Cooling systems for use on aircraft

Power plants – Combustion products used as motive fluid – Combustion products generator

Reexamination Certificate

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Details

C060S226100, C060S785000

Reexamination Certificate

active

07856824

ABSTRACT:
Cooling systems for an aircraft are provided. In an embodiment, a system includes an engine nacelle, an engine, a bypass duct, and a heat exchanger. The engine nacelle includes an airflow inlet. The engine is housed in the engine nacelle in flow communication with the airflow inlet. The bypass duct extends between the engine nacelle and the engine is in flow communication with the airflow inlet. The bypass duct includes an outer wall and an opening formed therein. The heat exchanger is integrated with the engine and is disposed over the opening of the bypass duct outer wall between the bypass duct outer wall and the engine nacelle.

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