发明名称 Turbofan exhaust system
摘要 A turbofan exhaust system includes at least one exhaust nozzle with a trailing edge having an upper edge, a lower edge, an inner lateral edge-and an outer lateral edge. The upper edge is upstream with respect to the lower edge. The outer lateral edge of the exhaust nozzle is also upstream of the inner lateral edge. This arrangement makes it possible to reduce the noise perceived in the cabin of the aircraft at the same time as the noise perceived on the ground.
申请公布号 US7845156(B2) 申请公布日期 2010.12.07
申请号 US20070627643 申请日期 2007.01.26
申请人 SNECMA 发明人 BIGOT PASCAL MOISE MICHEL;CHANEZ PHILIPPE GERARD
分类号 F02K1/00;F02K1/78 主分类号 F02K1/00
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