发明名称 Leading edge for aircraft wings and empennages
摘要 <p>The leading edge structure (10) comprises two or more multilayer panels (20) 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 layer (21) consisting of a metal foil, - a second intermediate layer (22) of fibre-glass securely fixed to the first layer (21), and - a third metal honeycomb layer (23) securely fixed to the second layer (22).</p>
申请公布号 EP2196309(B1) 申请公布日期 2011.11.09
申请号 EP20090177579 申请日期 2009.12.01
申请人 ALENIA AERONAUTICA S.P.A. 发明人 CAPASSO, LUIGI;FASSERO, MARCO;RICCIO, MASSIMO;RINALDI, ERNESTO;RUSSO, SALVATORE
分类号 B32B3/12;B32B15/14 主分类号 B32B3/12
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