US20050006441A1 - Stir-friction hot working control system - Google Patents
Stir-friction hot working control system Download PDFInfo
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- US20050006441A1 US20050006441A1 US10/773,045 US77304504A US2005006441A1 US 20050006441 A1 US20050006441 A1 US 20050006441A1 US 77304504 A US77304504 A US 77304504A US 2005006441 A1 US2005006441 A1 US 2005006441A1
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- Prior art keywords
- pin tool
- force
- workpiece
- penetration
- lead screw
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
- B23K20/12—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding
- B23K20/122—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding using a non-consumable tool, e.g. friction stir welding
- B23K20/123—Controlling or monitoring the welding process
Definitions
- This invention relates to control arrangements for stir-friction welders, and more particularly to automatic positioning systems for stir-friction welders.
- FIG. 1 is a simplified illustration of a prior-art stir-friction welding arrangement 10 .
- an anvil 12 supports a flat workpiece 14 , illustrated in phantom to make other portions of the arrangement more obvious.
- a friction-stir pin tool and spindle arrangement designated generally as 16 includes a spindle 18 which rotates about its axis 8 , carrying with it a pin tool or ligament holding arrangement 20 .
- the pin tool itself includes an elongated pin or ligament 22 , which also rotates in consonance with the rotating spindle 18 .
- the pin tool or ligament 22 of FIG. 1 must be maintained at a depth which provides full hot working of the desired region of the workpiece.
- the depth of plunge of the pin tool 22 is the depth to which the tip 28 of the pin tool 22 extends below the upper surface 14 us , which is the surface from which the pin tool is introduced into the workpiece.
- the depth of plunge cannot be such that the tip 28 of pin tool 22 extends beyond the second or lower surface 14 of the workpiece, because this might weld the workpiece 14 to the anvil 12 , or might damage the workpiece or pin tool.
- the position of the pin tool is maintained at the appropriate level by a set 26 of rollers, only one of which, namely roller 26 a , is illustrated.
- Roller 26 a is affixed by a shaft 26 to the spindle or tool holder, and rotates therewith, bearing on the upper surface 14 us of the workpiece 14 .
- the position of the tip 28 of the pin tool 22 in this prior-art arrangement extends below (or beyond) the lower rolling surface of the rollers by the desired penetration of the workpiece.
- the penetration of the workpiece may be termed “axial” penetration, because the penetration is in a direction coincident with, or at least parallel to, the axis of rotation 8 of the spindle 18 and the pin tool 22 .
- roller arrangement 26 for controlling the depth of penetration of the pin tool during stir-friction welding or hot working is effective, but the roller apparatus makes it inconvenient to change the penetration depth from one workpiece to another, and it is not possible to make small adjustments in the depth of penetration during a weld or hot-working procedure.
- Another prior-art method which can be used to control the depth of penetration of a stir-friction pin tool into a workpiece is by the use of distance measuring devices or sensors (not illustrated) which measure the distance between the upper surface of the workpiece, corresponding to surface 14 us in FIG. 1 , and a reference point on the spindle holding structure.
- Sensors which might be used in such a prior-art arrangement include laser systems and linear variable differential transformers (LVDTs).
- the sensor signal can be compared with a reference value representing the desired depth of penetration, and the spindle can be moved up or down, in the absence of rollers such as 26 a , in the direction of double-headed arrow 26 of FIG. 1 , in response to deviation of the measured position from the calculated position.
- This technique provides easy change of depth of penetration, by simply adjusting the signal representing the desired penetration, but is subject to error due to the large number of dimensions which must be added and subtracted in order to arrive at the calculated value, and because of axial position variation or changes due to slack in the spindle bearings, and similar tolerances.
- a method according to the invention for stir-friction welding a planar workpiece uses a rotating pin tool which includes a pin or ligament.
- the pin or ligament defines a diameter at locations closer to the tip of the pin tool than a particular location along its length, and also includes or defines a shoulder at the location.
- the shoulder has a larger diameter than the pin.
