The invention discloses a deformation parameter testing test bench for a deformation wing. According to the test bench, a digital infrared distance measurement sensor is utilized for non-contact distance measurement, the displacement values of different positions of the deformation wing are measured and input into a computer, and software is utilized for interpolation to obtain a deformation curveof the test wing; a workpiece is not in contact in the measurement process, and the surface of the workpiece cannot be scratched. Driving force for driving the deformation of the wing is measured bya micro force sensor, an inflatable airbag is utilized for loading aerodynamic load on the deformation wing, feedback is given to a controller, a closed-loop adjusting system is formed to control theapplication of the aerodynamic load, the application process of the aerodynamic load is effectively simulated, and distributed loading is achieved. The test bench is simple in layout structure, shortin measurement time, convenient to operate, assemble, disassemble, detect and maintain and low in cost. By means of the test bench, the measurement time can be effectively shortened, and the measurement efficiency is improved; the test bench has good applicability to tests of small and medium deformation wings.