FIELD: aerospace technology.
SUBSTANCE: invention is related to a rod end. The rod end includes a bearing that is at least partially enclosed within the component. The component extends at least partially as a loop around the bearing. The component includes a first plastic, which is a fibre-reinforced first plastic. The fibre-reinforced first plastic, which forms a loop around the bearing, extends at least partially into the threaded rod. The fibres in the fibre-reinforced first plastic correspond to the thread profile at the surface of the threaded rod. The component may be made of a continuous fibre-reinforced composite material (3) with a thermoplastic matrix and at the same time reinforced with continuous fibres. The thermoplastic matrix composite material may extend into the threaded rod (2) of the rod end. A component made from a continuous fibre-reinforced thermoplastic matrix composite material may be embedded in a short fibre-reinforced, long fibre-reinforced, or unreinforced thermoplastic (5).
EFFECT: increase in mass-strength characteristics is achieved.
23 cl, 8 dwg