- the method includes the steps of rotating the tool, and applying force to the pin tool with the pin tool plunged into one side of the workpiece, and with the shoulder essentially coincident with the surface of the one side of the workpiece, so that the rotating pin creates a friction-stirred region.
- the workpiece and the rotating tool are moved laterally (in a direction orthogonal to the axis of rotation) relative to each other, so that the friction-stirred region progresses along the workpiece.
- a signal is generated which is representative of the force applied to the pin tool.
- a reference signal is generated which is representative of that force which is sufficient to maintain the shoulder against the one surface of the workpiece.
- the signal representative of the force applied to the pin tool is compared with the reference signal, for generating an error signal representative of the difference between the force applied to the pin tool and the reference signal.
- the error signal is used to control the step of applying force in a manner tending to maintain the shoulder in contact with, or essentially coplanar with, the one surface of the workpiece, as a result of which, or whereby, the pin maintains substantially constant plunge depth.
- the step of applying force includes the steps of coupling a lead screw to the pin tool and to a fixed reference point, so that rotation of the lead screw applies pressure or force to the pin tool.
- the shaft of a force motor is coupled to the lead screw, for rotating the lead screw in response to rotation of the force motor, as a result of which, or whereby, the force applied to the pin tool is responsive to the rotational position of the shaft of the force motor.
- the shaft of the force motor is rotated in response to at least the magnitude of the error signal, and preferably in opposite rotational directions in response to the variation of the error signal relative to a particular value of the error signal, which is preferably a zero value.
- the maximum force which can be applied to the pin tool is limited.
- the method according to the invention may further include initial steps which cause the pin tool to plunge into the workpiece. These steps include positioning the tip of the pin tool adjacent the one surface of the workpiece, and generating a signal representing the plunge of the pin tool relative to the one surface of the workpiece. Other steps include generating a monotonically changing signal which represents a profile of the desired depth of plunge as a function of time, generating a difference signal representing the difference between the actual plunge of the pin tool and the desired depth of plunge, rotating the pin tool, and controlling the force in response to the difference signal in such a manner that the force increases when the actual plunge is less than the desired plunge, and decreases when the actual plunge is more than the desired plunge.
- the step of moving the workpiece and the rotating tool laterally relative to each other begins when the actual plunge equals the desired plunge.
- FIG. 1 is a simplified diagram illustrating a prior-art stir-friction technique using rollers to properly locate the rotating pin tool within the workpiece;
- FIG. 2 is a simplified diagram similar to FIG. 1 , illustrating a pin tool in accordance with the invention, which includes a shoulder designed to ride on the upper surface of the workpiece;
- FIG. 3 is a perspective or isometric view of a tool with a shoulder, separately from the spindle;
- FIG. 4 is a simplified diagram illustrating how axial pressure may be applied to the pin tool according to one aspect of the invention
- FIG. 5 a is a side elevation view of a pin tool according to an aspect of the invention
- FIG. 5 b is a plot of force or pressure for incremental penetration at a depth of penetration corresponding to the position along the tool of FIG. 5 a;
- FIG. 6 is a simplified diagram of a feedback control loop according to an aspect of the invention, suitable for use in the arrangement of FIG. 4 ;
- FIG. 7 is a plot of reference signal versus time for use in the arrangement of FIG. 6 according to an aspect of the invention.
- FIG. 8 is a simplified diagram similar to FIG. 4 , including a distance measuring device
- FIG. 9 is a simplified diagram of a feedback control system using the distance measurement to aid in generating the control signal.
- FIG. 10 is a dimensioned illustration of one embodiment of the pin tool in accordance with an aspect of the invention.
- FIG. 2 is a simplified diagram, similar to FIG. 1 , showing a pin tool 222 which includes a ligament 22 having a diameter d at locations away from the rounded tip, and also including a shoulder portion 224 having a larger diameter D than the diameter d of the ligament portion 22 .
