The present invention discloses a heavy type gas
turbine compressor exhaust cylinder
casting process, in order to fully feed the
casting solidification process, a cylinder body is vertically poured, an annular open riser is placed on the upper part of the cylinder body, a plurality of annular blind risers are placed on a sector, a
chiller and a patch are simultaneously assembled for feeding the
casting; a wood-type
skin sample is used for shaping to ensure a
precision casting size; an alkaline phenolic resin sand is used as back sand, chrome ore sand is used as a surface sand, and the air permeability and deformability of the sand mold surface can be increased; an open-type water
nozzle is used for pouring, the chance of casting
distortion can be reduced, and the casting quality is improved. Compared with the prior art, the beneficial effects are that: the technical problems of the defects of being complex in structure, large in volume, uneven in partial casting wall thickness, difficult to feed, easy to deform, easy to loosen, crack and deform, and the like of a heavy type gas
turbine compressor exhaust cylinder
steel casting part can be effectively solved.