发明名称 Composite anti-crash structure with lateral restraint for aircraft
摘要 <p>The structure has hollow profiles (51) extending remotely and with respect to a shroud (19). The profiles are fixed to a flange (54) or a wall (18H) and are arranged to serve as a support to a upper part of a beam (18V), where the upper part is separated from the shroud following the rupture of the beam. A bend wall (92) delimiting a fuel tank is supported against the beam and transmits a lateral thrust to the beam.</p>
申请公布号 EP1813527(B1) 申请公布日期 2008.08.06
申请号 EP20070001792 申请日期 2007.01.26
申请人 EUROCOPTER 发明人 PAYEN, HERVE
分类号 B64C1/00;B29D99/00;B64C27/04 主分类号 B64C1/00
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