Patent ID: 9469409
Filing Date: 2016-10-18
CPC Classification: B64C,B64D

Claim Text:
1. An aerodynamic fairing of a pylon of a turbo engine comprising: the fairing being in the form of a casing which extends along a longitudinal axis and which comprises a first lateral panel and a second lateral panel which are substantially parallel with the longitudinal axis and which are distributed at one side and the other of a plane of symmetry of the fairing, the aerodynamic fairing comprising at least two sub-assemblies which are arranged consecutively along the longitudinal axis and which are separated from each other by a gap, each sub-assembly comprising a frame which is oriented transversely relative to the longitudinal axis and a floor portion which extends along the longitudinal axis, wherein the floor portion of each sub-assembly is not directly connected to the floor portion of the adjacent sub-assembly at an inner face of the floor portions; each frame having, in a position for use, an upper edge, a lower edge which is fixed to the inner face of the floor portion of the sub-assembly, and a first lateral edge and a second lateral edge to which the first lateral panel and the second lateral panel are fixed, respectively.