发明名称 |
ESTRUCTURA INTEGRADA DE AERONAVE EN MATERIAL COMPUESTO |
摘要 |
Integrated aircraft structure in composite material that comprises a skin and stringers (1), with the skin comprising a skin part (5) and a basic skin (3), and said structure further comprises U-shaped elements (15) each of which comprises in its turn two L-shaped sections (4a+5a and 4b+5b) together with the skin part (5), in such a way that these U-shaped elements (15) fulfil two structural functions in said structure at the same time, acting as frame feet and as skin, providing an integrated fuselage structure without rivets or joints. The invention also relates to a manufacturing process of an integrated aircraft structure in composite material. |
申请公布号 |
ES2352941(B1) |
申请公布日期 |
2012.01.25 |
申请号 |
ES20080001426 |
申请日期 |
2008.05.16 |
申请人 |
AIRBUS ESPANA S.L.;AIRBUS OPERATIONS, S.L. |
发明人 |
MUNOZ ROYO, PEDRO LUIS;AREVALO RODRIGUEZ, ELENA |
分类号 |
B64C1/06;B29C65/70;B64C1/12 |
主分类号 |
B64C1/06 |
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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