摘要
对振动攻丝的力学模型进行了研究,找出了钛合金振动攻丝刀具破损失效时的力学特征,并建立了钛合金振动攻丝的振动控制、破损监测和报警停机的自动监控系统。
Tapping small size thread in deep holes in titanium alloy is a very difficult technology in airplane manufacture.The primary problem is that the frictional torque in the flank face of the tap is very big and makes the tap break or rupture,Although we have improved this operation remarkably by vibration tapping technique, with continuously running the vibration tapping pro-cess,the tap teeth are worn gradually and it makes the tap break or rupture also.Therefore,this paper describes some new researches including the study of mechanics model for vibration tap-ping,the analysis ofmechanics characteristic in tap failure,and the method to create an automat-ed monitoring and control system used for vibration control, tap breakage detection and alarm.
出处
《航空学报》
EI
CAS
CSCD
北大核心
1994年第2期181-187,共7页
Acta Aeronautica et Astronautica Sinica
基金
航空科学基金
关键词
攻丝
钛合金
应力测量
扭转振动
taps,titanium alloy, stress measurement, torsional vibration