Ceramic combuster can for a gas turbine engine

摘要

A combustor assembly (10) having a support assembly (16) between a metal support assembly and a ceramic combustor can section (18) that accommodates a thermal expansion difference therebetween. An air fuel mixer (12) and an igniter (14) are mounted to the support assembly (16) secured to the ceramic combustion can (18) which receives the ignition products of the ignited fuel and air mixture.