发明名称 Device for assembly of a shroud placed between an aircraft engine air intake and a pylon
摘要 The invention relates to a device ( 131 ) for assembly of a shroud ( 26 ) arranged between an air intake ( 22 ) and a pylon ( 2 ) fixed to the engine ( 4 ), the device comprising: stressed flexible means ( 130 ) provided with a first end ( 130 a) and a second end ( 130 b); first connection means connected to the air intake and to the end ( 130 a); and second connection means connected to the shroud and to the end ( 130 b). According to the invention, the second connection means comprise a primary assembly ( 140 ) fixed to the shroud and a secondary assembly ( 142 ) fixed to the second end ( 130 b), and the primary and secondary assemblies ( 140,142 ) are connected to each other through a pivot connection ( 144 ).
申请公布号 US7147185(B2) 申请公布日期 2006.12.12
申请号 US20040954192 申请日期 2004.10.01
申请人 AIRBUS FRANCE 发明人 BEAUFORT JACQUES
分类号 B64D27/00;B64D29/06 主分类号 B64D27/00
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