摘要
分析了航天某型号用紧固件在不同垫圈结构状态下的防松性能,以M16规格紧固件为研究对象,着重研究了M16紧固件在模拟航天某型号部段实际安装环境下,不同垫圈结构对防松性能以及支撑面摩擦系数、螺纹摩擦系数、预紧力等相关参数的影响及其相应变化的规律。结果表明,在装配条件一致的情况下,垫圈结构不同造成支承面摩擦系数出现较大变化,同时相同安装力矩条件下轴向预紧力出现了极大的差异;NordLock垫圈和双面斜齿垫圈防松性能最好,平垫圈+弹簧垫圈组合虽具有一定的防松能力,但失效的概率大,而平垫圈、HS垫圈防松性能最差。
The anti-loosening performance of fasteners for a certain type of aerospace under different gasket structures is analyzed.Taking the fasteners of M16 specification as the research object,the influence of different gasket structures on the anti-loosening performance,friction coefficient of support surface,friction coefficient of thread and clamp force and the corresponding variation of M16 fasteners under the actual installation environment of a certain type of spaceflight are studied.The results show that:under the same assembly conditions,the coefficient of friction between bearing surface changes greatly due to the different gasket structures,and there is a great difference in the axial clamp force under the same tightening torque.The anti-loosening performance of NordLock gasket and double-sided oblique gear gasket is best.Although the combination of flat gasket and spring gasket has a certain anti-loosening ability,the failure probability is high.However the anti-loosening performance flat gasket and HS gasket is the worst.
作者
高学敏
石大鹏
冯韶伟
关悦
闫路
杨冬梅
GAO Xuemin;SHI Dapeng;FENG Shaowei;GUAN Yue;YAN Lu;YANG Dongmei(Henan Aerospace Precision Machining Co.,Ltd.,Xinyang 464000,China;Henan Key Laboratory of Fastening Connection Technology,Xinyang 464000,China;Beijing Institute of Aerospace Systems Engineering,Beijing 100076,China)
出处
《航空制造技术》
CSCD
北大核心
2022年第13期105-109,共5页
Aeronautical Manufacturing Technology
基金
中国科协青年托举人才工程资助项目(2017QNRC001)。
关键词
振动
航天型号
摩擦系数
预紧力
防松性能
Vibration
Aerospace model
Friction coefficient
Clamp force
Anti-loosening performance