发明名称 |
REINFORCED COMPOSITE SANDWICH PANEL |
摘要 |
The invention relates to a composite sandwich panel (1) comprising at least a web (2) provided between an inner skin (3) and an outer skin (4), each skin being made of a composite material from a plurality of fibrous plies (5, 6, 7, 8), characterised in that a portion of the plies of the inner skin and/or of the outer skin each extends at least partially through the web at an uninterrupted area thereof in order to form together a through-reinforcement (9) extending from the inner skin to the outer skin of the composite sandwich panel. The invention further relates to an aircraft element including such a composite sandwich panel. |
申请公布号 |
WO2010034894(A1) |
申请公布日期 |
2010.04.01 |
申请号 |
WO2009FR01020 |
申请日期 |
2009.08.21 |
申请人 |
SOCIETE LORRAINE DE CONSTRUCTION AERONAUTIQUE;PACARY, JEAN-LUC;FRANCISCO, PAULO |
发明人 |
PACARY, JEAN-LUC;FRANCISCO, PAULO |
分类号 |
B32B5/02;B32B1/00;B32B7/00;B64C1/00 |
主分类号 |
B32B5/02 |
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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