TY - JOUR
T1 - Invariance of conveying capacity for drilling into lunar soil simulant
AU - Chen, Tao
AU - Zhao, Zhen
AU - Schwartz, Stephen R.
AU - Liu, Caishan
AU - Wang, Qi
N1 - Publisher Copyright:
© 2019 COSPAR
PY - 2019/11/1
Y1 - 2019/11/1
N2 - In this paper, we study the conveying dynamics in the helical groove of an auger drilling into lunar simulant. We demonstrate that the stress-coupling effect of the conveyed granules by the groove of a drill auger plays a significant role on the dynamics of conveyance. For this, a discrete element method (DEM) is adopted first to uncover the motion and the stress characteristics of conveyed granules in a working auger. Then, a simplified dynamic model following the stress characteristics of DEM is established. The simplified model can not only reflect the results by the discrete element method, but can also explain well the proportional relationship between the maximum conveying rate and the rotating speed of the auger in the experiment (Zhao et al., 2019).
AB - In this paper, we study the conveying dynamics in the helical groove of an auger drilling into lunar simulant. We demonstrate that the stress-coupling effect of the conveyed granules by the groove of a drill auger plays a significant role on the dynamics of conveyance. For this, a discrete element method (DEM) is adopted first to uncover the motion and the stress characteristics of conveyed granules in a working auger. Then, a simplified dynamic model following the stress characteristics of DEM is established. The simplified model can not only reflect the results by the discrete element method, but can also explain well the proportional relationship between the maximum conveying rate and the rotating speed of the auger in the experiment (Zhao et al., 2019).
KW - Coring drill
KW - Helical groove
KW - Maximum conveying rate
KW - Transverse coupling effect
UR - https://www.scopus.com/pages/publications/85070808880
U2 - 10.1016/j.asr.2019.08.001
DO - 10.1016/j.asr.2019.08.001
M3 - 文章
AN - SCOPUS:85070808880
SN - 0273-1177
VL - 64
SP - 1816
EP - 1824
JO - Advances in Space Research
JF - Advances in Space Research
IS - 9
ER -