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.
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
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