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a tilted platform. Gravity then causes
                                                                              the  panel  to slide  down.  The  panel,
                                                                              when moving, is not in contact with the
                                                                              handling robot; therefore, the elevated
                                                                              temperature is kept uniform across the
                                                                              panel while being transported. The
                                                                              mechanism to be applied for panel-level
                                                                              debonding is baselining the effectiveness
                                                                              on a 300mm format contactless transport.
                                                                              Thermal control
                                                                                A round 300mm thermal chuck surface
        Figure 9: Defined test vehicle based on the panel layout: a) single matrix; b) 2x2 matrix; and c) single matrix   is proven to be within the ±2°C for 200°C
        with rectangular die.                                                 (tighter range on lower temperature),
                                                                              which is above the release temperature
        Large-panel thermal debonding      thermal imbalance, causing the part in   range of 175-195°C of the commercially-
          I n ther mal  debondi ng  (Figure   contact to shrink/contract resulting in   available thermal release tapes.
        3), process temperat u re, timing,   warpage (Figure 4).                A previously presented paper [3] showed
        and handling are defined as critical   Handling is more complicated with   the effects of thermal nonuniformity
        factors to ensure high yield. Panel   a larger area. The end effector design,     on die shift. Wafers subjected to a high
        handling is essential to ensure no   weight, and size of the panel will   nonuniformity chuck vs. a chuck of
        excursion occurs. This is the first step   contribute to the overall warpage and the   186°C ± 1°C showed significant yield
        where panel fragility (thickness, die   stability of the panel when transported.   performance (Figure 7). The wafer in
        placement layout, etc.) and weight will   A common handling mechanism is pick-  Figure 7a showed high nonuniformity,
        be a factor to consider in defining a   and-place using a robot with a customized   while the wafer in Figure 7b has ±1°C
        handling mechanism.                end effector (Figure 5).           uniformity. The corresponding die shift
          Thermal control needs to be robust   Another method is the air cushion   showed that with higher nonuniformity
        to maintain adequate uniformity across   mechanism (Figure 6), which is   the  die  shift  is  larger  in magnitude
        a larger surface. The thermal sensitive   contactless transport whereby the panel   compared to a chuck with high thermal
        tape needs to activate across the entire   is lifted with controlled air pressure on   uniformity [3] (Figure 8).





















        Figure 10: Temperature profile of the chuck measured at: a) 100°C; b) 150°C; and c) 200°C.

        surface uniformly to eliminate not only
        potential cosmetic defects, but also
        excursion. The mechanical separation
        of the carrier and the panel can only
        happen when the thermal release tape
        has been fully activated uniformly
        across the whole surface.
          Hand l i ng and t ranspor t. T he
        handling method of molded wafers is
        critical in minimizing handling-induced
        warpage [2]. With a high-temperature
        molded  wafer,  any  introduction  of
        low-temperature objects will create   Figure 11: Warpage profiles for: a) sample 1; and b) sample 2.

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