A catalytic combustion system has been developed which feeds full fuel
and air to the catalyst but avoids exposure of the catalyst to the hi
gh temperatures responsible for deactivation and thermal shock fractur
e of the supporting substrate. The combustion process is initiated by
the catalyst and is completed by homogeneous combustion in the post ca
talyst region where the highest temperatures are obtained. Catalysts h
ave been demonstrated that operate at inlet temperatures as low as 320
degrees C at 11 atm total pressure and conditions typical of high per
formance industrial gas turbines. The ignition temperature is shown to
correlate with the specific catalytic activity of the washcoat layer
over a rather broad range of activities. A reaction model has been dev
eloped that can predict ignition behavior from the measured catalytic
activity.