发明名称 |
Aircraft panel |
摘要 |
An aircraft panel comprising a sandwich construction with an outer skin portion of high strength material, an inner portion of high strength material and an intermediate core material. The core material includes areas with low density core material and a reinforcement grid of high strength material, with longitudinal and transversal grid members.
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申请公布号 |
US2004155148(A1) |
申请公布日期 |
2004.08.12 |
申请号 |
US20030479800 |
申请日期 |
2003.12.05 |
申请人 |
FOLKESSON MATS;THURESSON STEFAN |
发明人 |
FOLKESSON MATS;THURESSON STEFAN |
分类号 |
B32B5/18;B32B15/20;B64C1/12;(IPC1-7):B64C1/00 |
主分类号 |
B32B5/18 |
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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