- the shoulder portion 224 rides on the upper surface 14 us of the workpiece 14 during operation, and the length of the ligament 22 in relation to the intended depth of hot-working or welding is selected to approximately equal the pin-tip-to-shoulder distance.
- the distance between the pin tip 28 and shoulder 224 in FIG. 2 is about equal to the depth of hot-working or welding.
- FIG. 3 illustrates the pin tool 222 of FIG. 2 separate from the spindle 18 .
- the pin tool 222 includes a shank 310 in addition to the shoulder portion 224 and pin or ligament 22 .
- the grooves cut into the pin support in FIG. 3 are for ______.
- FIG. 4 is a simplified diagram illustrating one method for applying force to the pin tool in accordance with an aspect of the invention.
- a fixed frame or housing 410 defines an aperture 412 for accommodating and supporting a first bearing 414 , and also defines a second mounting region 416 , to which a load cell 418 is mounted.
- Load cell 418 is a device which transduces force or pressure into electrical signals, which are available on a signal conductor set 420 .
- Load cell 418 supports a bearing holder 422 , which holds a bearing 424 .
- a threaded shaft or lead screw 430 extends between bearings 414 and 424 , and is rotatable about its axis 408 .
- a first motor 450 is connected to a gear or worm 451 which engages lead screw 430 , for, when the motor is energized, driving lead screw 430 to rotate around its axis 408 .
- a mounting or head 440 is mounted in a movable fashion, and is mechanically coupled to the threads of lead screw 430 by a pair of threaded bosses or travelling nuts 440 1 and 440 2 .
- Head 440 is controllably driven in the directions of arrow 46 by rotation of lead screw 430 .
- rotation of motor 450 in a first direction results in linear motion of head 440 in a first direction
- rotation of motor 450 in a second direction results in linear motion of head 440 in a second direction.
- Motor 450 is energized with electrical power transmitted over conductor set 452 .
- a computer or processor (PROC) 460 produces appropriate control signals, which are amplified by a power amplifier illustrated as 454 before application by way of conductors 452 to motor 450 .
- Processor 460 receives load-cell signals over conductor set 420 , and processes the signals as described in more detail below, to control the position of head 440 and its pin tool 222 .
- Head 440 of FIG. 4 supports shaft or spindle 18 on a pair of bearings 441 a and 441 b .
- Spindle 18 is affixed to a circumferential gear 442 .
- a spur gear 444 driven by a second or spindle motor 446 engages circumferential gear 442 , and drives the spindle with a rotary motion in response to energization of motor.
- spindle motor 446 is driven with a constant velocity, while lead-screw motor 450 is driven in response to signals from load cell 418 .
- the workpiece 14 has its upper surface adjacent to shoulder 224 of the pin tool 222 .
- Workpiece 14 is mounted on anvil 12 , and anvil 12 has a rack gear 472 on its underside.
- Rack gear 472 is driven by a gear 474 which is, in turn, driven by a third or workpiece motion motor 470 .
- FIG. 5 a illustrates details of the shoulder 224
- FIG. 5 b illustrates as a plot 500 the relative force tending to resist the plunging of the rotating tool 222 into a workpiece, plotted against the position or plunge depth of the pin tool 22
- the shoulder 224 is not absolutely flat, but is slightly cone-shaped or tapered, in such a manner that the outer edges of the shoulder 524 r , as measured from the axis 28 of rotation, are slightly behind (more distant from) the inner or leading portion 524 , as measured from the tip 28 .
- 5 b can be interpreted by noting that at the moment at which the tip 28 of pin tool 22 comes into contact with the workpiece, corresponding to position 510 of FIGS. 5 a and 5 b , the force is at or near zero.
- the force represented by plot 500 increases, and eventually reaches a level A.
- the level A is reached as the plunge depth is such as to bring the upper surface of the workpiece to the position indicated as 512 . Further plunging of the tool 222 into the workpiece, represented by those positions between position 512 and 514 of FIG.
- the maximum force C illustrated in plot 500 represents a condition in which the upper surface 14 u of the workpiece 14 is even with outer portion 524 r of the shoulder 224 at its maximum radius from the axis 28 .
