发明名称 Rib for blended wing-body aircraft
摘要 Structural ribs for providing structural support for a structure, such as the pressure cabin of a blended-wing body aircraft. In a first embodiment, the ribs are generally "Y-shaped", being comprised of a vertical web and a pair of inclined webs attached to the vertical web to extend upwardly and outwardly from the vertical web in different directions, with only the upper edges of the inclined webs being attached to a structural element. In a second embodiment, the ribs are generally "trident-shaped", whereby the vertical web extends upwardly beyond the intersection of the inclined webs with the vertical web, with the upper edge of the vertical web as well as the upper edges of the inclined webs being attached to the same structural element.
申请公布号 US5893535(A) 申请公布日期 1999.04.13
申请号 US19970878628 申请日期 1997.06.19
申请人 MCDONNELL DOUGLAS CORPORATION 发明人 HAWLEY, ARTHUR V.
分类号 B64C3/00;B64C39/10;B64D11/00;(IPC1-7):B64C1/06 主分类号 B64C3/00
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