发明名称 SYSTEM AND METHOD OF JOINING COMPONENTS
摘要 PROBLEM TO BE SOLVED: To provide a system and method for joining composite components which accommodates variations in contours of mating surfaces of the composite components while minimizing bondline thickness.SOLUTION: A method of forming a structural assembly may include providing a first component 300 and a second component 400 to be joined together. The method may additionally include scanning a contour of a first mating surface of the first component and scanning a contour of a second mating surface of the second component. The method may further include producing a thermoplastic element including a thermoplastic radius filler 512, having a first element surface 514 and a second element surface which oppose each other and substantially match the contour of the first mating surface and the contour the second mating surface.
申请公布号 JP2015120335(A) 申请公布日期 2015.07.02
申请号 JP20140226750 申请日期 2014.11.07
申请人 BOEING CO 发明人 PREBIL CHARLES R;FOX JAMES R
分类号 B29C65/40;B64C1/00;B64C1/12;B64F5/00;C09J5/00;C09J5/06;C09J7/00;C09J7/02;C09J201/00 主分类号 B29C65/40
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