AIRCRAFT COOLING SYSTEM AND METHOD FOR OPERATING AN AIRCRAFT COOLING SYSTEM

摘要

The invention relates to a cooler (10) for an aircraft cooling system (100), comprising a matrix body (12) in which a plurality of coolant channels (16) are designed and extend from a first surface (18) of the matrix body (12) to a second surface (20) of the matrix body (12), allowing a coolant to flow through the matrix body (12). The matrix body (12) of the cooler is designed to form a section of the outer skin of the aircraft.