发明名称 Splicing Fuselage Sections without Shims
摘要 Fuselage sections of an aircraft are joined using splice elements that compensate for gaps caused by mismatches between mating surfaces on the fuselage sections. The fuselage sections are virtually assembled using computer models that are based on non-contact measurements of as-built fuselage sections. The virtually assembled fuselage sections are used to map the gaps between the mating surfaces. The mapped gaps are used to produce tool inserts having profiles that reflect the dimensions of the gaps. The tool inserts are used to manufacture splice elements having profiles that fill the gaps when the fuselage sections are assembled and joined, thereby eliminating the need for shims and spaces to fill the gaps.
申请公布号 US2008223985(A1) 申请公布日期 2008.09.18
申请号 US20070685934 申请日期 2007.03.14
申请人 THE BOEING COMPANY 发明人 MARSH BOBBY J.;VANSCOTTER KINSON D.;MALEN-HOGLE KAREN
分类号 B64C1/00;B23P19/00;B41J2/01;G06F17/50 主分类号 B64C1/00
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