发明名称 |
LEADING EDGE FOR AIRCRAFT WINGS AND EMPENNAGES |
摘要 |
A leading edge structure includes two or more multilayer panels at least partially overlapping and suitably curved with at least partially congruent concavities. Each multilayer panel includes at least the following three layers: a first metal foil layer metal foil, a second intermediate layer of fibre-glass securely fixed to the first layer, and a third metal honeycomb layer securely fixed to the second layer.
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申请公布号 |
US2010140405(A1) |
申请公布日期 |
2010.06.10 |
申请号 |
US20090634402 |
申请日期 |
2009.12.09 |
申请人 |
ALENIA AERONAUTICA S.P.A. |
发明人 |
CAPASSO LUIGI;FASSERO MARCO;RICCIO MASSIMO;RINALDI ERNESTO;RUSSO SALVATORE |
分类号 |
B64C3/20 |
主分类号 |
B64C3/20 |
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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