发明名称 |
Arrangement of a circumferential joint of structural elements with a coupling element manufactured in composite material |
摘要 |
A joint construction for an aeronautical structure made from composite material having an internal structural element and an adjoining skin element which define the aeronautical structure, which includes a coupling element disposed between and contiguous with the internal structural element and the adjoining skin element, wherein the coupling element has opposing adjoining diagonally configured end portions which form a wedge shaped diagonal joint therebetween which terminates at the internal structural element at one end and the skin element at the other end, and a plurality of rivets extending from the internal structured element to the adjoining skin, across the coupling element and across the diagonal joint.
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申请公布号 |
US8500068(B2) |
申请公布日期 |
2013.08.06 |
申请号 |
US20100876875 |
申请日期 |
2010.09.07 |
申请人 |
VILLARES ENRIQUE VERA;LOPEZ JOSE MARIA PINA;HERNANDEZ IGNACIO JORGE OUTON;AIRBUS OPERATIONS, S.L. |
发明人 |
VILLARES ENRIQUE VERA;LOPEZ JOSE MARIA PINA;HERNANDEZ IGNACIO JORGE OUTON |
分类号 |
B64C1/12 |
主分类号 |
B64C1/12 |
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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