Page 240 - Engineered Interfaces in Fiber Reinforced Composites
P. 240

222               Engineered interfaces in fiber reinforced composites

                                    500 I


                                 I 400
                                 m
                                 a
                                 E
                                   300
                                 c
                                 L
                                 u)
                                 kj
                                 5  200
                                 -
                                 IQ  ._
                                 u
                                 tu
                                 -
                                 re
                                 kJ 100
                                 +
                                 c
                                     0
                                      0      2     4      6     a     10     12
                                               Inverse of coating thickness Qm-ll
                    Fig. 5.36. Interface shear strength as a function of coating thickness for Nicalon  Sic fiber-Sic  matrix
                                            composites. After Lowden (1991).
                    fibers by  a  CVD process is also shown to be quite promising  for improved  high-
                    temperature  mechanical properties of  barium magnesium aluminosilicate (BMAS)
                    matrix composites (Sun et al., 1994). The duplex coating produces a stable interface
                    structure which is resistant to gross reaction at 1100°C for extended periods of time.
                    The turbostratic BN  layer offers a relatively weak interfacial zone,  allowing crack
                    deflection with associated high fracture toughness.
                      Some interesting results have been reported  based on the studies using Nicalon
                    Sic fibers-glass  matrix composites containing lithium aluminosilicate (LAS). X-ray
                    diffraction study shows two distinct carbon-rich reaction layers (Bender et al., 1986).
                    The first layer is essentially amorphous carbon of thickness about 100 nm, which is
                    adjacent to the Sic fiber. The carbon layer originates from excess carbon in the Sic
                    fiber which migrates to the fiber surface (Chaim and Heuer,  1987). Another source
                    of carbon is the residue left after heat cleansing of the organic size from the Sic and
                    of the organic binder from the prepreg. The second reaction layer is located between
                    the  first layer  and  the  LAS matrix,  consisting  predominantly  of  microcrystals  of
                    NbC. The niobium originates from the additive to the LAS glass as a crystallization
                    aid. The thickness of the second layer varies from 20 to 100 nm. Trace amounts of
                    impurities like Zr, Mg, Ti, K, Ba, Fe and As are also detected in the second layer,
                    that migrate to the interface region during processing. In this SIC-LAS  system, the
                    interface is relatively weak compared to the bulk fiber and matrix. It follows then
                    that debonding occurs inevitably between  the two reaction layers where the NbC
                    microcrystals are well developed (see Fig. 5.37).
   235   236   237   238   239   240   241   242   243   244   245