发明名称 |
Aircraft fuselage frame with tapered section |
摘要 |
The structural frame element (1) has the general form of an elongated profile, comprising a web (2) and at least one flange (4,6). The flange has an arc-shaped cross-section over the length of the profile apart from on at least one end portion (46) of the profile in which the cross-section varies so as to have a straight cross-section perpendicular to the web. |
申请公布号 |
EP2692631(A1) |
申请公布日期 |
2014.02.05 |
申请号 |
EP20130177850 |
申请日期 |
2013.07.24 |
申请人 |
AIRBUS OPERATIONS |
发明人 |
CAZENEUVE, HÉLÈNE;MONTEILLET, FABRICE;MARCHIPONT, YANN |
分类号 |
B64C1/06 |
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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