This application is based upon and claims the benefit of priority from UK Patent Application No. GB 1806323.0, filed on 18 Apr. 2018, the entire contents of which are herein incorporated by reference.
This disclosure relates to a welding process and to a welding apparatus for carrying out the welding process. The disclosure relates particularly, although not exclusively, to resistance welding apparatus.
According to a first aspect, the present disclosure provides a welding process comprising:
The process may include outputting from the data capture and processing equipment a second weld parameter signal representing the centreline position of the weld.
The or each weld parameter signal may be provided to a user interface.
The or each weld parameter signal may be provided to a weld controller, operation of the welding unit being adjusted in response to the or each weld parameter signal.
The probe may be an ultrasonic probe.
The process may be a resistance welding process.
According to a second aspect, the present disclosure provides an apparatus for carrying out a welding process in accordance with the first aspect, the welding apparatus comprising:
The welding unit may comprise a pair of oppositely disposed resistance seam welding electrode wheels. In alternative embodiments, the welding unit may be, for example, a laser welding unit.
The probe may comprise a phased array ultrasonic probe unit comprising an array of piezoelectric elements. The array of piezoelectric elements may be a linear array extending transversely of the weld direction.
The ultrasonic probe may be situated in a cavity of a housing having a coupling liquid inlet. The housing may have an open face positioned for at least partial closure by the workpiece. The housing may be configured to be supported on the workpiece by liquid flowing from the cavity through a gap between the housing and the workpiece.
The probe may be provided with support wheels for supporting the probe on the workpiece.
The probe may have an encoding device responsive to relative displacement between the probe and the workpiece.
The encoding device may comprise at least one encoding wheel positioned for rolling contact with the workpiece.
The probe may be fixed in position with respect to the welding unit in the welding direction.
In alternative embodiments, the weld monitoring equipment may, for example, comprise a laser ultrasonic testing (LUT) system.
The distance between the welding unit and the weld monitoring equipment may be not less than 5 mm and not more than 20 mm.
The data capture and processing equipment may be configured to process signals from the probe and to output data to a user interface.
The data capture and processing equipment is configured to process signals from the ultrasonic probe and to output control signals to a weld controller for the welding unit.
By providing the weld monitoring equipment as part of the welding apparatus, it is possible to assess the weld as it is being formed by the welding unit, enabling adjustments to be made to the operation of the welding unit during the course of the welding process if the weld characteristics deviate from predetermined parameters.
According to a third aspect, the present disclosure provides a method of modifying existing welding apparatus comprising:
Arrangements will now be described, by way of example, with reference to the accompanying drawings, in which:
Resistance welding processes are well known, and may take a variety of forms. The description below refers to a seam welding process using electrodes in the form of conductive electrode wheels which sit on opposite sides of a workpiece to be welded. In some such processes, the wheels make direct contact with the workpiece, but in others at least one of the electrode wheels is grooved so that a shaped copper wire can be introduced between the wheel and the workpiece. In other resistance welding processes, different forms of electrode are used. Also, other forms of welding are known, such as laser welding. It will be appreciated that the seam welding process described below can be replaced by alternative welding processes.
The apparatus shown in
Drive wheels 10, 12 engage the peripheries of the respective electrode wheels 4, 6. The drive wheel 10 is shown in
As shown in
The apparatus shown in
The probe 24 is provided with encoding wheels 36 (only one of which I shown in
The probe unit 30 is a phased array probe unit comprising a plurality of individual piezoelectric elements 38 which are disposed in a linear array extending transversely of the weld line 20 and of sufficient length to extend on both sides beyond the weld line 20 itself.
The ultrasonic probe 24 is carried by the supporting structure 2 so that it maintains a fixed position behind the welding unit, with respect to a welding direction 40, as shown in
The weld monitoring equipment 22 also comprises a data logging and processing unit 46 and a graphical user interface in the form of a screen 54. The data logging and processing unit 46 is in communication, for example by wiring 48 and 52, with the ultrasonic probe 24 and the screen 54. The data logging and processing unit 46 is also connected, as indicated at 50, with a weld controller 56, which controls inputs to the electrode wheels 4, 6.
For operation, the components 8A and 8B are positioned between the electrode wheels 4, 6, which may be moved apart for this purpose. The components 8A and 8B are positioned together, possibly with the aid of suitable clamps or jigs, so that they overlap in the regions to be welded. The electrode wheels 4, 6 are then brought towards each other to clamp the overlapping regions of the components 8A and 8B under high pressure. For example, one of the electrode wheels 4, 6 may be mounted displaceably on the supporting structure 2 so that it can be moved under power towards the other of the electrode wheels 4, 6.
The electrode wheels 4, 6 are then rotated in opposite directions, as indicated by arrows in
The ultrasonic probe 24 is positioned closely behind the wheel 4, and consequently the newly-formed weld 62 passes beneath it shortly after it is formed. Water supplied under pressure through the inlet 32 enters the cavity 28 and is discharged at the open face 34, passing through a gap 64 formed between the housing 26 and the upper face (as shown in
The probe unit 30 is controlled to emit an input signal in the form of a series of ultrasonic pulses from the individual piezoelectric elements 38 in a predetermined time sequence. Each pulse propagates through the water layer within the cavity 28, into the material of the workpiece 8 and the formed weld 62. The pulses are reflected from features of the components 8A and 8B that they encounter, and in particular the various surfaces and transitions of the components 8A and 8B, and the returning reflected pulses, constituting an output signal derived from the input signal but modified by the features of the components 8A and 8B, are captured by the elements 38. In addition, the encoding wheels 36 provide signals representing the position of the workpiece 8, in order that the signals from the probe unit 30 can be correlated with the position along the weld 62.
