TURBINE ENGINE DIFFUSER ASSEMBLY WITH AIRFLOW MIXER

摘要

A diffuser assembly is provided for a turbine engine. This diffuser assembly includes a diffuser module 50 with a combustor plenum 48 and a mixing chamber 70. The diffuser module 50 is configured to receive first and second airflows into the mixing chamber 70 and direct a mixed airflow out of the mixing chamber 70. The diffuser module 50 includes a mixer 102 configured to mix the first and the second airflows together within the mixing chamber 70 to provide the mixed airflow.