发明名称 Connector for connecting fuselage to aerofoil of aircraft, has aerofoil upper skin panel for sealing rib, where rib extends above panel and is joined with fuselage in upper line higher than junction line between panel and rib
摘要 <p>The connector has an aerofoil rib (13) for prolonging a fuselage (2), and an aerofoil upper skin panel (3) for sealing the rib. The rib extends above the aerofoil panel, and is joined with the fuselage in an upper line (14) higher than a junction line (15) between the panel and the rib. The upper line extends to a neutral bending line of an aircraft in a vertical plane. The upper line belongs to another junction line of two horizontal panel bands of fuselage, where the fuselage is made of a composite material.</p>
申请公布号 FR2972997(A1) 申请公布日期 2012.09.28
申请号 FR20110052493 申请日期 2011.03.25
申请人 AIRBUS OPERATIONS 发明人 GUITTARD DOMINIQUE;EVE OLIVIER;FORT FREDERIC;COLMAGRO JEROME;LOYANT FRANCOIS
分类号 B64C1/26 主分类号 B64C1/26
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