航空学报 > 1994, Vol. 15 Issue (2): 181-187

钛合金振动攻丝刀具破损监测的研究

张德远, 韩云台, 陈鼎昌   

  1. 北京航空航天大学707教研室,北京,100083
  • 收稿日期:1992-08-17 修回日期:1992-12-07 出版日期:1994-02-25 发布日期:1994-02-25

STUDY ON MONITORING OF TOOL BREAKAGE FOR VIBRATION TAPPING IN TITANIUM ALLOYS

Zhang Deyuan, Han Yuntai, Chen Dingchang   

  1. FacuLty 707 of Beijing University of Aeronautics and Astronautics,Beijing,100083
  • Received:1992-08-17 Revised:1992-12-07 Online:1994-02-25 Published:1994-02-25

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。

关键词: 攻丝, 钛合金, 应力测量, 扭转振动

Abstract: 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.

Key words: taps, titanium alloy, stress measurement, torsional vibration

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