Patent ID: 7147185

Claim:
Device for assembly of a shroud arranged between firstly an air intake of an aircraft engine and secondly a pylon fixed to the said engine and to a structure element of this aircraft, the said device comprising: stressed flexible means provided with a first end and a second end, said flexible means being designed to force the shroud into contact with the air intake and the engine pylon; first connection means connected firstly to one of the elements among the group composed of the pylon and the air intake, and secondly to the first end of the flexible means, these first connection means being designed such that the first end of the flexible means is fixed to said one of the elements among the group composed of the pylon and the air intake; and second connection means connected firstly to the shroud and secondly to the second end of the flexible means, characterized in that the second connection means comprise a primary assembly fixed to the shroud and a secondary assembly fixed to the second end of the flexible means, and in that the primary and secondary assemblies are connected to each other through a pivot connection.