- the actual pressure exerted on the underlying material of the workpiece may differ from the force illustrated, because in the range between penetrations 510 and 512 , and between 514 and 516 , the area of contact is increasing at a rate greater than the rate of increase of the force. Thus, the forces and the pressures may not track each other exactly in these plots.
- FIG. 6 is a simplified diagram of a feedback control arrangement, which may be implemented by processor 460 of FIG. 4 , for control of lead-screw motor 450 in such a manner as to tend to maintain constant pressure or force on the pin tool 222 .
- processor 460 includes a source of signal 610 which represents the desired pressure or force which is to be applied to the pin tool.
- the signal representing the desired pressure or force is applied to the noninverting (+) input port of a summing circuit 612 .
- Summing circuit also receives at an inverting ( ⁇ ) input port a signal representing the actual force applied to the load cell 418 .
- the force applied to the load cell 418 is the reaction force arising from the force applied by the lead screw 430 to the head 440 to drive the head, and the pin tool with it, toward the workpiece 14 .
- Summing circuit 612 acts as an error signal generator, and subtracts the actual-pressure or actual-force signal from the desired-pressure or desired-force signal, to thereby produce an error signal.
- the error signal is applied to control the lead-screw motor 450 in a bidirectional manner.
- the motor is connected by way of mechanical elements, illustrated as a block 614 , to the load cell 418 . The connections as described in conjunction with FIG.
- the target pressure or force is selected to be that pressure or force represented by B of FIG. 5 b , which corresponds to the corner 501 , where there is a marked change from a relatively low rate of increase of force or pressure to a relatively high rate of increase as a function of penetration depth.
- This selection makes it easy for moderate pressures or forces (those lying between A and B of FIG. 5 b ) to cause penetration to depth 510 , but any error in the feedback which gives a value of error signal greater than that required to reach depth 510 results in a relatively small additional penetration.
- FIGS. 4 and 6 may tend to apply forces larger than desired to the pin tool at the beginning of penetration, before the pin tool has reached its full operating depth.
- the reference signal source 610 of FIG. 6 produces a ramp voltage at initial start-up, which ramps from zero to the desired value, and then remains at the desired maximum value.
- FIG. 7 is a plot 710 of reference signal versus time according to this aspect of the invention. In plot 710 , the amplitude of the error signal ramps from zero value at zero time to the desired steady-state value at a time t1, and remains at the steady-state value thereafter (or until a new plunge is undertaken).
- FIG. 8 is a simplified illustration of a stir friction hot-working or welding arrangement similar to that of FIG. 4 , but including a measuring device or sensor in the form of a linear variable differential transformer (LVDT) 710 , which produces signals on a signal path 712 for application to the controller 460 .
- FIG. 9 is a simplified block diagram of the control system of the arrangement of FIG. 8 . Elements of FIG. 9 corresponding to those of FIG. 6 are designated by like reference numerals.
- motion of the pin tool caused by movement of motor 450 is coupled to LVDT 710 , which produces a signal representing pin tool position relative to the surface.
- the position signals are applied to an encoder 912 , which may be as simple as a differentiator, for determining the rate of change of position.
- the rate of change of position signal is applied to a modulator or multiplier 910 , which couples more or less of the pressure error signal from error detector 612 to the motor, depending upon the rate of change signal. The purpose of this arrangement is to prevent application of excessive force to the pin tool during initial penetration, which might damage the system.
- a method according to an aspect of the invention for stir-friction hot-working or welding a planar workpiece ( 14 ) uses a rotating pin tool ( 22 ) which includes a pin or ligament defining a diameter at locations closer to the tip of the pin tool ( 22 ) than at a particular location along its length, and also including or defining a shoulder ( 224 ) at the location.
- the shoulder ( 224 ) has a larger diameter (D) than the pin diameter (d).
