensile strength ≥ 590N / mm2, elongation 16% performance standard.
Embodiment 3
[0102] Embodiment 3 differs from Embodiment 1 in that it is a copper alloy for manufacturing propellers, and the copper-aluminum alloy is composed of the following components in weight ratio: 10% of aluminum, 20% of manganese, 6% of iron, and 6% of nickel. 3%, 6% zinc, 0.3% titanium, 0.3% chromium, 0.025% cobalt, and the rest is copper.
[0103] The propeller made of the manufacturing materials produced in this case has been tested and has the following properties: the yield point of the propeller is 300N / mm2, the tensile strength is ≥680N / mm2, and the elongation is 20.5%, which is higher than the mechanical properties of the existing nickel-aluminum-bronze propeller . The performance index of the existing nickel-aluminum-bronze propeller: yield point 245N / mm2, tensile strength ≥ 590N / mm2, elongation 16% performance standard.
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