首页|发动机撑杆表面损伤形貌与应力分布的研究

发动机撑杆表面损伤形貌与应力分布的研究

扫码查看
本文研究了发动机撑杆表面凹坑及划伤两种损伤与应力分布的影响规律,并开展疲劳试验评估预置损伤撑杆的可靠性.结果表明:当表面存在凹坑损伤时,应力集中随着凹坑椭圆长、短半轴的比值增大而变大,当长短比值超过2时会产生应力尖端,随着入射角度的减小而显著降低,然而应力对凹坑深度的变化响应较弱;当表面存在划伤损伤时,应力集中随着划伤深度的增加而显著增大,划伤深度0.4mm时的应力已超过材料疲劳强度极限,当入射角度减小时应力显著降低.此外,两种损伤形貌的试验件均在焊缝附近的热影响区发生疲劳断裂,预置损伤区未发现工程可检裂纹.
Study on Damage Morphology and Stress Distribution on Engine Spacer Surface
The influence of two kinds of damage on the surface of engine spacer,pit and scratch,on the stress distribution is investigated,and fatigue tests are carried out to evaluate the reliability of the spacer with preset damage.The results show that when there is a pit damage on the surface,the stress concentration increases with the ratio of long and short half-axis of the pit ellipse,and when the ratio of long and short exceeds 2,the stress tip would be generated,and it decreases significantly with the decrease of the incidence angle,however,the response of stress to the change of pit depth is weaker;when there is a scratch damage on the surface,the stress concentration increases significantly with the increase of scratch depth,and the stress has exceeded the fatigue strength limit of the material when the scratch depth is 0.4mm.The stress has exceeded the material fatigue strength limit at 0.4 mm scratch depth,and the stress decreases significantly when the incidence angle decreases.In addition,the fatigue fracture occurred in the heat-affected zone near the weld for both damage patterns,and no engineering detectable cracks were found in the preset damage zone.

damage morphologystress distributionfatigue fracture

杨恺迪、狄小刚、温泉、任寿伟、赵静、王宏罡

展开 >

国营四达机械制造公司,咸阳 712200

损伤形貌 应力分布 疲劳断裂

2024

航空精密制造技术
北京航空精密机械研究所

航空精密制造技术

CSTPCD
影响因子:0.228
ISSN:1003-5451
年,卷(期):2024.60(6)