- the method includes the steps of rotating the tool, and applying pressure or force to the pin tool ( 22 ) with the pin tool ( 22 ) plunged into one side ( 14 us ) of the workpiece ( 14 ), and with at least a portion ( 524 ) of the shoulder ( 224 ) essentially coincident with the surface ( 14 us ) of the one side of the workpiece ( 14 ), so that the rotating pin creates a friction-stirred region.
- the workpiece ( 14 ) and the rotating tool ( 22 ) are moved laterally (in a direction orthogonal to the axis of rotation) relative to each other (by motor 470 , rack 472 and gear 474 ), so that the friction-stirred region ( 14 b ) progresses along the workpiece ( 14 ).
- a signal is generated, which is representative of the pressure or force applied to the pin tool ( 22 ).
- a reference signal is generated (block 610 ) which is representative of that force (B) which is sufficient to maintain the shoulder ( 224 ) against the one surface ( 14 us ) of the workpiece ( 14 ).
- the signal representative of the force applied to the pin tool ( 22 ) is compared (in error signal generator 612 ) with the reference signal, for generating an error signal representative of the difference between the force applied to the pin tool ( 22 ) and the force represented by the reference signal.
- the error signal is used to control the step of applying force in a manner tending to maintain the shoulder ( 224 ) in contact with, or essentially coplanar with, the one surface of the workpiece ( 14 ), as a result of which, or whereby, the pin maintains substantially constant plunge depth.
- the step of applying force includes the steps of coupling a lead screw ( 430 ) to the pin tool ( 22 ) and to a fixed reference point ( 410 ), so that rotation of the lead screw ( 430 ) applies pressure or force to the pin tool ( 22 ).
- the shaft of a force or lead-screw motor ( 450 ) is coupled (by gear 451 ) to the lead screw ( 430 ), for rotating the lead screw ( 430 ) in response to rotation of the force or lead-screw motor ( 450 ), as a result of which, or whereby, the pressure or force applied to the pin tool ( 22 ) is responsive to the rotational position of the force motor ( 450 ) shaft ( 450 s ).
- the shaft ( 450 s ) of the force motor ( 450 ) is rotated in response to at least the magnitude of the error signal (generated by error signal generator 612 ), and preferably in opposite rotational directions in response to the variation of the error signal relative to a particular value of the error signal, which is preferably a zero value.
- the maximum pressure or force which can be applied to the pin tool ( 22 ) is limited.
- the method according to the invention may further include initial steps which cause the pin tool ( 22 ) to plunge into the workpiece ( 14 ). These steps include positioning the tip of the pin tool ( 22 ) adjacent the one surface of the workpiece ( 14 ), and generating a signal representing the plunge of the pin tool ( 22 ) relative to the one surface of the workpiece ( 14 ).
- Other steps include generating a monotonically changing signal which represents a profile of the desired depth of plunge as a function of time, generating a difference signal representing the difference between the actual plunge of the pin tool ( 22 ) and the desired depth of plunge, rotating the pin tool ( 22 ), and controlling the force in response to the difference signal in such a manner that the force increases when the actual plunge is less than the desired plunge, and decreases when the actual plunge is more than the desired plunge.
- the step of moving the workpiece ( 14 ) and the rotating tool laterally relative to each other begins when the actual plunge equals the desired plunge.
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Abstract
A stir-friction hot-working or welding arrangement uses a pin tool having a ligament 22 and a shoulder 224. The force required for incremental penetration increases markedly when the shoulder is reached. A control system for maintaining a set penetration depth includes a load cell for measuring force or pressure applied to the pin tool. The control system compares a reference signal representing the desired force with the actual force from the load cell, to produce an error signal which controls the penetration force, thereby tending to maintain a desired penetration depth. In a particular embodiment, the reference signal ramps up from a low or zero value at turn-on, to reduce forces applied upon initial penetration. In another embodiment, position signals are used to control a modulator or multiplier, which changes the error signal applied at certain positions of penetration, or at certain velocities of penetration.
Description
- This invention relates to control arrangements for stir-friction welders, and more particularly to automatic positioning systems for stir-friction welders.
