发明名称 CONE D'ECHAPPEMENT AVEC SYSTEME D'ATTENUATION ACOUSTIQUE
摘要 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.
申请公布号 FR2987079(B1) 申请公布日期 2017.02.10
申请号 FR20120051472 申请日期 2012.02.17
申请人 SNECMA PROPULSION SOLIDE 发明人 MECUSON GAUTIER;CONETE ERIC
分类号 F02K1/44;F02K9/97 主分类号 F02K1/44
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