发明名称 EXHAUST CONE WITH ACOUSTIC ATTENUATION SYSTEM
摘要 <p>An aeroengine exhaust cone is arranged to extend from upstream to downstream along a longitudinal axis. The cone comprises a structural core of composite material made up of an axisymmetric part having an upstream endpiece at its upstream end and a downstream endpiece at its downstream end. The core provides structural strength to the cone. The cone has an acoustic attenuation system made of composite material and fastened on the structural core.</p>
申请公布号 EP2815118(A1) 申请公布日期 2014.12.24
申请号 EP20130710461 申请日期 2013.02.15
申请人 HERAKLES 发明人 MECUSON, GAUTIER;CONETE, ERIC
分类号 F02K1/82;F01D25/30;F02C7/24 主分类号 F02K1/82
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