Jet deflection module for a thrust reverser of an aircraft turbine engine

Abstract

A jet deflection module for a thrust reverser of an aircraft turbine engine, this module extending in a surface and including longitudinal members which are spaced apart from one another and parallel to one another; at least one deflection element which extends between the longitudinal members and which is connected to these longitudinal members; and two attachment profiles, front and rear, respectively, which are connected to the longitudinal members, these two profiles forming, with two of these longitudinal members, a peripheral contour of the module, wherein a first of the attachment profiles includes a plurality of hooks at a distance from one another, each of these hooks including at least one opening oriented perpendicularly to the surface and additionally a bearing surface parallel to this surface.

Dependencies are inferred from the claim text.