Device for assembly of a shroud placed between an aircraft...

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 1/16 (2006.01) B64D 29/06 (2006.01) F02C 7/20 (2006.01)

Patent

CA 2485435

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).

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