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    It is known that a remarkable difference from sintering and
    posttreatment processes will result from different powder
    materials used in SLS process. Unlike the pretext investiga-
    tions, polymer powder mixed composite elemental metal
    powders were used for forming materials in this work, which
    had been proven to be flexible and convenient in literature [6].
    This work is concerned mainly on how the green part was
    formed with polymer powder mixed with composite elemental
    metal powders, the influences fromheat transmission when the
    powders were heated by laser beam, the removal of redundant
    loose powders from the cooling channels, the detailed
    infiltration method, the microstructure of infiltrated materials,
    and the injection plastic part generated by the final mold.
    2 Experimental
    2.1 Materials
    Epoxy powders mixed with composite elemental metal
    powders presented in literature [6] were chosen as SLS-
    forming powders in this work. The content of epoxy in the
    mixed powders was 4%. The composite elemental metal
    powders were composed of iron, copper, nickel, and carbon
    as shown in Table 1. Bronze powders were chosen for
    infiltrating materials in the posttreatment process.2.2 Experiment path
    Elemental metal powders and epoxy powders weremixed in a
    three-dimensional motional blending machine initially. Then
    the composite powders were sintered in an SLS system
    developed by Huazhong University of Science and Technol-
    ogy. According to dimensional and structural characteristics
    of the insert, forming path and process parameters were
    designed to guarantee the precision and strength of the SLS
    green insert. Two cubic green parts (120 mm×20 mm×
    15mm)werealsoformedtobeemployedascomparative
    specimens with the inserts. The green inserts and the cubic
    parts were both heated at 80°C/1 h for strength enhancement
    in a furnace. Then, they were infiltrated by bronze melt under
    the protection of H2 in a graphite cabin after they had been
    debinded and sintered at 1,000°C/1 h. The infiltrating
    temperature was set at 1,080°C and then, the infiltrated
    inserts were cooled naturally in the furnace. Debinding
    process followed what was expressed in literature 6. The
    infiltrated inserts and one of the cubic parts were treated
    following the process listed in Table 2, and then, two groups
    of tensile test samples (Fig. 1) made from the cubic parts
    before and after thermal treatment were processed. There
    were five tensile test samples in each group, and the final test
    results were the mean value of five samples in each group.
    SEM samples made of the cubic parts before and after
    thermal treatment were also produced to analyze the
    variation of alloys microstructures.Polymer powders are heated by laser beam in the composite
    powders, and they turn into viscous liquid to adhere other
    hard powders around them together. It is possible for the
    powders which do not belong to scanning cross-sections to
    be softened owing to the heat accumulation and transmis-
    sion within the powders during sintering process. There-
    fore, loose powders inside of the cooling channels are liable
    to be heated to stick to the channels' wall. This will trouble
    the removal of powder and further affect the precision of
    the green inserts under such conditions. Thermal accumu-
    lations and transmissions are affected by the positionrelationship between the channel structure and the laser
    beam, which is decided by the forming path.
    Figure 3 shows the heat transmission between the
    successive layers. qSG in Fig. 3 is heat flux density of
    convection and qSS is heat flux density of conduction. T1 is
    the temperature after laser energy has been absorbed by a
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