An
airplane body wallboard pressurizing test device relates to the technical field of
airplane strength test device designing. Long bottom beams are parallely and fixedly arranged on a same plane. Short bottom beams are fixedly arranged on the long bottom beams and are perpendicular with the long bottom beams; a square
steel frame is fixed on the short bottom beams and furthermore the shape of the square
steel frame matches a supporting bottom box. Each connecting part comprises a small pulling plate, a middle pulling plate, a large pulling plate, a long pulling plate, double ears, a load
equalizer and a single ear; wherein the small pulling plate, the middle pulling plate, the large pulling plate, the long pulling plate, the double ears, the load
equalizer and the single ear are successively connected. A tested member covers and presses the supporting bottom box, and furthermore the tested member is connected with a supporting part through the connecting part. The tested member is connected with a hydraulic
servo control device and inflates the tested member for realizing a pressurizing test on the
airplane body wallboard. The airplane body wallboard pressurizing test device provided by the invention has advantages of saving testing space, reducing weight of the test device; effectively ensuring uniform
load bearing in an adaptive loading manner; reducing a connecting process, effectively increasing loading frequency, realizing uniform boundary load, saving space and realizing repeated use.