基于嫦娥五号月壤粒形特征的离散元模拟方法

    王思远, 蒋明镜

    王思远, 蒋明镜. 基于嫦娥五号月壤粒形特征的离散元模拟方法[J]. 岩土工程学报, 2024, 46(4): 833-842. DOI: 10.11779/CJGE20230040
    引用本文: 王思远, 蒋明镜. 基于嫦娥五号月壤粒形特征的离散元模拟方法[J]. 岩土工程学报, 2024, 46(4): 833-842. DOI: 10.11779/CJGE20230040
    WANG Siyuan, JIANG Mingjing. Lunar regolith simulations with discrete element method based on Chang'E-5 mission's lunar soil particle morphology[J]. Chinese Journal of Geotechnical Engineering, 2024, 46(4): 833-842. DOI: 10.11779/CJGE20230040
    Citation: WANG Siyuan, JIANG Mingjing. Lunar regolith simulations with discrete element method based on Chang'E-5 mission's lunar soil particle morphology[J]. Chinese Journal of Geotechnical Engineering, 2024, 46(4): 833-842. DOI: 10.11779/CJGE20230040

    基于嫦娥五号月壤粒形特征的离散元模拟方法  English Version

    基金项目: 

    海南省重点研发计划项目 ZDYF2021SHFZ264

    国家重大自然灾害防控与公共安全重点专项项目 2022YFC3003403

    国家自然科学基金创新研究群体项目 42221002

    国家自然科学基金重大项目 51890911

    土木工程防灾国家重点实验室自主研究课题基金项目 SLDRCE19-A-06

    详细信息
      作者简介:

      王思远(1995—),男,博士研究生,主要从事太空土数值模拟及土体宏微观力学方面研究。E-mail: wsiy@tju.edu.cn

      通讯作者:

      蒋明镜, E-mail: mingjing.jiang@usts.edu.cn

    • 中图分类号: TU43

    Lunar regolith simulations with discrete element method based on Chang'E-5 mission's lunar soil particle morphology

    • 摘要: 为满足当前中国探月任务中的“堪测、采、建”战略规划,获取更加贴近真实的月壤物理力学特性,考虑月壤颗粒形状的影响,结合嫦娥五号探月任务中的月壤颗粒图像,将月壤粒形特征与颗粒级配联系起来,提出考虑中国月壤粒形特征的离散元数值模拟方法。首先,基于嫦娥五号探月任务获取的部分月壤颗粒图像,对颗粒的形状特征及尺寸信息进行提取,依据其球度特征将月壤的颗粒形态分为6类,并同月壤颗粒的粒形特征与颗粒尺寸建立对应关系;其次,结合本团队开发的三维离散元月壤接触模型,引入形状参数用以表征月壤颗粒的抗转动能力,进而在离散元中考虑月壤颗粒的粒形特征,最终建立考虑中国月壤粒形特征的离散元数值模型;通过与已知月壤试验结果的对比表明,该方法可将月壤颗粒形状的可变性直接映射到离散元中。在此基础上,通过与不考虑粒形特征的数值样进行对比,探究考虑月壤粒形特征的优势。结果表明:含嫦娥五号月壤粒形特征的离散元数值模型可以有效捕捉月壤力学行为的主要特征,为开展月球资源勘探及开发利用研究提供基础。
      Abstract: To align with the current strategic planning of "survey, mining, and development" in China's lunar exploration mission, and to obtain more accurate physical and mechanical properties of lunar regolith, this study focuses on the influences of lunar regolith particle shape based on particle images from the lunar regolith of the Chang'E-5 mission. A discrete element numerical simulation method that considers lunar regolith particle morphology is proposed by linking particle shape characteristics with gradation. Initially, the shape characteristics and size information of the particles are extracted from the lunar regolith images. The particles are subsequently categorized into six groups based on their sphericity, establishing the corresponding relationships. Secondly, the study utilizes a three-dimensional (3D) lunar regolith contact model and calculates rolling and twisting resistances at inter-particle contact by incorporating shape parameters to account for lunar particle shape effects. Subsequently, the model considers particle size characteristics within the discrete element analysis. Ultimately, a discrete element numerical model that incorporates the particle shape characteristics of the China's lunar regolith is developed. Comparison with the results of Apollo lunar regolith laboratory tests reveals that the variability of grain shape in lunar particles can be directly incorporated into the discrete model. Additionally, the benefits of considering the grain shape characteristics of lunar regolith are discussed in comparison to numerical samples that neglect the characteristics. The results show that the proposed method can effectively capture the main characteristics of the mechanical behavior of lunar regolith, and provide a basis for the lunar resource exploration and exploitation methods.
    • 致谢: 感谢中国科学院地质与地球物理研究所杨蔚研究员对本文提供的巨大帮助!感谢团队硕士生管成良、李天赐、石宵宵、杨越群在本文中提供的帮助。
    • 图  1   部分月球表面颗粒[22]

      Figure  1.   Multiple lunar regolith particles[22]

      图  2   基于图像识别月壤粒形特征捕获流程图

      Figure  2.   Implementation of lunar soil particle shape feature capture based on image processing

      图  3   嫦娥五号月球样品的颗粒形状和尺寸分布

      Figure  3.   Particle shape and size distributions of Chang'E lunar sample

      图  4   月壤颗粒球度和抗转动的散点分布

      Figure  4.   Scatter distribution of sphericity and rolling resistances of lunar soil particles

      图  5   月壤粒间接触示意图

      Figure  5.   Schematic diagram of lunar soil particle contact

      图  6   考虑抗转动影响的粒间演化规律

      Figure  6.   Contact evolution between particles considering resistance rotation coefficient

      图  7   DEM模拟颗粒级配曲线及抗转动参数

      Figure  7.   DEM simulation of grain grading curve and corresponding resistance rotation coefficient

      图  8   Apollo 12/16月壤颗粒形态特性

      Figure  8.   Morphological characteristics of soil particles in Apollo 12/16 mission

      图  9   数值模拟与室内试验对比

      Figure  9.   Comparison between numerical simulations and laboratory tests

      图  10   不同围压下试样三轴试验结果

      Figure  10.   Results of conventional triaxial tests under different confining pressures

      图  11   剪切过程中力学配位数及APR演化规律

      Figure  11.   Evolution of mechanical coordination number and porosity during shearing

      表  1   月壤的颗粒形态分布表

      Table  1   Representative particle morphologies of lunar particles

      球度范围 颗粒占比/% 代表性颗粒形态
      Sp < 0.6 1.3
      0.6 < Sp < 0.7 5.8
      0.7 < Sp < 0.8 18.1
      0.8 < Sp < 0.9 39.27
      0.9 < Sp < 0.94 18.3
      0.94 < Sp < 1.0 17.18
      下载: 导出CSV

      表  2   离散元模拟参数[21]

      Table  2   Parameters used in DEM simulations

      接触类型 细观参数 取值
      球-球 颗粒密度/(kg·m-3) 2320
      有效模量Ep/MPa 800
      法向与切向刚度比ζ 5
      抗转动系数β 图 7
      局部破碎系数 4
      颗粒摩擦系数 0.5
      局部阻尼 0.7
      下载: 导出CSV
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