发明名称 Fuselage longeron for an aircraft and a central wing box with such a longeron
摘要 <p>The longeron has peripheral zones, a central zone (c) and a recess (5) in the central zone, where the recess has an oblong form. The peripheral zones are constituted of an upper zone (z1) near an upper skin panel, a lower zone (z2) near a lower skin panel (I), and two lateral zones (z3) near wing longerons. The peripheral zones reduce normal forces conveyed by the wing longerons. An independent claim is also included for a central wing box comprising a fuselage longeron.</p>
申请公布号 EP1571079(A1) 申请公布日期 2005.09.07
申请号 EP20050300154 申请日期 2005.03.01
申请人 AIRBUS FRANCE 发明人 SARPY, BRUNO
分类号 B64C1/06;B64C1/26;(IPC1-7):B64C1/06 主分类号 B64C1/06
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