发明名称 Engine inlet with blown air drag reduction
摘要 An air intake system (10) for a turbo engine, wherein external engine boundary layer separation drag and external engine friction drag may be selectively reduced. A first air exit port (16) in the form at a plurality of air exit jets (30) is in fluid communication with air inlet pores (28) and noise reduction cells (24) for reduction in boundary layer separation drag. A second air exit port (18) in the form of air exit pores (32) is in fluid communication with air inlet pores (28) and noise reduction cells (24) for reduction in external engine friction drag. A control device (20) uses input from engine drag sensing device (36) and environmental sensing device (38) to respectively control air flow to air exit jets (30) and air exit pores (32) with first port valve (40) and second port valve (42).
申请公布号 GB2354812(A) 申请公布日期 2001.04.04
申请号 GB20000009552 申请日期 1998.07.16
申请人 * NORTHROP GRUMMAN CORPORATION 发明人 RUNYON H * TINDELL;CHARLES A * PARENTE
分类号 B64C21/02;B64C21/08;B64D29/02;(IPC1-7):B64C21/08;B64D33/02 主分类号 B64C21/02
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