AIRCRAFT TAIL REGION WITH A COOLING SYSTEM INSTALLED IN AIRCRAFT TAIL REGION

摘要

An aircraft tail region (10) includes a cooling system (12) installed in the aircraft tail region (10). The cooling system (12) comprises a cooler (14), which forms a section of an outer skin (16) of the aircraft tail region (10), and includes coolant channels (20) allowing a flow of ambient air therethrough, and extending from a first surface (22) of the cooler (14) to a second surface (24) of the cooler (14). The cooling system (12) also includes a fan system (28), which is adapted to convey ambient air through the coolant channels (20) of the cooler (14) at least in specified operating phases of the cooling system (12), and a first opening (34), which is formed in the outer skin (16) of the aircraft tail region (10), and which allows, in conveying operation of the fan system (28), ambient air which is supplied through the coolant channels (20) of the cooler (14) into an interior of the aircraft tail region (10) to be discharged back into the aircraft environment.