Propeller design rule extraction based on rough set theory
-
摘要:
不同于由专家通过理论推导或经验得到设计规则的传统方法,提出了数据驱动的螺旋桨设计规则提取方法。使用粗糙集理论对螺旋桨优化设计过程中产生的大量方案数据进行分析,发展了适当的属性表示方法和属性离散方法。结果表明:在对两类不同参数螺旋桨型号的研究中,均提取出了“当各剖面诱导速度的差异越小时,螺旋桨效率越高”的设计规则,这一规则与Betz条件相当,验证了方法的有效性。基于数据驱动的螺旋桨设计规则提取方法可为后续三维设计规则的发现和优化设计研究提供技术支持,该思想也可供其他设计领域参考。
Abstract:Different from the traditional method of obtaining design rules by experts through theoretical derivation or experience, a data-driven propeller design rule extraction method was proposed. The rough set theory was used to analyze a large number of scheme data generated in the process of propeller optimization design. An appropriate attribute representation method and an attribute discrete method were developed. Result showed that, in the study of two types of propeller models with different parameters, the design rule that the smaller the difference of the induced velocity of each section of the propeller, the higher the propeller efficiency was extracted. This rule was equivalent to the Betz condition, which verified the effectiveness of the method. The data-driven propeller design rule extraction method can provide technical support for the subsequent discovery of three dimensional design rules and optimal design research. This idea can also be used as a reference for other design fields.
-
Key words:
- rule extraction /
- propeller design /
- data driven /
- rough set theory /
- Betz condition
-
表 1 螺旋桨主要参数
Table 1. Main parameters of propellers
参数 桨Ⅰ 桨Ⅱ 叶数 4 2 直径/mm 1200 2600 转速/(r/min) 2263 450 速度/(m/s) 55.5 18.5 高度/km 10 12 表 2 原始决策信息表
Table 2. Original decision information table
论域编号 分散程度(条件属性) 效率(决策属性) 1 0.108 0.7922 2 0.150 0.7904 3 0.123 0.7908 4 0.154 0.7891 5 0.289 0.7756 6 0.341 0.7734 7 0.306 0.7712 8 0.205 0.7877 9 0.280 0.7750 10 0.329 0.7728 11 0.412 0.7685 12 0.404 0.7673 13 0.093 0.7870 14 0.098 0.7858 15 0.131 0.7841 16 0.279 0.7698 17 0.156 0.7844 18 0.155 0.7828 19 0.260 0.7694 20 0.307 0.7673 21 0.353 0.7638 22 0.063 0.7768 23 0.082 0.7809 24 0.113 0.7797 25 0.122 0.7782 26 0.252 0.7639 表 3 离散结果中的不相容
Table 3. Incompatibility in discrete results
分散程度水平值 效率水平值 1 2 2 1 2 2 表 4 离散后的决策信息表
Table 4. Discrete decision information table
论域编号 离散后的条件属性 决策属性 分散程度水平值 随机数 效率水平值 1 1 20 2 2 1 21 2 3 1 3 2 4 1 26 2 5 2 14 1 6 2 16 1 7 2 10 1 8 1 12 2 9 2 6 1 10 2 18 1 11 2 4 1 12 2 9 1 13 1 24 2 14 1 2 2 15 1 11 2 16 2 7 1 17 1 22 2 18 1 5 2 19 2 1 1 20 2 15 1 21 2 19 1 22 1 8 2 23 1 23 2 24 1 25 2 25 1 17 2 26 2 13 1 -
[1] 周盛, 顾高墀, 潘杰元. 航空螺旋桨与桨扇[M]. 北京: 国防工业出版社, 1994. [2] 张伟伟,寇家庆,刘溢浪. 智能赋能流体力学展望[J]. 航空学报,2021,42(4): 26-71.ZHANG Weiwei,KOU Jiaqing,LIU Yilang. Prospect of artificial intelligence empowered fluid mechanics[J]. Acta Aeronautic et Astronautica Sinica,2021,42(4): 26-71. (in Chinese) [3] BRUNTON S L,NOACK B R,KOUMOUTSAKOS P. Machine learning for fluid mechanics[J]. Annual Review of Fluid Mechanics,2020,52: 477-508. doi: 10.1146/annurev-fluid-010719-060214 [4] SIMPSON T, TOROPOV V, BALABANOV V, et al. Design and analysis of computer experiments in multidisciplinary design optimization: a review of how far we have come-or not[R]. AIAA-2008-5802, 2008. [5] JEONG S,SHIMOYAMA K. Review of data mining for