中国机械工程 ›› 2025, Vol. 36 ›› Issue (9): 1934-1941.DOI: 10.3969/j.issn.1004-132X.2025.09.004

• 机械基础工程 • 上一篇    

基于内聚力模型的某型挂钩悬挂失效分析

李增伟1,2(), 侯泽伟1, 洪家旺1(), 祁军义2   

  1. 1.北京理工大学宇航学院, 北京, 100080
    2.郑州飞机装备有限责任公司, 郑州, 450052
  • 收稿日期:2024-08-26 出版日期:2025-09-25 发布日期:2025-10-15
  • 通讯作者: 洪家旺
  • 作者简介:李增伟,男,1999年生,硕士研究生,研究方向为机载悬挂发射装置。E-mail:894269070@qq.com
    洪家旺*(通信作者),男,1981年生,教授、博士研究生导师。研究方向为智能材料多场耦合力学。E-mail:hongjw@bit.edu.cn
  • 基金资助:
    国家自然科学基金(12102007)

Failure Analysis of a Certain Type of Hook Suspension Based on Cohesive Zone Model

Zengwei LI1,2(), Zewei HOU1, Jiawang HONG1(), Junyi QI2   

  1. 1.School of Aerospace Engineering,Beijing Institute of Technology,Beijing,100080
    2.Zhengzhou Aircraft Equipment Co. ,Ltd. ,Zhengzhou,450052
  • Received:2024-08-26 Online:2025-09-25 Published:2025-10-15
  • Contact: Jiawang HONG

摘要:

针对某型挂钩在进行挂载试验时阻铁镉镀层脱落造成阻铁下滑而导致悬挂物悬挂姿态发生偏转甚至有掉落风险的问题展开研究。基于内聚力模型建立了预设垂直裂纹和界面裂纹的挂钩挂载有限元模型,通过裂纹损伤因子判定裂纹失效形式,并构建了止动臂/阻铁的局部接触模型,研究镀层界面脱黏过程中的摩擦因数变化情况。结果表明,在挂钩挂载过程中,阻铁镀层与基材在结合面处产生面内剪切应力差导致界面脱黏,但整个过程不产生垂直裂纹,同时在界面脱黏过程中接触面摩擦因数会短暂降低至0.05以下,低于阻铁下滑的临界滑动摩擦因数。

关键词: 挂钩, 摩擦因数, 镀层, 内聚力模型, 脱黏损伤

Abstract:

During the mount tests of a certain type of hook, Cd-Ti coating of latch was delaminated, and caused the latch slide downward, then the suspension might deflected, posing a risk of suspension detachment. A research on this risk was conducted. Based on cohesive zone model, a finite element model of the hook under load was established, incorporating predefined vertical cracks and interfacial cracks. The crack damage factor was employed to determine the crack failure modes, and a local contact model of the stop arm/latch was developed to investigate the variations in friction coefficient during coating interface debonding. Results reveal that during the hook's load-bearing processes, in-plane shear stress differences at the interfaces between the latch coating and the substrate induce interfacial debonding, without the formation of vertical cracks. Meanwhile, the friction coefficient at the contact interfaces temporarily drops below 0.05 during debonding, which is lower than the critical sliding friction coefficient required to prevent latch slippages.

Key words: hook, friction coefficient, coating, cohesive zone model, debonding damage

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