发明名称 Method and apparatus for evaluating clamp force in a bolt by means of ultra-sonic measurements
摘要 In an apparatus and a method of evaluating a clamp force (F) in a threaded joint between a bolt and a matching threaded piece during a tightening operation, a torque (T) provided to the joint is continuously measured and ultra-sonic pulses are simultaneously induced into the bolt such that a time of flight (TOF) of the pulses in the bolt is measured. In response to an increase of the measured torque (T) an increase rate (dT/dα) of the torque (T) is determined, from which an initial rotation angle (α0) where the torque (T) starts to increase due to bolt deformation is determined. An increase rate (dTOF/dα) of the time of flight (TOF) is also determined. A total increase of the time of flight (ΔTOF) during the tightening operation is then determined based on the initial rotation angle (α0) and the increase rate (dTOF/dα) of the time of flight (TOF).
申请公布号 US9482588(B2) 申请公布日期 2016.11.01
申请号 US201314651881 申请日期 2013.12.10
申请人 ATLAS COPCO INDUSTRIAL TECHNIQUE AB 发明人 Persson Erik Vilhelm;Roloff Arne Torgny
分类号 F16B31/02;G01L5/24;G01L1/25;B25B23/147;G01L5/00 主分类号 F16B31/02
代理机构 Holtz, Holtz & Volek PC 代理人 Holtz, Holtz & Volek PC
主权项 1. A method of evaluating a clamp force (F) in a threaded joint between at least one bolt and a matching threaded piece during a tightening operation, comprises: tightening the joint by means of a torque delivering device, registering a rotation angle (α) between the at least one bolt and the matching threaded piece during tightening of the joint, measuring a torque (T) provided to the joint during tightening thereof, simultaneously inducing ultra-sonic pulses into the at least one bolt and measuring a time of flight (TOF) of the pulses in the at least one bolt, monitoring, in response to a measured increase of the torque (T), the torque (T) as a function of the rotation angle (α) in order to determine an increase rate (dT/dα) of the torque (T), monitoring a time of flight (TOF1) of the ultra-sonic pulses as a function of the rotation angle (α), in order to determine an increase rate (dTOF/dα) of the time of flight (TOF), determining, based on the determined increase rate (dT/dα) of the torque (T), an initial rotation angle (α0) of the tightening operation where the torque (T) starts to increase as a function of bolt deformation, defining the initial rotation angle (α0) of the tightening operation as a rotation angle where the time of flight (TOF) starts to increase, determining a total increase of the time of flight (ΔTOF) during the tightening operation based on the initial rotation angle (α0) of the tightening operation and the increase rate (dTOF/dα) of the time of flight (TOF), and evaluating an established clamp force (F) in the joint based on the total increase of the time of flight (ΔTOF), the clamp force (F) being presumed to be proportional to the total increase of the time of flight (ΔTOF) according to the equation F=k1*ΔTOF, where k1 is a bolt specific constant dependent on the geometry and material of the bolt.
地址 Stockholm SE