发明名称 Tubular acoustic attenuation piece for an aircraft jet engine air intake
摘要 Tubular acoustic attenuation piece for an aircraft jet engine air intake.According to the invention, said tubular piece (1) is made up of shells (2) with a cellular core (5) assembled only by external fish plate strips (8), the facing edges (6) simply being edge faces of said shells (2) forming slots (9) between them.
申请公布号 US6761245(B2) 申请公布日期 2004.07.13
申请号 US20020274967 申请日期 2002.10.22
申请人 AIRBUS FRANCE 发明人 PORTE ALAIN
分类号 F02C7/045;F02K1/82;(IPC1-7):G10K11/00 主分类号 F02C7/045
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