Positioning equipment for integral cementing of composite material fuselage wall plate stringer

The utility model discloses a positioning device for integral glue joint of a composite material fuselage wall plate stringer, which comprises a structural frame, the structural frame comprises a rotary assembly and a frame assembly arranged along the longitudinal axis of the rotary assembly, the rotary assembly comprises a shaft and discs arranged at the two ends of the shaft, and the frame assembly is arranged on the shaft. The frame assembly comprises a plurality of hollowed-out plates arranged perpendicular to the shaft of the rotary assembly, and the hollowed-out plates comprise openings used for containing the shaft of the rotary assembly and bent edges formed to be consistent with the curvature of the composite material fuselage wall plates; and the hot pressing device is arranged on the bent edges of the multiple hollow plates and comprises pressurizing, heating and positioning modules distributed in the length direction of the stringer, and each pressurizing, heating and positioning module comprises