Station balance design method of aero-engine general assembly pulse assembly line
An aero-engine and design method technology, which is applied in the directions of design optimization/simulation, calculation, calculation model, etc., can solve the problems of complex arrangement of assembly operations in the station, difficulty in balancing the total load of the station operation, and complex station design, etc. The effect of reducing manual calculation work, shortening design time, and strong practicability
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[0069] The technical scheme of the present invention will be described in further detail below in conjunction with accompanying drawing and embodiment:
[0070] See attached figure 1 As shown, the steps of the site balance design method for this kind of aero-engine final assembly pulsating assembly line are as follows:
[0071] Step 1. Input the station balance process conditions of the final assembly pulsating assembly line, which is used to construct the assembly operation priority map, the man-hours of the structured assembly process and the number of people required for assembly, and form the optimal objective function, that is, the maximum beat minimization and the standard deviation of the station operation time Minimize; include:
[0072] 1.1 Construction of the assembly operation priority map, which is used to read the problem input file composed of the serial number of the single operation, the name of the single operation, the time consumption of the single operatio...
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