发明名称 |
Method and system for determining and verifying ply orientation of a composite laminate |
摘要 |
A method (66) for determining and verifying ply orientation (98) of composite laminates (28) includes performing a first scan (104) of a prepared edge (92a) of a composite laminate (28) using an off-axis inclined light source (106) directing light (108) at a first acute angle (110) to a first area (112) on the prepared edge (92a) to produce a first scanned image (116); rotating an orientation (117) of the off-axis inclined light source (106) relative to the prepared edge (92a), such that the off-axis inclined light source (106) directs light at a second acute angle (130) symmetrically opposite the first acute angle (110); and performing a second scan (126) of the prepared edge (92a) using the off-axis inclined light source (106) directing light (108) at the second acute angle (130) to the first area (112) on the prepared edge (92a) to produce a second scanned image (128). The method (66) includes comparing the first and second scanned images (116, 128) to determine a ply orientation (98) of each ply (94), and verifying the ply orientation (98) against a baseline ply orientation (99). |
申请公布号 |
EP2896496(A1) |
申请公布日期 |
2015.07.22 |
申请号 |
EP20150151541 |
申请日期 |
2015.01.16 |
申请人 |
THE BOEING COMPANY |
发明人 |
GONZE, THOMAS J.;KENDALL, JAMES R.;JACKSON, DAVID C. |
分类号 |
B29C70/20;G01N21/47;G01N21/84;G01N21/898 |
主分类号 |
B29C70/20 |
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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