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of the mechanical protection layer   a s s e m b l y  a n d  i n ter c o n n ec t i o n   ne e d for va cuu m-ba se d br a z i ng
        b e t we e n t h e si nt e r e d l aye r a n d   technologies. Various metal ceramic   tech nolog y. T he tech nolog y ha s
        the die, then propagating into the   substrates have been used; however,   been proven by thermal shock, peel
        front-side metallization of the die.   each provides drawbacks, including   st reng th, ther mal measu rements
        A degradation of the die attach is   precious metal content and a slow   and  thermal simulations. Numerous
                                                                                                         ®
        also observed. In the case of direct   vacuum brazing process. We have   studies show that Condura .ultra
        cooling, the same break propagation   found a solution that offers a cost-  enables  cost-efficient,  but  highly-
        f rom the edge of the mechanical   eff icient, highly-reliable Ag-free   reliable met al ceramic subst rate
        protection layer down to the  front-  thick-f il m copper bonding paste   manufacturing using Ag-free paste
        side met a l l i z at ion of t he d ie is   that joins nitride-based ceramics   and a non-vacuum-based brazing
                                                                                                          ®
        also obser ved. However, t here’s   with Cu foils and eliminates the   process. Additionally, DTS  can
        no degradation of the die attach,
        probably due to the more efficient
        heat  d issipat ion.  Fi n ite  element
        model (FEM) analyses show that
        t he l ifet i me reduct ion m ig ht be
        r el a t e d  t o  a n  i n c r e a s e d  pl a s t ic
        s t r a i n p e r c ycle i nt o t he f r ont-
        side metallization of the die. This
        could be due to a higher stiffness
        of the test vehicle and /or to the
        temperature being locally higher on
        the die at higher currents [6].
          B y e n a b l i n g h i g h e r p o w e r
        d e n s it ie s a n d  h ig h e r  o p e r a t i n g
        t e m p er a t u r e s ,  o u r  m ec h a n i c a l
        p r o t e c t i o n  l a y e r  t u r n s  o u t  t o
        b e  a s u i t a b l e s o l u t i o n f o r t h e
        i nt e r c o n n e c t io n s of SiC m e t a l-
        oxide semiconductor f ield-effect
        t r a n s i s t o r s  ( S i C -M O S F E TS ) .
        Power cycling tests demonstrated
        a  doubli ng  of  t he  lifet i me  when
                  ®
        using DTS  compared to sintered
        dies with Al interconnections [8].
        More  recently,  power  cycling  tests
        up to 20 0°C have  been repor ted
        w it h  D T S   a n d a 1, 20 0 V  S i C -
                   ®
        MOSFET from Wolfspeed [9]. In
        this case, the failure mechanism
        is a cohesive break in the sintered
        l a y e r, a l t hou g h a b r e a k i n t h e
        f r on t- s i d e  m e t a l l i z at ion  of  t h e
        d ie wa s expected. However, t he
        number of cycles  to failure is in
        line with results reported at lower
        o p er a t i n g  te m p er a t u r e s ,  t h er e -
        by demonst rating the robust ness
        of both die and package at 200°C
        (Figure 13).

        Summary
          As the semiconductor indust r y
        c o n t i n u e s  s e e i ng h i g h - p o w e r
        electronics applications, there is
        a need to provide reliable met al
        ceramic substrates that offer superior
        electrical, thermal, insulation and
        mechanical performance while also
        bei ng able to work w it h t y pical


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