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
2024-03-26
Patent
Electronic Resource
English
Cooling of Military Avionic Equipment
SAE Technical Papers | 2015
NTIS | 1987
|NTIS | 1987
|The Cooling of a Pod-Mounted Avionic System
NTIS | 1976
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