The application discloses a kind of progressive forming device, process and
process design method of engine boss component, belong to
aerospace equipment technical field, the progressive forming process of engine boss component includes the following steps: S1.to high-temperature
alloy material is preheated;S2.high-temperature
alloy strip after preheating is handled by progressive die, and the boss component is prepared.The process method disclosed in the application effectively solves the problems existing in the traditional
processing method by the continuity of production and high-speed production
rhythm of progressive die, combined with material
heating temperature control system.The process method has the advantages of improving production efficiency, reducing cost, improving product precision and consistency, and reducing deformation risk, etc., and can realize high-quality, high-efficiency boss product production.