An aero-engine part marking device comprises a marking device body, a part moving tool, a guide rail and a
workbench, and the marking device body is arranged on the
workbench; the part moving tool and the
workbench are arranged adjacently, and a guide rail is arranged in a matched mode and used for guiding the part moving tool to be close to the workbench. The guiding track limits the
butt joint track of the part moving tool, and the part moving tool is in
butt joint with the positioning part B of the workbench through the positioning part A, so that the working area of the marking device falls on a part fixed to a rotary disc of the part moving tool. The marking device comprises a controller, a marking device body, a marking supporting rack and a
cantilever. A marking pen of the marking device body is arranged towards a rotary disc of the part moving tool. The marking supporting rack is fixed to the workbench, the
cantilever is arranged on the marking supporting rack and can rotate relative to the marking supporting rack, the marking device is arranged on the
cantilever, and the position of the marking device on the cantilever is adjustable.