Mullite-based fiber-reinforced composites are favorite candidates for the a
pplication in combustion chambers of gas turbines. The application requires
damage tolerance, temperature and oxidation-resistance at high temperature
s (> 1200 degreesC) over long terms. In order to realize crack deflection a
nd fiber pull-out, an interphase coating of the mullite fibers (Nextel (TM)
720) is necessary to obtain a weak bonding between fibers and matrix. Two
systems of interphases produced by CVD were described. The first system is
a carbon/metal-oxide double layer (C/ZrO2, C/Al2O3). Properties of the resu
lting composites after heat-treatment (1300 degreesC, 1000 h) under cyclic
and continuous heating conditions were described.
The second system is the codeposition of La2O3 and Al2O3 on the fibers. Aft
er heat-treatment at 1300 degreesC lanthanum hexaluminate (LaAl11O18) with
a magneto plumbite structure containing sliding planes should be formed.