Riveting method for anti-collision pressing strip of front avionics composite cabin door of airplane

The invention discloses a riveting method for an anti-collision pressing strip of a front avionic composite cabin door of an airplane, and belongs to the technical field of riveting. The method comprises the steps that A, the rivet (1) sequentially penetrates through the composite cabin door (4), the rubber anti-collision strip (3) and the pressing strip (2); b, a riveting auxiliary block (5) is arranged at the penetrating end of the rivet (1) in a sleeving mode; c, a rivet (1) penetrates into the end part through a riveting machine and is fixed with the pressing strip (2); and D, the riveting auxiliary block (5) and the rubber fixing piece (6) are dismantled. According to the method, the pre-pressure on the pressing strip (2) around the rivet (1) during riveting is increased through the riveting auxiliary block (5), and deviation of the rivet (1) caused by sinking of the pressing strip around the rivet (1) is prevented. The problems that a pressing strip (2) around a rivet (1) sinks due to direct riveting in