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从系统动力学的角度描述了航空发动机研发机构内部的知识转移过程,分析了知识转移的因果关系,建立了知识转移的SD模型,利用Vensim软件功能对系统进行了仿真和灵敏度分析。通过该方法建立的仿真模型能较好地模拟航空发动机研发机构内部知识的转移过程;健全的设计体系能有效地提高航空发动机R&D知识转移量和研发机构内部平均知识总量,进而促进航空发动机R&D核心能力加快提升。
From the perspective of system dynamics, the internal knowledge transfer process of aeroengine R&D institutions is described. The causality of knowledge transfer is analyzed. An SD model of knowledge transfer is established. The simulation and sensitivity analysis of the system are performed using Vensim software functions. The simulation model established by this method can better simulate the internal knowledge transfer process of the aeroengine R&D organization; a sound design system can effectively increase the transfer of knowledge of R&D knowledge of aeroengine and the average total internal knowledge of the R&D organization, thereby promoting aeroengine R&D. The core capabilities have been accelerated.