发明名称 Soundproof aircraft engine nacelle
摘要 The pod has a tubular air intake (6) comprising an acoustic-attenuation internal tubular piece (10) of resonator type. A tubular transition part (17), which has an acoustically homogeneous internal face, connects the air intake to a tubular fan casing (16). The internal face of the internal tubular piece and the internal face of the transition part are in aerodynamic continuity. The internal tubular piece has no internal assembly fishplate.
申请公布号 EP1426587(A1) 申请公布日期 2004.06.09
申请号 EP20030292321 申请日期 2003.09.22
申请人 AIRBUS FRANCE 发明人 PORTE, ALAIN;BATARD, HERVE
分类号 F02C7/045;(IPC1-7):F02C7/045 主分类号 F02C7/045
代理机构 代理人
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