multi-disciplinary design optimization[J]. Proceedings of the Institution of Mechanical Engineers: Part G Journal of Aerospace Engineering,2011,225(5): 469-479. doi: 10.1177/09544100JAERO906 [6] JEONG S,CHIBA K,OBAYASHI S. Data mining for aerodynamic design space[J]. Journal of Aerospace Computing, Information, and Communication,2005,2(11): 452-469. doi: 10.2514/1.17308 [7] CHIBA K,OYAMA A,OBAYASHI S,et al. Multidisciplinary design optimization and data mining for transonic regional-jet wing[J]. Journal of Aircraft,2007,44(4): 1100-1112. doi: 10.2514/1.17549 [8] CHIBA K, JEONG S, OBAYASHI S, et al. Knowledge discovery in aerodynamic design space for fly back-booster wing using data mining[R]. Canberra, Australia: the 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, 2006. [9] 汪伟,莫蓉,张岩. 叶片气动优化仿真数据的数据挖掘应用研究[J]. 计算机工程与应用,2013,49(12): 11-15. doi: 10.3778/j.issn.1002-8331.1210-0105WANG Wei,MO Rong,ZHANG Yan. Applied research on simulation data of blade optimization designing based on data mining[J]. Computer Engineering and Applications,2013,49(12): 11-15. (in Chinese) doi: 10.3778/j.issn.1002-8331.1210-0105 [10] 郭振东,宋立明,李军,等. 基于子元模型的全局优化与设计空间知识挖掘方法[J]. 推进技术,2015,36(2): 207-216. doi: 10.13675/j.cnki.tjjs.2015.02.007GUO Zhendong,SONG Liming,LI Jun,et al. Meta model-based global design optimization and exploration method[J]. Journal of Propulsion Technology,2015,36(2): 207-216. (in Chinese) doi: 10.13675/j.cnki.tjjs.2015.02.007 [11] 刘卓,李自启,梁斌,等. 基于粗糙集理论的翼型参数优选方法研究[J]. 航空工程进展,2016,7(1): 87-93,111. doi: 10.16615/j.cnki.1674-8190.2016.01.012LIU Zhuo,LI Ziqi,LIANG Bin,et al. Method of airfoil selection in wing design using rough set theory[J]. Advances in Aeronautical Science and Engineering,2016,7(1): 87-93,111. (in Chinese) doi: 10.16615/j.cnki.1674-8190.2016.01.012 [12] 刘深深,陈江涛,桂业伟,等. 基于数据挖掘的飞行器气动布局设计知识提取[J]. 航空学报,2021,42(4): 350-364.LIU Shenshen,CHEN Jiangtao,GUI Yewei,et al. Knowledge discovery for vehicle aerodynamic configuration design using data mining[J]. Acta Aeronautic et Astronautica Sinica,2021,42(4): 350-364. (in Chinese) [13] 庞梦洋,索中英,郑万泽,等. 基于RS-CART决策树的航空发动机小样本故障诊断[J]. 航空动力学报,2020,35(7): 1559-1568. doi: 10.13224/j.cnki.jasp.2020.07.024PANG Mengyang,SUO Zhongying,ZHENG Wanze,et al. Small sample fault diagnosis of aeroengine based on RS-CART decision tree[J]. Journal of Aerospace Power,2020,35(7): 1559-1568. (in Chinese) doi: 10.13224/j.cnki.jasp.2020.07.024 [14] PAWLAK Z. Rough set theory and its applications to data analysis[J]. Cybernetics and Systems,1998,29(7): 661-688. doi: 10.1080/019697298125470 [15] PAWLAK Z. Rough sets[J]. International Journal of Computer & Information Sciences,1982,11(5): 341-356. doi: 10.1007/BF01001956 [16] 苗夺谦, 李道国. 粗糙集理论、算法与应用[M]. 北京: 清华大学出版社, 2008. [17] 周炜, 周创明, 史朝辉, 等. 粗糙集理论及应用[M]. 北京: 清华大学出版社, 2015. [18] HAN Jiawei, KAMBER M, PEI Jian, 等. 数据挖掘: 概念与技术[M]. 范明, 孟小峰, 译. 机械工业出版社, 2012. [19] 郝丽,莫蓉,魏斌斌,等. 粗糙集理论在关键功能零件识别中的应用[J]. 哈尔滨工业大学学报,2021,53(2): 61-70. doi: 10.11918/202001068HAO Li,MO Rong,WEI Binbin,et al. Application of rough set theory in identification of key functional parts[J]. Journal of Harbin Institute of Technology,2021,53(2): 61-70. (in Chinese) doi: 10.11918/202001068 -

下载: