The invention relates to the technical field of
turbofan casting and in particular relates to a
casting method of a
turbofan. The technological process of the
casting method comprises the steps of material inspection, production of precoated sand, core producing / modeling, core setting, mould assembling,
smelting, pouring, mould disassembling, casting head knocking, coarse
polishing, clearing, burnishing, elaborate
polishing, appearance inspection, oiling, warehousing inspection, packaging and delivery, wherein in the core setting step, a core III is set into a lower mould firstly, and then a core II and a core I are set into the lower mould sequentially; in the pouring steps, molten iron is poured in a suspended manner through a traveling crane to enter from an upper mould and is poured at the periphery while oppositely poured at two sides, and then
exhaust gas is ignited by
open fire by a worker. The casting method adopts a flat mould pouring method, and the core head part of the mud core II extends and is pressed and fixed by the mud core I, so that
scrap caused by upward floating of the mud cores can be effectively prevented. According to an existing pouring process, the molten iron enters from the periphery, and the top end is open for exhaust, so that the mould filling of the molten iron can be relatively stable and is conducive to exhaust.