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FIG. 1 is a simplified illustration of a prior-art stir-friction welding arrangement 10. InFIG. 1 , ananvil 12 supports aflat workpiece 14, illustrated in phantom to make other portions of the arrangement more obvious. A friction-stir pin tool and spindle arrangement designated generally as 16 includes aspindle 18 which rotates about itsaxis 8, carrying with it a pin tool orligament holding arrangement 20. The pin tool itself includes an elongated pin orligament 22, which also rotates in consonance with the rotatingspindle 18. As thespindle 18,holder 20, andpin tool 22 rotate, a relative motion is introduced between the anvil 12 (carrying the workpiece 14) and the spindle-and-pin-tool arrangement 16. The motion is represented by anarrow 24, which suggests movement of the spindle-and-pin-tool to the right inFIG. 1 , assuming that theanvil 12 andworkpiece 14 remain fixed. As a consequence of the friction resulting from the rotation of thepin tool 22 within theworkpiece 14, that portion of the workpiece near thepin tool 22 is heated and becomes plastic. The relative motion represented byarrow 24 indicates that theportion 14 a ofworkpiece 14, which lies to the right ofpin tool 22 inFIG. 1 , has not yet been welded or hot worked, while thatportion 14 b ofworkpiece 14, which lies to the left of thepin tool 22, has already been hot-worked, as suggested by the dashed hatching. Those skilled in the stir-friction hot working arts know that the described motion results in a line weld or hot working of the workpiece. - In order to make appropriate welds, the pin tool or
ligament 22 ofFIG. 1 must be maintained at a depth which provides full hot working of the desired region of the workpiece. The depth of plunge of thepin tool 22 is the depth to which thetip 28 of thepin tool 22 extends below theupper surface 14 us, which is the surface from which the pin tool is introduced into the workpiece. The depth of plunge cannot be such that thetip 28 ofpin tool 22 extends beyond the second orlower surface 14 of the workpiece, because this might weld theworkpiece 14 to theanvil 12, or might damage the workpiece or pin tool. In U.S. patent application Ser. No. 09/006,915, the position of the pin tool is maintained at the appropriate level by aset 26 of rollers, only one of which, namely roller 26 a, is illustrated. Roller 26 a is affixed by ashaft 26 to the spindle or tool holder, and rotates therewith, bearing on theupper surface 14 us of theworkpiece 14. The position of thetip 28 of thepin tool 22 in this prior-art arrangement extends below (or beyond) the lower rolling surface of the rollers by the desired penetration of the workpiece. The penetration of the workpiece may be termed “axial” penetration, because the penetration is in a direction coincident with, or at least parallel to, the axis ofrotation 8 of thespindle 18 and thepin tool 22. - The
roller arrangement 26 for controlling the depth of penetration of the pin tool during stir-friction welding or hot working is effective, but the roller apparatus makes it inconvenient to change the penetration depth from one workpiece to another, and it is not possible to make small adjustments in the depth of penetration during a weld or hot-working procedure. - Another prior-art method which can be used to control the depth of penetration of a stir-friction pin tool into a workpiece is by the use of distance measuring devices or sensors (not illustrated) which measure the distance between the upper surface of the workpiece, corresponding to
surface 14 us inFIG. 1 , and a reference point on the spindle holding structure. Sensors which might be used in such a prior-art arrangement include laser systems and linear variable differential transformers (LVDTs). The sensor signal can be compared with a reference value representing the desired depth of penetration, and the spindle can be moved up or down, in the absence of rollers such as 26 a, in the direction of double-headed arrow 26 ofFIG. 1 , in response to deviation of the measured position from the calculated position. This technique provides easy change of depth of penetration, by simply adjusting the signal representing the desired penetration, but is subject to error due to the large number of dimensions which must be added and subtracted in order to arrive at the calculated value, and because of axial position variation or changes due to slack in the spindle bearings, and similar tolerances. - Improved control arrangements are desired for stir friction welding.
