发明名称 CIRCUMFERENCE SPLICE FOR JOINING SHELL STRUCTURES
摘要 A splice comprises a strap to bridge a first panel and a second panel, the strap comprising a top surface, a bottom surface, a first side, and a second side opposite the first side. The top surface defines a flat middle region, a flat first tapered region extending from proximate the middle region to proximate the first side, and a flat second tapered region extending from the middle region to proximate the second side. A first fitting is associated with the first stringer, the first fitting comprising a first tapered section contacting at least a portion of the first tapered region of the strap and extending from proximate the middle region to proximate the first side of the strap and a first flat section extending beyond the first side of the strap. A second fitting is associated with the second stringer, the second fitting comprising a second tapered section contacting at least a portion of the second tapered region of the strap and extending from proximate the middle region to proximate the second side of the strap and a second flat section extending beyond the second side of the strap, wherein the first fitting and the second fitting are spaced apart by the middle region of the strap.
申请公布号 CA2828723(C) 申请公布日期 2016.11.22
申请号 CA20132828723 申请日期 2013.10.01
申请人 THE BOEING COMPANY 发明人 DIEP, PAUL;DOPKER, BERNHARD
分类号 B64C1/00;F16B5/00 主分类号 B64C1/00
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