There are lots of problems in Testing Table for aircraft wheel brake, such as the huge equipment space, the low efficiency and heavy workload in adjusting the attitude of aircraft wheel, in order to deal with them, the structure is designed with a servo cylinder driving the friction plate, following a bearing and wheel rotational driven. By using the structure, the angle of the yaw could be automatically adjusted. Also the structure was designed which taking hydraulic brake to release and clamp friction plate, and the base back end was designed to rotate around front pivot in horizontal plane by step. By using the structure, the angle of the lean could be simulated, with considering of rational position of the pivot and structure. Through force analysis, strength and calculation check, the design is perfected. The improved equipment represents an upgrade of the Testing Table for aircraft wheel.