- A method according to the invention for stir-friction welding a planar workpiece uses a rotating pin tool which includes a pin or ligament. The pin or ligament defines a diameter at locations closer to the tip of the pin tool than a particular location along its length, and also includes or defines a shoulder at the location. The shoulder has a larger diameter than the pin. The method includes the steps of rotating the tool, and applying force to the pin tool with the pin tool plunged into one side of the workpiece, and with the shoulder essentially coincident with the surface of the one side of the workpiece, so that the rotating pin creates a friction-stirred region. According to an aspect of a method according to the invention, the workpiece and the rotating tool are moved laterally (in a direction orthogonal to the axis of rotation) relative to each other, so that the friction-stirred region progresses along the workpiece. During the moving step, a signal is generated which is representative of the force applied to the pin tool. A reference signal is generated which is representative of that force which is sufficient to maintain the shoulder against the one surface of the workpiece. The signal representative of the force applied to the pin tool is compared with the reference signal, for generating an error signal representative of the difference between the force applied to the pin tool and the reference signal. The error signal is used to control the step of applying force in a manner tending to maintain the shoulder in contact with, or essentially coplanar with, the one surface of the workpiece, as a result of which, or whereby, the pin maintains substantially constant plunge depth.
- In a particularly advantageous mode of practicing a method according to the invention, the step of applying force includes the steps of coupling a lead screw to the pin tool and to a fixed reference point, so that rotation of the lead screw applies pressure or force to the pin tool. The shaft of a force motor is coupled to the lead screw, for rotating the lead screw in response to rotation of the force motor, as a result of which, or whereby, the force applied to the pin tool is responsive to the rotational position of the shaft of the force motor. The shaft of the force motor is rotated in response to at least the magnitude of the error signal, and preferably in opposite rotational directions in response to the variation of the error signal relative to a particular value of the error signal, which is preferably a zero value. In a most preferred embodiment of the invention, the maximum force which can be applied to the pin tool is limited.
- The method according to the invention may further include initial steps which cause the pin tool to plunge into the workpiece. These steps include positioning the tip of the pin tool adjacent the one surface of the workpiece, and generating a signal representing the plunge of the pin tool relative to the one surface of the workpiece. Other steps include generating a monotonically changing signal which represents a profile of the desired depth of plunge as a function of time, generating a difference signal representing the difference between the actual plunge of the pin tool and the desired depth of plunge, rotating the pin tool, and controlling the force in response to the difference signal in such a manner that the force increases when the actual plunge is less than the desired plunge, and decreases when the actual plunge is more than the desired plunge. The step of moving the workpiece and the rotating tool laterally relative to each other begins when the actual plunge equals the desired plunge.
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FIG. 1 is a simplified diagram illustrating a prior-art stir-friction technique using rollers to properly locate the rotating pin tool within the workpiece; -
FIG. 2 is a simplified diagram similar toFIG. 1 , illustrating a pin tool in accordance with the invention, which includes a shoulder designed to ride on the upper surface of the workpiece; -
FIG. 3 is a perspective or isometric view of a tool with a shoulder, separately from the spindle; -
FIG. 4 is a simplified diagram illustrating how axial pressure may be applied to the pin tool according to one aspect of the invention; -
FIG. 5 a is a side elevation view of a pin tool according to an aspect of the invention, andFIG. 5 b is a plot of force or pressure for incremental penetration at a depth of penetration corresponding to the position along the tool ofFIG. 5 a; -
FIG. 6 is a simplified diagram of a feedback control loop according to an aspect of the invention, suitable for use in the arrangement ofFIG. 4 ; -
