发明名称 Tandem air inlet apparatus and method for an airborne mobile platform
摘要 <p>A tandem inlet apparatus for use with a high speed mobile platform, for example a commercial or military aircraft. The tandem inlet apparatus includes a Pitot inlet for feeding air to a cabin air compressor (CAC) of an air conditioning pack carried on the mobile platform. A flush heat exchanger inlet is disposed forwardly of the Pitot inlet and longitudinally aligned with the Pitot inlet, for supplying cooling air to a heat exchanger of the air conditioning pack. By locating the heat exchanger inlet forwardly and longitudinally in line with the Pitot inlet, the heat exchanger inlet is able to effectively swallow a large portion of the boundary layer, which results in a thinner boundary layer at the inlet face of the Pitot inlet. This enables a smaller throat area Pitot inlet to be used, as well as a shorter diverter height to be employed with the Pitot inlet, while still realizing an improved recovery factor (RF) performance with the Pitot inlet. The reduced height Pitot inlet also enables drag to be reduced.</p>
申请公布号 GB2456465(B) 申请公布日期 2011.03.16
申请号 GB20090008935 申请日期 2007.10.16
申请人 THE BOEING COMPANY 发明人 WARREN A ATKEY;PRADIP G PARIKH
分类号 B64D13/02;B64C21/00 主分类号 B64D13/02
代理机构 代理人
主权项
地址