西南石油大学学报(自然科学版) ›› 2025, Vol. 47 ›› Issue (6): 151-167.DOI: 10.11885/j.issn.1674-5086.2023.10.16.02

• 石油机械与油田化学 • 上一篇    下一篇

基于内聚力模型的螺杆马达界面力学研究及改善

任美鹏1, 谢仁军1, 祝效华2, 石昌帅2, 张兴全1   

  1. 1. 中海油研究总院有限责任公司, 北京 朝阳 100027;
    2. 西南石油大学机电工程学院, 四川 成都 610500
  • 收稿日期:2023-10-16 发布日期:2026-01-12
  • 通讯作者: 任美鹏,E-mail:renmp@cnooc.com.cn
  • 基金资助:
    四川省自然科学基金(23NSFSC2137);南充市 西南石油大学市校科技战略合作项目(SXHZ049);“十四五”重大科技项目(KJGG2021–0800)

Research and Improvement of Interface Mechanical Behavior of Screw Motor Based on Cohesive Zone Model

REN Meipeng1, XIE Renjun1, ZHU Xiaohua2, SHI Changshuai2, ZHANG Xingquan1   

  1. 1. CNOOC Research Institute Company Limited, Chaoyang, Beijing 100027, China;
    2. School of Mechatronic Engineering, Southwest Petroleum University, Chengdu, Sichuan 610500, China
  • Received:2023-10-16 Published:2026-01-12

摘要: 针对螺杆马达定子橡胶衬套易脱胶失效的问题,开展了7/8头常规及等壁厚螺杆马达定子衬套失效机理的研究,研究中采用了橡胶-金属界面内聚力原理,通过橡胶-金属粘接力学试验和橡胶单轴拉伸试验,以及有限元和数值分析,获得了界面切应力是造成衬套粘接失效的主要因素,且衬套线型最小圆弧半径是造成界面最大切应力改变的主要原因;钻井液、过盈量对等壁厚衬套界面切应力影响显著,钻井液液柱压力由15 MPa增大到60 MPa,等壁厚衬套界面最大切应力增大146%,等壁厚螺杆马达更容易出现粘接失效。最后提出异壁厚衬套结构,异壁厚衬套界面切应力小于等壁厚衬套,且随最小圆弧半径增大而减小,具有良好的散热性;异壁厚衬套发生疲劳失效时使用时长与最小圆弧半径成正比,预测疲劳失效时最大使用时长为240.99 h,率先发生疲劳失效区域为衬套内腔弧顶,与实际失效现象一致。为螺杆马达设计优化提供了理论依据,并为提高螺杆马达工作寿命做出重要贡献。

关键词: 内聚力模型, 界面切应力, 粘接失效, 异壁厚衬套, 疲劳寿命预测

Abstract: Aiming at the problem of debonding failure of the stator rubber bushing of the screw motor, the failure mechanism of the stator bushing of the 7/8 head conventional and equal wall thickness screw motor was studied. The principle of rubber-metal interface cohesion was adopted in the study. Through rubber-metal bonding mechanics test and rubber uniaxial tensile test, and finite element and numerical analysis, the interface shear stress was found to be the main factor causing the bushing bonding failure, and the minimum arc radius $R$ of the bushing profile was the main reason for the change of the maximum interface shear stress. The drilling fluid and interference have a significant effect on the shear stress at the interface of the equal wall thickness bushing. When the drilling fluid pressure increases from 15 MPa to 60 MPa, the maximum shear stress at the interface of the equal wall thickness bushing increases by 146%, and the equal wall thickness screw motor is more prone to bonding failure. Finally, the different wall thickness bushing structure is proposed. The interface shear stress of the different wall thickness bushing is less than that of the equal wall thickness bushing, and decreases with the increase of the minimum arc radius $R$, which has good heat dissipation. The service life of the bushing with different wall thickness is proportional to the minimum arc radius when fatigue failure occurs. The maxi-mum service life is predicted to be 240.99 h when fatigue failure occurs. The first fatigue failure area is the inner cavity arc top of the bushing, which is consistent with the actual failure phenomenon. This paper provides a theoretical basis for the design optimization of screw motor, and makes an important contribution to improve the working life of screw motor.

Key words: cohesive zone model, interface shear stress, bonding failure, different wall thickness bushing, fatigue life prediction

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