Ball-and-socket joint member

An end fitting for a flight control linkage for an aircraft, comprising a ball-and socket joint member, comprising:

• an inner ring, of a general shape of revolution around a first rotation axis, comprising an outer surface provided with an inner raceway,
• an outer ring, of a general shape of revolution around a second rotation axis, concentrically disposed around the inner ring and comprising an inner surface provided with an outer raceway,
• at least one row of balls aligned circumferentially, extending radially between the inner raceway and the outer raceway,
• wherein:
• the inner surface of the outer ring comprises, for each row of balls, a corresponding annular groove of a shape complementary to that of the balls of a respective row, said grooves collectively forming the outer raceway,
• at least one of the inner and outer rings is made of stainless steel with a hardness lower than 58 HRC, and
• the end fitting comprises a rod, integral with the outer ring, and a shaft integral with the inner ring, and wherein the inner ring comprises:
• a sleeve of a general shape of revolution around the first axis,
• an element in the shape of a sphere truncated at the first and second ends thereof, centrally disposed on and integral with the sleeve, the outer surface thereof forming the inner raceway of the inner ring, and
• first and second annular abutment elements, each stamped on the sleeve at a respective first or second axial side of the spherical element, having an outer radial dimension that is greater than or equal to an outer radial dimension of the spherical element at its first or second end, the first and second annular abutment elements forming abutments that oppose the movement of the inner ring when the outer ring is displaced in rotation around any swivel axis perpendicular to the first or second axes, and
• the end fitting for a control linkage comprises first and second gaskets, each arranged on a respective first or second outer axial side of the rows of balls in a longitudinal direction defined by the second axis, and extending radially between the inner ring and the outer ring, each gasket having a general annular shape, having an outer edge integral with the inner surface of the outer ring, and an inner edge forming a lip in contact with the first or second abutment element, respectively.