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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

Pending Publication Date: 2022-04-15
CHINA AVIATION PLANNING & DESIGN INST GRP
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  • Abstract
  • Description
  • Claims
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Problems solved by technology

[0031] The present invention is designed to provide a station balance design method for the pulsating assembly line of the general assembly of the aero-engine just aiming at the above-mentioned existing technical conditions. The manual calculation is very complicated and the total load balance of the station operation is difficult, especially the hardware facilities have been installed in place, and the assembly process needs to be distributed to each station, so as to reduce the complexity of the station balance design of the aero-engine pulse mobile assembly production line, Intelligently achieve the optimal assignment of each assembly station operation, and at the same time balance the total operation time of each station to maximize production efficiency

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  • Station balance design method of aero-engine general assembly pulse assembly line
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  • Station balance design method of aero-engine general assembly pulse assembly line

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Embodiment Construction

[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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Abstract

The invention relates to a position balance design method for an aero-engine final assembly pulsation assembly line, which comprises the following six steps of: inputting a balance process condition of the aero-engine final assembly pulsation assembly line, setting and verifying an operation arrangement rule, encoding a particle swarm, decoding the particle swarm, dynamically constructing a directed acyclic network diagram module, and carrying out reverse differential evolution on the particle swarm. Through a mutation operator, a crossover operator, a selection operator and a reverse transition operator, in combination with population evolution state monitoring and disturbance application, the particle swarm is iteratively evolved in a high-dimensional solution space, and an optimal solution is finally found. According to the method, the design complexity of the aero-engine pulse movement assembly production line is reduced, optimal operation distribution of all the assembly stations is intelligently achieved, the method adapts to the situation that parallel operation and procedures in the stations have constraints on the distributed stations, meanwhile, the maximum takt of operation of all the stations is minimized, total duration balance is considered, and the production efficiency is maximized.

Description

technical field [0001] The invention relates to a station position balance design method of an aero-engine general assembly pulsation assembly line, which belongs to the technical field of design of an aero-engine general assembly production line. Background technique [0002] There are various types of assembly lines, which can be divided into continuous mobile type and pulse mobile type according to the continuous degree of production process. In the continuous mobile upper assembly line, the product is continuously carried out between the processes from input to output, without waiting and interval time. Assembly lines are generally used for mass production and are a relatively complete form of organization. The necessary condition for organizing a continuous assembly line is that the process is mature and stable, and the processing time of all processes is equal to the takt time or an integer multiple of the takt time, so the production organization is difficult; Equal...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F30/27G06F30/25G06N3/00G06F111/04
Inventor 张超李慧
Owner CHINA AVIATION PLANNING & DESIGN INST GRP