An aircraft includes an airframe defining a first enclosed space, an engine bay disposed within the first enclosed space, and a cooling system. The engine bay includes a firebox defining a second enclosed space and an engine disposed at least partially within the second enclosed space. The cooling system is configured to selectively fluidly couple the first enclosed space with the second enclosed space.
AVIONIC EXHAUST AIR FOR COOLING ENGINE BAY
02.03.2023
Patent
Elektronische Ressource
Englisch
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