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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Bibliographic Details
Main Authors CUNHA, Frank J, KOSTKA, Stanislav
Format Patent
LanguageEnglish
French
German
Published 28.04.2021
Subjects
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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Summary: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.
Bibliography:Application Number: EP20150185959