发明名称 STIFF PANEL FOR AIRCRAFT, COMPRISING STIFFENERS WITH NOTCHED CORES
摘要 A stiffened panel includes a panel at least one of whose surfaces is equipped with stiffeners each of which includes a base that is pressed against the surface of panel, as well as a core that is oriented orthogonally relative to the base and whose first longitudinal edge is integral to the latter. At least one of the stiffeners includes a multitude of notches that cross over a second longitudinal edge of the core opposite the first edge, so that they extend towards the outside of the stiffener.
申请公布号 US2013026292(A1) 申请公布日期 2013.01.31
申请号 US201213557390 申请日期 2012.07.25
申请人 AIRBUS OPERATIONS S.A.S.;DUBOST JEROME;LACOMBE JEAN CLAUDE 发明人 DUBOST JEROME;LACOMBE JEAN CLAUDE
分类号 B64C1/06;B32B3/08;B64C25/00 主分类号 B64C1/06
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