发明名称 Circumference splice for joining shell structures
摘要 <p>CIRCUMFERENCE SPLICE FOR JOINING SHELL STRUCTURES The disclosed shell structure splice (10) and method may include a first panel (1 10a) having a first edge, a second panel (1 10b) having a second edge, the second edge being positioned in edgewise alignment with the first edge to form a splice joint (106), a strap (12) bridging the splice joint (106) and attached to the first panel (1 10a) and the second panel (1 10b), the strap (12) having a first tapered region (22a)and a second tapered region (22b), a first fitting (34) having a tapered section (34) and a flat section (36), the tapered section (34) being attached to the first tapered region (22a) of the strap (12), and a second fitting (24) having a tapered section (34) and a flat section (36), the tapered section (34) being attached to the second tapered region (22b) of the strap (12).</p>
申请公布号 AU2013228054(A1) 申请公布日期 2014.05.15
申请号 AU20130228054 申请日期 2013.09.16
申请人 THE BOEING COMPANY 发明人 DIEP, PAUL;DOPKER, BERNHARD
分类号 B64C1/12;B64C1/00 主分类号 B64C1/12
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