发明名称 |
painel de estruturação composto, método para fabricar painel e elemento de aeronave. |
摘要 |
The invention relates to a composite structuring panel (1) for the trailing edge of an aircraft element, having: an upper surface (3); a lower surface (5); an edge (7) connecting said upper (3) and lower (5) surfaces; the upper surface (3) and the lower surface (5) being connected by transverse stiffeners (9) and the structuring panel being made of a unitary part forming the upper surface (3), the lower surface (5), the edge (7), and the transverse stiffeners (9). The invention also relates to a method for manufacturing such a panel (1), and to an aircraft element comprising such a panel (1). |
申请公布号 |
BRPI1012058(A2) |
申请公布日期 |
2016.03.15 |
申请号 |
BR2010PI12058 |
申请日期 |
2010.05.28 |
申请人 |
SOCIETE LORRAINE DE CONSTRUCTION AERONAUTIQUE |
发明人 |
ARNAUD BERTRAND;DENIS MILLEPIED;DIDIER REMENE;JEAN-LUC PACARY;PAULO FRANCISCO;VALÉRIAN MONTAGNE |
分类号 |
B29C70/30;B29D24/00;B29D99/00;B32B3/06;B64C3/18;B64C3/20;B64C3/26;B64C3/28 |
主分类号 |
B29C70/30 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|