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.
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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 |
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代理人 |
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主权项 |
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地址 |
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