发明名称 FUSELAGE BUTT JOINT STRUCTURE CONNECTED TO AIRCRAFT VERTICAL FIN, AND AIRCRAFT COMPRISING FUSELAGE BUTT JOINT STRUCTURE
摘要 A fuselage butt joint structure (10) connected to an aircraft vertical fin, the fuselage butt joint structure (10) comprising: a structural main body (20) provided with a plurality of reinforcing ribs (21); and a plurality of joints (30), the joints (30) being installed back-to-back in pairs at the front side and rear side of the structural main body (20); two ends of each joint (30) are respectively provided with reinforcing ribs (31); the reinforcing ribs (31) of the joint (30) are connected to the reinforcing ribs (21) of the structural main body (20) via fasteners; and the aircraft vertical fin is installed onto the joint via fasteners. The fuselage butt joint structure of the present invention has performance against fatigue, and is easy to maintain.
申请公布号 WO2015032276(A1) 申请公布日期 2015.03.12
申请号 WO2014CN84771 申请日期 2014.08.20
申请人 COMMERCIAL AIRCRAFT CORPORATION OF CHINA, LTD;COMMERCIAL AIRCRAFT CORPORATION OF CHINA, LTD SHANGHAI AIRCRAFT DESIGN AND RESEARCH INSTITUTE 发明人 LU, BINGHE;WU, CHENGSI;LI, XIYAN;GONG, ZHANFENG;LI, PING;LUO, TENGTENG
分类号 B64C1/26 主分类号 B64C1/26
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