Research and application of analysis leads design method
-
摘要: 对产品设计过程中的大量迭代现象,从设计方法上进行了深入分析与高度总结,提出了分析驱动设计(ALD)方法,定义了设计信息(DI)、设计活动(DA)、设计模型(DM)、设计文件(DF)和分析驱动设计流程(ALDF)等基本概念.分析驱动设计方法的核心内容是分析驱动设计流程.详细阐述了分析驱动设计流程中的设计信息和设计活动;重点讲解了分析驱动设计流程的设计活动规划方法,并给出了串行化和并行化的设计活动规划的时间计算公式.基于自动化的分析驱动设计流程对产品设计方案进行验证和优化,提高了产品设计效率和设计质量,解决了分析驱动设计方法中的部分关键技术,并以航发涡轮叶片为例验证了分析驱动设计方法.Abstract: The analysis leads design(ALD) method was advanced to summarize the key concepts and analyze the essential ideas from the iterative phenomena during the product design process. The concepts of design information(DI), design activity(DA), design model(DM), design file(DF) and analysis leads design flow(ALDF) in the ALD method were defined. As self-driven design flow, ALDF was the core concept of the ALD method. The process of establishing the ALDF was the ALD method. The design information and the design activity of the ALD flow were elaborated. The serial and parallel methods to order the design activity of the ALDF were emphasized, of which the function of time cost was given. The product design plan was optimized by the ALDF to improve the design quality and efficiency. Some key techniques of the ALD method were resolved, and the ALD method was exemplified by the structure design of the turbo-jet blade. And the conditions, the self-driven design flow, the diagram of geometry variables and performance variables of the example were given.
-
Key words:
- product design /
- analysis /
- optimization /
- turbines
-
[1] 王振国,陈小前,罗文彩,等.飞行器多学科设计优化理论与应用研究[M].北京:国防工业出版社,2006:35 Wang Zhenguo, Chen Xiaoqian, Luo Wencai, et al. Research on the theory and application of multidisciplinary design optimization of flight vechicles[M]. Beijing:National Defence Industry Press,2006:35(in Chinese) [2] Pahl G, Beitz W. Engineering design[M]. London: Springer, 2001 [3] 吴立强,尹泽勇,蔡显新.航空发动机涡轮叶片的多学科设计优化[J].航空动力学报, 2005, 20 (5):795-801 Wu Liqiang, Yin Zeyong, Cai Xianxin. MDO technology applied to the aeroengine turbine blade design[J]. Journal of Aerospace Power, 2005, 20(5):795-801(in Chinese) [4] 舒彪,韩前鹏,邓家褆.基于多学科涡轮叶片气动设计优化[J].南京航空航天大学学报,2005,37(6):714-719 Shu Biao, Han Qianpeng, Deng Jiati. Aerodynamic design optimization of turbine blade based on multidiscipline[J]. Journal of Nanjing University of Aeronautics & Astronautics,2005,37(6):714-719(in Chinese) [5] 宋玉旺, 席平. 基于特征造型技术的涡轮叶片参数化设计[J]. 北京航空航天大学学报, 2004, 30(4):321-324 Song Yuwang, Xi Ping.Parametric design of turbine blades based on feature modeling[J]. Journal of Beijing University of Aeronautics and Astronautics,2004,30(4):321-324(in Chinese) [6] 宋玉旺,余伟巍,朱剑,等.变壁厚涡轮叶片参数化设计[J].计算机辅助设计与图形学报,2008,20(3):304-309 Song Yuwang, Yu Weiwei, Zhu Jian, et al. Parametric design of turbo-jet blades with unequal thickness[J]. Journal of Computer-Aided Design & Computer Graphics, 2008,20(3):304-309(in Chinese)
点击查看大图
计量
- 文章访问数: 2646
- HTML全文浏览量: 49
- PDF下载量: 877
- 被引次数: 0