发明名称 |
複合材航空機の広範囲修理 |
摘要 |
A randomly damaged area of a one-piece composite component of an aircraft is repaired according to a method herein. The damaged area covers skin and underlying stiffening substructure of the component. The method includes generating a design of a customized composite replacement panel for replacing the damaged area. The design includes replacement skin and underlying co-cured replacement stiffening substructure. The method further includes fabricating the composite replacement panel according to the design. |
申请公布号 |
JP6068838(B2) |
申请公布日期 |
2017.01.25 |
申请号 |
JP20120133353 |
申请日期 |
2012.06.13 |
申请人 |
ザ・ボーイング・カンパニーThe Boeing Company |
发明人 |
ミラー, ジェフリー エル.;スペンサー, スコット エム.;オークス, ゲーリー ディー.;ドステルト, ステファン ジェイ. |
分类号 |
B64F5/00;B29C73/04;B64C1/00 |
主分类号 |
B64F5/00 |
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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