发明名称 |
Cooling system for use in airplane, comprises device for exhausting boundary layer air at flow critical upper surface of airplane |
摘要 |
<p>The cooling system (100) comprises a device (101) for exhausting a boundary layer air at a flow critical upper surface (120) of the airplane. A heat exchanger is provided for cooling of a medium, where the heat exchanger is flown through the exhausted boundary layer air.</p> |
申请公布号 |
DE102007019820(A1) |
申请公布日期 |
2008.11.06 |
申请号 |
DE20071019820 |
申请日期 |
2007.04.26 |
申请人 |
AIRBUS DEUTSCHLAND GMBH |
发明人 |
WESTENBERGER, ANDREAS;ARENDT, MARTIN;MARQUARDT, TILL;FRAHM, LARS;SCHRAUF, GEZA |
分类号 |
B64D13/08;B64C21/06 |
主分类号 |
B64D13/08 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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