发明名称 |
AIRCRAFT CABIN FLOOR STRUCTURE, SYSTEM, AND METHOD |
摘要 |
<p><P>PROBLEM TO BE SOLVED: To provide an integrally structured aircraft cabin flooring. <P>SOLUTION: The integrated aircraft cabin flooring structure includes a longitudinally separated series of transverse bridges having an upper doubler flange which defines latitudinally separated upper openings and a latitudinally separated series of beams which include an upper flange and a pair of separated suspending web flanges received within respective upper opening of transverse bridges. The upper flanges and web flanges of the beams may thus be connected to the transverse bridges in a load-supporting aircraft flooring system and structure as a representative of the integrated aircraft cabin flooring structure. The relevant method is also disclosed. <P>COPYRIGHT: (C)2010,JPO&INPIT</p> |
申请公布号 |
JP2010137845(A) |
申请公布日期 |
2010.06.24 |
申请号 |
JP20090246639 |
申请日期 |
2009.10.27 |
申请人 |
EMBRAER-EMPRESA BRASILEIRA DE AERONAUTICA SA |
发明人 |
OSORIO SILVIO LUIZ FRANCISCO;SCHAAY ERICH ROBERT;ARANTES MARCOS DRESSIER |
分类号 |
B64C1/18 |
主分类号 |
B64C1/18 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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