The invention relates to the technical field of
aviation conduit fatigue tests, and provides an
aviation conduit rotation bending test flexural disc, which is provided with a self-aligning bearing, a basic disc and a bearing seat, a joint at one end of an
aviation conduit is inserted into an inner hole of the self-aligning bearing, and a joint at the other end of the aviation conduit is mounted on an aviation conduit rotation
bending fatigue test mounting device. The aviation conduit rotation
bending fatigue test installation device is installed on a
workbench, a basic disc is fixedly installed at one end of a rotating shaft through an installation hole, the rotating shaft is connected with a synchronous belt, the synchronous belt is connected with a motor, the motor is arranged in a
headstock, the
headstock is installed on the
workbench, and a bearing seat is assembled with the outer
diameter of a self-aligning bearing. The bearing seat is arranged on one side of the basic disc in a position-adjustable mode and can move relative to the basic disc to generate eccentricity during position adjustment, so that the aviation conduit is subjected to
bending force, and the reasonability, reliability and safety of the flexure disc structure are improved.