发明名称 Aircraft fuselage frame with tapered section
摘要 <p>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.</p>
申请公布号 EP2692631(B1) 申请公布日期 2015.05.06
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
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