The present application relates to the technical field of equipment life cycle management, and specifically includes an
aviation equipment
full life cycle management method and
system based on digital threads, the method comprising: acquiring process parameters of each stage, determining first digital thread
master data and a first layer of associated test sequences, second digital thread
master data and a second layer of associated test sequences, mapping the deviation of the physical
equipment state and the virtual
simulation state, and identifying the performance difference point under the cross-stage
data correlation link; setting a
management strategy for collaborative optimization. The technical problem of being unable to identify the cross-stage performance difference point equipment performance fluctuation
root cause positioning in real time, causing the reliability of
aviation equipment to be limited is solved, the first and second digital thread
master data and the associated test sequences are constructed, the deviation of the physical equipment and the virtual
simulation state is accurately mapped, the
management strategy is set in combination with the double thread data and the performance difference point, and
full life cycle collaborative optimization is performed, and the technical effect of effectively improving the equipment reliability is achieved.