ATTACHE DE SIEGE D'AERONEF MUNI D'UNE LIAISON HELICOIDALE DE SERRAGE

摘要

The invention relates to an aircraft seat fastener (20) which comprises a body (21) intended to be secured to an aircraft seat and a shank (24) provided at one of its ends with a stud (25), said body (21) and said shank (24) being connected to one another by a helicoidal connection (30) that is irreversible under axial load so that a turning of the shank (24) brought about via an operating device (34) is able to cause the stud (25) to move toward the body (21) so as to clamp a lip (2) of a rail (1) between said stud (25) and an underside (22) of said body (21).