DIFFUSER CASE HEAT EXCHANGER

A gas turbine engine includes a bypass duct for a bypass airflow and a diffuser case including an inlet in communication with the bypass duct for communicating a bypass flow to a heat exchanger portion. An outlet passage extends through the bypass duct to exhaust airflow exiting the heat exchanger p...

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Bibliographic Details
Main Authors DISORI, Michael A, STILLMAN, William P, HYLAND, Dave J
Format Patent
LanguageEnglish
French
German
Published 24.03.2021
Subjects
AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Summary:A gas turbine engine includes a bypass duct for a bypass airflow and a diffuser case including an inlet in communication with the bypass duct for communicating a bypass flow to a heat exchanger portion. An outlet passage extends through the bypass duct to exhaust airflow exiting the heat exchanger portion outside of the bypass duct.
Bibliography:Application Number: EP20200172476