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 (130a) and a second end (130b) ; - first connection means connected to the air intake and to the end (130a) ; and - second connection means connected to the shroud and to the end (130b). 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 (130b), and the primary and secondary assemblies (140,142) are connected to each other through a pivot connection (144).
申请公布号 CA2485435(C) 申请公布日期 2012.05.15
申请号 CA20042485435 申请日期 2004.10.19
申请人 AIRBUS FRANCE 发明人 BEAUFORT, JACQUES
分类号 B64C1/16;B64D29/06;F02C7/20 主分类号 B64C1/16
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