煤炭工程 ›› 2023, Vol. 55 ›› Issue (10): 185-192.doi: 10.11799/ce202310031

• 装备技术 • 上一篇    

非均质底板下掘锚机履带系统散-动耦合行驶性能分析#br#

杜尚宇   

  1. 1. 中煤科工开采研究院有限公司,北京 100013
    2. 煤炭科学技术研究院有限公司,北京 100013
  • 收稿日期:2023-04-20 修回日期:2023-08-03 出版日期:2023-10-20 发布日期:2025-04-08
  • 通讯作者: 杜尚宇 E-mail:3269828434@qq.com

Driving performance analysis of MB670-1 anchor digger on roadway floor based on DEM-MBD coupling

#br#   

  • Received:2023-04-20 Revised:2023-08-03 Online:2023-10-20 Published:2025-04-08
  • Contact: yu shangdu E-mail:3269828434@qq.com

摘要: 摘 要: 为研究掘锚机在巷道底板平整度发生改变时的行驶性能, 以MB670-1型掘锚机为对象, 以张家峁煤矿5-2 煤层为背景, 建立了掘锚机的运动分析模型, 并运用多体动力学理论和离散元理论, 对掘锚机履带系统和巷道底板进行了精细化描述, 最后采用DEM-MBD 耦合方法分析了掘进机在巷道底板行驶过程中的运动状态及其履带系统的力学特性。研究结果表明: 掘锚机在巷道底板改变时的行驶状态良好, 其中纵向平均滑移率为19%, 竖直方向的最大沉陷量为20.2mm, 横向最大偏移量为3.8mm; 位于承重轮下方的履带板张紧力随驱动轮转矩增大而变大, 其余位置履带板的张紧力基本不变; 在履带系统中驱动轮受到的载荷最大, 平均值为129.6kN; 位于机头下方位置的承重轮受到的载荷最大, 平均值为78kN; 位于机身中后部的拖带轮受到的载荷最大, 为5.7kN。研究结果为提高掘锚机可靠性以及稳定性控制提供一定参考。

关键词: MB670-1型掘锚机, DEM-MBD耦合, 行驶性能, 履带系统

Abstract:

Aiming at the problem of windlass running deviation and serious wear of its track system, taking MB670-1 windlass as the object, and taking 5-2 coal seam of a coal mine as the background, the motion analysis model of the windlass is established, and the detailed description of the windlass track system and the roadway floor is carried out using the multi-body dynamics theory and discrete element theory, Finally, the DEM-MBD coupling method is used to analyze the movement state of the roadheader and the mechanical characteristics of its track system during the driving process of the roadway floor. The research results show that the driving state of the windlass on the roadway floor is good, with the average longitudinal slip rate of 19%, the maximum vertical settlement of 20.2 mm, and the maximum lateral displacement of 20.2 mm; The tension force of the track shoe under the bearing wheel increases with the torque of the driving wheel, and the tension force of the track shoe at other positions is basically unchanged; In the track system, the driving wheel receives the largest load, with an average value of 129.6kN; The load bearing wheel located under the machine head is the largest, with an average value of 78kN; The tug wheel at the middle and rear of the fuselage bears the maximum load of 5.7kN. The research results provide a basis for improving the reliability and stability control of the windlass.

中图分类号: