发明名称 |
AIRCRAFT COOLING SYSTEM AND METHOD FOR OPERATING AN AIRCRAFT COOLING SYSTEM |
摘要 |
<p>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.</p> |
申请公布号 |
EP2408671(B1) |
申请公布日期 |
2013.05.08 |
申请号 |
EP20100708126 |
申请日期 |
2010.03.05 |
申请人 |
AIRBUS OPERATIONS GMBH |
发明人 |
BAUMGARDT, TORBEN;STOLTE, RALF-HENNING;WEBER, CARSTEN;REYNAUD, REMY;MUELLER, CHRISTIAN |
分类号 |
F28F13/00;F28F7/02 |
主分类号 |
F28F13/00 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|