发明名称 Circumference splice for joining shell structures
摘要 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).
申请公布号 AU2013228054(B2) 申请公布日期 2016.12.22
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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