发明名称 Optimized fuselage structure
摘要 A fuselage structure including an upper fuselage portion defined by a first cross-section including at least three different radii of curvature. The fuselage structure may also include a lower fuselage portion defined by a second cross-section including at least three different radii of curvature, wherein the first cross-section is different from the second cross-section.
申请公布号 GB0721312(D0) 申请公布日期 2007.12.12
申请号 GB20070021312 申请日期 2007.10.30
申请人 BOEING COMPANY, THE 发明人
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