Composite material beam for structure of aircraft, has flange connected to plate and pressed against heel, and anchoring point connected to plate, where rib is extended between anchor point and flange

摘要

The beam has a cross section part comprising a core (42), two beads (44, 44') and a binding element (46) for connecting a beam element. The binding element comprises two portions (48) having a plate (50), where the plate is pressed and fixed to the core. A flange (52) is connected to the plate and pressed against a heel. An anchoring point (54) is connected to the plate. A rib (56) is extended between the anchor point and the flange. The portions of the binding element are placed on sides of the core.