发明名称 Acoustic processing panel for nacelle of aircraft, has ducts provided for hot air, where each duct is defined by partitions extending from resistive structure to reflective layer to insulate cell strips in longitudinal direction of nacelle
摘要 <p>The panel has an acoustic resistive structure and a reflective layer between which strips of honeycomb cells are provided in a direction perpendicular to a longitudinal direction of a nacelle. The strips are spaced apart so as to enable passage of hot air flow for treating icing, and hot air ducts are provided for passage of the hot air. Each duct is defined by two partitions (36.1, 36.2) extending from the resistive structure to the reflective layer so as to insulate the cell strips in the longitudinal direction. Draining ducts evacuate water, and are placed against the reflective layer.</p>
申请公布号 FR2950325(A1) 申请公布日期 2011.03.25
申请号 FR20090056552 申请日期 2009.09.23
申请人 AIRBUS OPERATIONS 发明人 CHELIN FREDERIC;LAMBERT DAVID;HARO DOMINIQUE
分类号 B64D33/02;B64D15/04;F02C7/045;F02C7/047 主分类号 B64D33/02
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