发明名称 Sound absorbing panel particularly for aircraft engine
摘要 <p>The sandwich noise insulation panel for an aircraft has a reinforcing layer (10), a reflector (12) and a frame (14) between these to form cells (16) separated by partitions (18). Separators (20) in the cells each have a circular peripheral wall (20a) and positioners (22) for he separators in the cells. The positioners are attached to the separators and engage against the partitions.</p>
申请公布号 EP1201420(A1) 申请公布日期 2002.05.02
申请号 EP20010402803 申请日期 2001.10.29
申请人 AIRBUS FRANCE 发明人 PORTE, ALAIN;BATARD, HERVE
分类号 B32B3/12;E04C2/36;F02C7/045;F02K1/82;G10K11/172;(IPC1-7):B32B3/12;G10K11/168 主分类号 B32B3/12
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