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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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