发明名称 Air intake of a turbofan engine
摘要 <p>The inlet has lower and upper parts (115I, 115S), and internal and external lateral leading edges (115int, 115ext) defining a lip (115) between external and internal surfaces (111, 113) of a nacelle (110) for forming an air supply channel. The external leading edge is arranged in rear with respect to the internal leading edge. The profile of the air inlet sleeve conforms to an aerodynamic profile.</p>
申请公布号 EP1813529(A1) 申请公布日期 2007.08.01
申请号 EP20070101190 申请日期 2007.01.25
申请人 SNECMA 发明人 CHANEZ, PHILIPPE;LOHEAC, PIERRE
分类号 B64D33/02;B64C1/40;F02C7/045 主分类号 B64D33/02
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