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航空液压管路轴向挤压式接头组件连接强度的数值分析

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针对目前航空液压管接头无法满足高工作压力要求的问题,以Φ12 mm的钛合金轴向挤压式接头为研究对象,利用Abaqus平台建立了轴向挤压连接成形与拉脱试验过程的有限元模型,通过同参数条件下的拉脱试验验证了有限元模型的准确性.结果表明,有限元模型计算误差仅为3.4%,接头组件连接强度是由导管与管套凹槽的轴向对抗阻力和导管与管套径向接触力共同决定的.系统研究了管套材料力学性能、凹槽结构、摩擦因数对接头组件连接强度的影响规律,管套材料屈服强度越高,连接强度越强;管套凹槽宽度每增长0.2 mm,连接强度提高约2.4%;摩擦因数每增加0.01,接头连接强度平均提升18%左右.
Numerical analysis of connection strength of axial extrusion joint for aviation hydraulic pipeline
In view of the problem that the current aviation hydraulic pipe joint cannot meet the requirements of high working pressure,taking the Φ12 mm titanium alloy axial extrusion joint as the research object,the finite element model of axial extrusion connection form-ing and pulling-out test process were established by Abaqus platform.The accuracy of the finite element model was verified by pulling-out test under the same parameter condition.The results show that the calculation error of the finite element model is only 3.4%,the connec-tion strength of the joint is jointly determined by the antagonistic resistance between pipe and groove of sleeve in the axial direction and the radial contact force between pipe and sleeve.The influence of the mechanical properties,groove structure and friction factor on connection strength of joint was systematically studied.The higher the yield strength of sleeve material,the stronger the connection strength.For ev-ery 0.2 mm increase of groove width,the connection strength increases by about 2.4%;for every 0.01 increase of friction factor,the con-nection strength of the joint increases by 18%on average.

axial extrusiontitanium alloypipeconnection strengthfinite element

赵天章、张铁森、白雪山、张帅、韩颖杰、戴群

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沈阳航空航天大学航空宇航学院,辽宁沈阳 110135

沈阳飞机工业(集团)有限公司,辽宁沈阳 110850

轴向挤压 钛合金 导管 连接强度 有限元

国家自然科学基金青年资助项目辽宁省教育厅项目沈阳市中青年科技创新人才支持计划

51605310LJKZ0180RC210422

2024

塑性工程学报
中国机械工程学会

塑性工程学报

CSTPCD北大核心
影响因子:0.46
ISSN:1007-2012
年,卷(期):2024.31(1)
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