Connecting rod for the structural reinforcement of a fuselage structure of an aircraft

摘要

A connecting rod for the structural reinforcement of a fuselage structure of an aircraft includes a shank and eyes arranged at the shank ends on both sides for connecting the connecting rod to the fuselage structure. The connecting rod may have a reinforcing arrangement, which is configured as an all-over casing, the casing being formed by mechanically high-strength reinforcing fibers. The casing may also be formed by reinforcing fiber strands, which for their part can include a multiplicity of discrete reinforcing fibers running parallel to one another. Carbon fibers, glass fibers, aramid fibers and high-strength ceramic fibers come into consideration in particular as reinforcing fibers.

主权项

1. A connecting rod for the structural reinforcement of a fuselage structure of an aircraft, the connecting rod comprising
a shank and eyes arranged at shank ends on both sides for connecting the connecting rod to the fuselage structure, wherein on at least one shank end an eye can be screwed on for length compensation; and a reinforcing arrangement enclosing at least in certain regions both eyes, the shank and the shank ends, wherein the eyes are connected by the reinforcing arrangement which is formed by a multiplicity of reinforcing fibers, and both eyes have a peripheral groove with a concave cross-sectional geometry for a precise lateral guidance of the reinforcing arrangement in the region of the eyes, wherein the reinforcing arrangement is formed as a casing which encloses at least in certain regions both eyes and the shank as well as the shank ends, and wherein the casing is under mechanical prestress to be able to immediately absorb tensile loads without prior stretching to ensure an adequate mechanical load-bearing capacity of the connecting rod in an accident situation.