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COOLER FOR AN AIRCRAFT COOLING SYSTEM, AIRCRAFT COOLING SYSTEM AND METHOD FOR OPERATING AN AIRCRAFT COOLING SYSTEM
COOLER FOR AN AIRCRAFT COOLING SYSTEM, AIRCRAFT COOLING SYSTEM AND METHOD FOR OPERATING AN AIRCRAFT COOLING SYSTEM
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机译:用于飞机冷却系统的冷却器,飞机冷却系统以及用于操作飞机冷却系统的方法
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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.
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