发明名称 SPLICE ASSEMBLY FOR JOINING STRUCTURAL COMPONENTS
摘要 A splice assembly may include a first splice bracket including first longitudinal axis, a first connecting member, and a first mating member extending from the first connecting member along the first longitudinal axis, the first mating member including a first mating surface disposed as a non-zero first angle relative to the first longitudinal axis. The disclosed slice assembly may further include a second splice bracket including second longitudinal axis, a second connecting member, and a second mating member extending from the second connecting member along the second longitudinal axis, the second mating member including a second mating surface disposed as a non-zero second angle relative to the second longitudinal axis. The first mating surface and the second mating surface are complementary. Surface contact between the first mating surface and the second mating surface defines a fastening location for connecting the first splice bracket and the second splice bracket.
申请公布号 CA2904562(A1) 申请公布日期 2016.06.02
申请号 CA20152904562 申请日期 2015.09.16
申请人 THE BOEING COMPANY 发明人 REEVES, ANDREW C.
分类号 B64C1/06;B64C1/12;B64C3/18;B64F5/00 主分类号 B64C1/06
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