The invention discloses a test
bed and a test method for fatigue life of a steel cable of an aircraft
control system, in the test
bed, a first hollow guide rail 2a for mounting a test
pulley 8 is arranged at the upper part of a mounting bottom plate 3 of a support frame along a longitudinal center line, and two second hollow guide rails 2b for the second hollow guide rails 2b are symmetrically arranged along a transverse center line; a driving
pulley in the driving
control system is mounted at the bottom of the longitudinal center line of the mounting bottom plate 3; after the test steel cable 1 bypasses the test
pulley 8 and the two auxiliary pulleys 13, the two ends of the test steel cable 1 are respectively connected with the two ends of the driving steel cable 11 wound on the driving pulley 12 through one tension
regulator 10 to form a steel cable loop, and the driving steel cable 11 is fixedly connected with the driving pulley 12; the test
bed adjusts the pulley wrap angle of the test steel cable 1 wound on the test pulley 8 through the mounting positions of the two auxiliary pulleys 13 and the test pulley 8 on the mounting bottom plate 3, and drives the test steel cable 1 to reciprocate around the test pulley 8 through the driving of the driving
control system to the driving pulley 12, so as to perform a fatigue
life test on the steel cable test piece. According to the technical scheme provided by the invention, the problems that the fatigue life of the steel cable under various working conditions needs to be obtained through a test mode due to the fact that the existing fatigue
life test of the steel cable in the soft control
system relates to the steel cable under various working conditions, the test
workload is huge, and the cost input is relatively large are solved.