Aircraft structure static test method, device, equipment and medium

The embodiment of the invention provides an aircraft structure static test method and device, electronic equipment and a computer storage medium, and relates to the technical field of static tests. Comprising the following steps: respectively constructing virtual three-dimensional models for a real test tool and a real loading device, and carrying out virtual installation to obtain a virtual test tool; acquiring a virtual test point marked on the virtual test tool, and synchronously installing a strain sensor at a corresponding test point position of the real test tool based on the virtual test point; adding load tests to the real test tool step by step according to a preset level based on the real loading device to obtain real test data corresponding to each level, and adding load tests to the virtual test tool step by step according to a preset level by the virtual loading device corresponding to the real loading device to obtain virtual test data corresponding to each level; and displaying the real test da