基于dsm的复杂航空航天项目开发流程设计与优化

Weitao Xiong, Cang Liu, Qingsong Zhao, Ke-Wei Yang
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引用次数: 1

摘要

随着航空航天工程规模和复杂程度的不断提高,如何缩短航空部件的研制时间已成为一个亟待解决的问题。本文主要研究航空航天项目复杂产品开发过程规划(CPDPP)中的技术需求。复杂航空部件设计的难点不仅在于任务数量庞大,还在于任务之间的耦合迭代。迭代是一个有点消极的词,因为它意味着重新做工作,并且在整个开发过程中通常需要很长时间才能收敛。在以往研究的支持下,本文明确了构建设计结构矩阵(DSM)的步骤,并提出了重叠迭代和顺序迭代的处理方法,使设计师能够将从不同角度建立的所有DSM进行整合,从整体上理解产品的设计结构。并在相关分析的基础上提出了一种新的需求侧需求解耦方法,该方法采用由灵敏度和可变性组成的指标体系进行评价。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
DSM-based complex aerospace projects development process design and optimization
With the scale and complexity of aerospace projects raising, how to shorten the development time of aero-components has become an emergent problem. In this paper, we focus on the technical needs in Complex Product Development Process Planning (CPDPP) for aerospace projects. The difficulties of designing a complex aero-component result not only from masses of tasks, but also from iterations between coupled tasks. Iteration is a somewhat negative word since it implies re-doing work and often takes a long time to converge during a whole development process. Under the support of researches in the past, this paper specifies the steps of constructing Design structure matrix (DSM) and proposes a method of handling overlapping iteration and sequential iteration, which makes designers integrate all DSMs established from different views and understand products design structure on the whole. Furthermore it proposes a new decoupling method of DSM based on relevant analyses which is evaluated by an index system consisted of sensitivity and changeability.
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