The invention relates to a slat tilting detection device of an aircraft
high lift system. The slat tilting detection device comprises a slat tilting detection sensor and a
steel rope, wherein the
steel rope sequentially penetrates through a plurality of parallel slats, one end of the
steel rope is fixedly connected with the outermost slat, and the other end of the steel
rope is fixedly connected with the innermost slat through the slat tilting detection sensor; the slat tilting detection sensor comprises a fixed support seat, a step cylinder, a sleeve cylinder, a
piston, a target and a probe, the fixed support seat is fixedly arranged on the corresponding slat, the step cylinder is fixedly arranged on the fixed support seat, the sleeve cylinder and the
piston are sequentially sheathed into the step cylinder, the target is fixedly arranged at the sealing end of the sleeve cylinder, and the probe is fixedly arranged on the fixed support seat corresponding to the target; the probe and the target form a
proximity sensor, and the output end of the probe is used as the output end of the slat tilting detection
detector; a sleeve cylinder spring is sheathed on the exterior of the sleeve cylinder; one end of the sleeve cylinder spring is connected with the sleeve cylinder, and the other end of the sleeve cylinder spring is connected with a spring clamping boss; a pre-tightening
piston spring is sheathed on the part, extending into the sleeve cylinder, of the piston; one end of the piston spring is connected with the piston, and the other end of the piston spring is connected with the sleeve cylinder; the extending end of the piston is connected with the steel
rope.