发明名称 |
BONDED COMPOSITE AIRFOIL AND FABRICATION METHOD |
摘要 |
An airfoil includes at least one precured composite spar having a web and at least one flange integrated with an end of the web. A precured composite skin is attached to the spar by adhesive bonding the skin to the flange. |
申请公布号 |
CA2808770(A1) |
申请公布日期 |
2013.11.30 |
申请号 |
CA20132808770 |
申请日期 |
2013.03.07 |
申请人 |
THE BOEING COMPANY |
发明人 |
NORDMAN, PAUL STANLEY |
分类号 |
B64C3/26;B64C1/12;B64C3/28;B64F5/00;F16B11/00 |
主分类号 |
B64C3/26 |
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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