| 摘要 |
A cooling air supply system ( 10 ) for an aircraft in order to supply cooling air from the aircraft surrounds to at least two devices requiring cooling air ( 38, 44, 56 ) within the aircraft, is designed with an air inlet ( 12 ), an air channel ( 16 ) communicating with the air inlet ( 12 ) and with an air distribution device ( 30, 32, 34 ) for the distribution of air to at least two devices requiring cooling air ( 38, 44, 56 ), whereby the air inlet ( 12 ) is proportioned in such a way that it covers the maximum cooling air requirement of at least two devices requiring cooling air ( 38, 44, 56 ).
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