Integral gating system of certain airplane cabin door casting
An integral pouring and casting technology, applied in the direction of mold, core, mold composition, etc., can solve the problems of low filling pressure head and filling speed, low filling capacity and low tissue density
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[0018] The technical scheme of the present invention will be described in further detail below in conjunction with accompanying drawing and embodiment:
[0019] See attached Figure 1~5 As shown, the overall pouring system of a certain type of aircraft door casting, the outline size of the aircraft casting is 2225mm × 1200mm × 340mm, the casting includes an outer frame A, and 11 reinforcing ribs B are distributed along the width direction in the outer frame A , the cross-section of rib B is "I" shape, the thickness of the upper and lower beams of "I" shape is 6.5mm, the thickness of the middle longitudinal beam is 3mm, there are six bosses C on the outer frame A, two of which are bosses Platform C is located on one end face of the fourth and eighth reinforcement ribs B on the same side from the left, and it is characterized in that the gating system of the casting includes:
[0020] The first layer of runners 3 arranged below the casting mold 7, the first layer of runners 3 i...
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