METAL ANNULAR CONNECTING STRUCTURE FOR AN AIRCRAFT TURBINE ENGINE

摘要

The invention relates to a metal annular structure (50) for connecting two aircraft turbine engine parts, said structure having, within any half-section, two primary arms and a base (62), forming a first U (64) radially opening relative to a longitudinal axis (4), said structure moreover having two secondary arms forming, with one of the two primary arms, a longitudinally opening second U (68). According to the invention, the primary and secondary branches, as well as the base (62) of the first U, are created from a single part.