发明名称 Lifting structure for aircraft
摘要 It is essentially applicable to a horizontal stabilizer that includes two side symmetrical boxes that converge at one end (its root) thereof in a shared center area in order to connect integrally in said central area. It is characterized in that both boxes connect by means of a single part that constitutes a center rib with a double T-shaped profile. The root of the side boxes overlap converging on the inside surfaces of the wings of the center rib. The connection is ensured with rivets (lap joint). The proposed connecting means simplifies the assembly process (single part) and lead to a weight reduction since that a carbon fiber connecting rib can be used.
申请公布号 US2009159742(A1) 申请公布日期 2009.06.25
申请号 US20080073770 申请日期 2008.03.10
申请人 RAMIREZ BLANCO GONZALO;BARROSO VLOEDGRAVEN DANIEL;LOZANO GARCIA JOSE LUIS;LUQUE BUZO MIGUEL 发明人 RAMIREZ BLANCO GONZALO;BARROSO VLOEDGRAVEN DANIEL;LOZANO GARCIA JOSE LUIS;LUQUE BUZO MIGUEL
分类号 B64C5/02;B64C3/20 主分类号 B64C5/02
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