ENGINE COOLING SYSTEM FOR AIRPLANE

摘要

The present invention relates to an engine cooling system for an airplane. The engine cooling system for an airplane according to one embodiment of the present invention includes a cowl which surrounds an aerial engine and a baffle which divides the inner part of the cowl into an upper part and a lower part. According to one embodiment of the present invention, an air inlet is formed in one side of the cowl. An air outlet is formed in the other side of the cowl. According to one embodiment of the present invention, the baffle is formed in the inner part of the baffle. More particularly, in an aspect of the present invention, the engine cooling system for an airplane can include other embodiments.