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 US2008105785(A1) 申请公布日期 2008.05.08
申请号 US20060555829 申请日期 2006.11.02
申请人 发明人 GRIESS KENNETH H.;GEORGESON GARY E.
分类号 B64C1/00 主分类号 B64C1/00
代理机构 代理人
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