Some researches on the current multi-disciplinary collaborative design process of domestic compressor of aeroengine are done, and the optimized work breakdown structure based on the concept of maturity is put forward after analyzing primary one. The concept of design maturity, the key elements of maturity model as well as work breakdown structure based on maturity are introduced, eventually testification is done on Teamcenter platform.%航空发动机工作分解结构一直是型号研制的重要依据.通过研究国内中小航空发动机压气机组件现行多学科协同设计过程,在对原来的工作分解结构进行分析后,提出基于成熟度的优化工作分解结构.使得航空发动机压气机组件的协同设计过程效率得到了提高,并在Teamcenter平台系统中进行了实例验证.
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