发明名称 STRUCTURE OF AN AIRCRAFT AEROFOIL
摘要 Aircraft aerofoil structure, in particular rear spar structure (1) for the joining of lateral box beams (2) of a horizontal stabilizer of an aircraft, said rear spar (1) comprising a right rear spar (5) and a left rear spar (6), moreover said structure of said rear spar (1) includes a central section formed by an integrated component (10), and said integrated component (10) includes fittings (11) that serve for joining said rear spar structure (1) to the aircraft fuselage and projections (12) that serve for joining the central section formed by the integrated component (10) to the right rear spar (5) and left rear spar (6).
申请公布号 US2009321575(A1) 申请公布日期 2009.12.31
申请号 US20080201310 申请日期 2008.08.29
申请人 AIRBUS ESPANA S.L. 发明人 BARROSO VLOEDGRAVEN DANIEL;RAMIREZ BLANCO GONZALO;LOZANO GARCIA JOSE LUIS;LUQUE BUZO MIGUEL
分类号 B64C1/26 主分类号 B64C1/26
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