The resulting signals are sent to the data logging and processing unit 46, which analyses the signals and provides an output to the screen 54. The screen 54 can display a variety of images representing parameters and other characteristics of the weld 62. An example of such images is shown in
The lower image in
The images of
Also, automatic intervention can be achieved as a result of the data logging and processing unit providing feedback signals to the weld controller 56. For example, if the output from the data logging and processing unit 46 indicates that the width of the weld 62 has decreased towards a lower limit value, the weld controller 56 may adjust various parameters of the welding operation, for example the pressure applied by the electrode wheels 4, 6, their speed of rotation (and hence the relative travel speed of the workpiece 8 past the electrode wheels 4, 6), or the welding current supplied to the electrode wheels, in order to maintain the width within acceptable limits. The probe 24 thus enables real-time monitoring of the welding process, with the facility to adjust the process, either manually or automatically, to correct deviations.
A practical embodiment of welding apparatus as shown in
number of piezoelectric elements 38 in the linear phased array 30: 120
length of linear phased array 30: 20 mm
width of weld 62: 5-7 mm
thickness of components 8A, 8B: 0.6 to 3.2 mm
width of electrode wheels 4, 6 at point of contact: 8 mm
diameter of electrode wheels 4, 6: approximately 300 mm
feed rate: 25-50 mm/minute
stand-off of ultrasonic probe 24 from electrode wheel 4: 5-20 mm
At step 84, welding current is supplied to the electrode wheels 4, 6, to fuse the material of the components 8A, 8B causing them to become welded together as they pass between the electrode wheels 4, 6. At step 86, the ultrasonic probe 24 is activated to emit ultrasonic pulses into the workpiece 8 and to receive reflected pulses as signals which are transmitted to the data logging and processing unit 46. At step 88, the signals from the ultrasonic probe 24 are processed in the data logging and processing unit 46 to produce output data which, at step 90, is compared with reference data to determine whether or not the welding process is proceeding in accordance with requirements. If the output at step 90 is “YES” the process returns to step 88 without any modification of the welding parameters. However, if the output from 90 is “NO”, the process proceeds to step 92 at which modifications to the welding parameters are made by way of the weld controller 56 in order to bring the process into line with predetermined requirements.
It will be appreciated that, although the present disclosure describes the welding of a large-diameter workpiece 8, the process can be adapted to other forms of workpiece, for example bellows, flexible seals, smaller components of cylindrical form such as food cans, and automotive components.
Although the probe 24 is shown supported on the workpiece 8 by means of the water from the cavity 28 flowing through the gap 64, it could be supported by other means, for example by a tracking wheel or set of rollers.
It will be appreciated that the screen or other graphical user interface 54 need not be situated in the immediate vicinity of the remainder of the welding apparatus. Instead, the screen 54 could be situated remotely, with the facility for the operator to monitor progress of the welding operation, and to provide input to the weld controller 56, from the remote location.
It will be appreciated that the monitoring unit 22 can easily be detached from the rest of the welding apparatus if it is not required for a particular welding operation. Similarly, the monitoring unit 22, being a self-contained unit, could be retrofitted to an existing welding installation.
In cases where a weld line follows a complex path, measures may need to be taken to ensure that the monitoring unit 22 follows the line of the weld 62 accurately, without cutting corners as it follows the path of the wheels 4, 6. Accurate following of the line of the weld 62 is assisted by minimising the distance d at which the monitoring unit 22 follows the wheels 4, 6.
Although the description above refers to the probe unit 30 as an ultrasonic device, other forms of monitoring are possible. For example, the weld characteristics could be monitored using X-rays, or by assessing heat transfer rates across the components 8A and 8B.
In the arrangement described above with reference to the drawings, the welding unit is a resistance welding unit utilizing the electrode wheels 4, 6. In other embodiments, the welding unit may be a laser welding unit. Laser welding processes do not employ a coolant such as water. A trailing monitoring system using weld monitoring equipment 22 which includes an ultrasonic probe 24 could nevertheless be employed provided that the workpiece 8 is kept dry local to the beam impingement position. Alternatively an LUT (laser ultrasonic testing) system can be used, in which a pulsed laser (separate from the welding laser) is directed at the weld 62. The pulsed laser ablates the surface of the workpiece 8 to a minimal depth. The shockwave from the ablation provides a sonic source which is then picked up by another laser serving as a detection laser. The surface of the workpiece 8 is scanned as a transverse array of inspection events (analogous to the piezo-electric system used for the resistance welding as described above). Laser welds are typically narrower than resistance welds, so the inspection width and spacing would scale accordingly. Significantly, laser welding has more of a risk of joint separation in a lap condition as there is no direct pressure through the weld 62 at the point of welding as there is for resistance welding.
As an alternative to weld monitoring using laser ablation, a system using laser heating, without ablation, could be employed.
Number | Date | Country | Kind |
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1806323.0 | Apr 2018 | GB | national |