TURBINE ENGINE DIFFUSER ASSEMBLY WITH AIRFLOW MIXER

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 mi...

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Bibliographische Detailangaben
Hauptverfasser:	CUNHA, Frank J, KOSTKA, Stanislav
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	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.