Structural intermediate casing for e.g. turbojet of aircraft, has set of non-structural rectifiers arranged interdependent of hub, where non-structural rectifiers are fixed in removable manner by its ends internally at internal ring

摘要

The casing (120) has a hub (136) surrounded by an internal coaxial ring (138) and an external coaxial ring (140), where a set of radial arms (142) extends between the rings. A set of structural rectifiers (144) crosses the internal coaxial ring, where the rectifiers are fixed by its ends internal to the hub. A set of non-structural rectifiers (144') is arranged interdependent of the hub, where the non-structural rectifiers are fixed in a removable manner by its ends internally at the internal ring.