FIG. 7 is a plot of reference signal versus time for use in the arrangement ofFIG. 6 according to an aspect of the invention; -
FIG. 8 is a simplified diagram similar toFIG. 4 , including a distance measuring device; -
FIG. 9 is a simplified diagram of a feedback control system using the distance measurement to aid in generating the control signal; and -
FIG. 10 is a dimensioned illustration of one embodiment of the pin tool in accordance with an aspect of the invention. -
FIG. 2 is a simplified diagram, similar toFIG. 1 , showing apin tool 222 which includes aligament 22 having a diameter d at locations away from the rounded tip, and also including ashoulder portion 224 having a larger diameter D than the diameter d of theligament portion 22. As illustrated inFIG. 2 , theshoulder portion 224 rides on theupper surface 14 us of theworkpiece 14 during operation, and the length of theligament 22 in relation to the intended depth of hot-working or welding is selected to approximately equal the pin-tip-to-shoulder distance. Thus, the distance between thepin tip 28 andshoulder 224 inFIG. 2 is about equal to the depth of hot-working or welding. -
FIG. 3 illustrates thepin tool 222 ofFIG. 2 separate from thespindle 18. As illustrated inFIG. 3 , thepin tool 222 includes ashank 310 in addition to theshoulder portion 224 and pin orligament 22. The grooves cut into the pin support inFIG. 3 are for ______. -
FIG. 4 is a simplified diagram illustrating one method for applying force to the pin tool in accordance with an aspect of the invention. InFIG. 4 , a fixed frame orhousing 410 defines anaperture 412 for accommodating and supporting afirst bearing 414, and also defines asecond mounting region 416, to which aload cell 418 is mounted.Load cell 418 is a device which transduces force or pressure into electrical signals, which are available on a signal conductor set 420.Load cell 418 supports abearing holder 422, which holds abearing 424. A threaded shaft orlead screw 430 extends betweenbearings axis 408. Afirst motor 450 is connected to a gear orworm 451 which engageslead screw 430, for, when the motor is energized, drivinglead screw 430 to rotate around itsaxis 408. A mounting orhead 440 is mounted in a movable fashion, and is mechanically coupled to the threads oflead screw 430 by a pair of threaded bosses or travellingnuts Head 440 is controllably driven in the directions of arrow 46 by rotation oflead screw 430. Thus, rotation ofmotor 450 in a first direction results in linear motion ofhead 440 in a first direction, and rotation ofmotor 450 in a second direction results in linear motion ofhead 440 in a second direction.Motor 450 is energized with electrical power transmitted over conductor set 452. A computer or processor (PROC) 460 produces appropriate control signals, which are amplified by a power amplifier illustrated as 454 before application by way ofconductors 452 tomotor 450.Processor 460 receives load-cell signals over conductor set 420, and processes the signals as described in more detail below, to control the position ofhead 440 and itspin tool 222. - It should be noted that pressure divided by area equals force, so they are not identical measures. However, with a constant-area system, force and pressure are proportional, and they are often used interchangeably.
-
Head 440 ofFIG. 4 supports shaft orspindle 18 on a pair ofbearings Spindle 18 is affixed to acircumferential gear 442. Aspur gear 444 driven by a second orspindle motor 446 engagescircumferential gear 442, and drives the spindle with a rotary motion in response to energization of motor. During operation of the apparatus ofFIG. 4 ,spindle motor 446 is driven with a constant velocity, while lead-screw motor 450 is driven in response to signals fromload cell 418. - As illustrated in
FIG. 4 , theworkpiece 14 has its upper surface adjacent to shoulder 224 of thepin tool 222.Workpiece 14 is mounted onanvil 12, andanvil 12 has arack gear 472 on its underside.Rack gear 472 is driven by agear 474 which is, in turn, driven by a third orworkpiece motion motor 470. -
FIG. 5 a illustrates details of theshoulder 224, andFIG. 5 b illustrates as aplot 500 the relative force tending to resist the plunging of therotating tool 222 into a workpiece, plotted against the position or plunge depth of thepin tool 22, As can be seen inFIG. 5 a, theshoulder 224 is not absolutely flat, but is slightly cone-shaped or tapered, in such a manner that the outer edges of theshoulder 524 r, as measured from theaxis 28 of rotation, are slightly behind (more distant from) the inner or leadingportion 524, as measured from thetip 28. Theplot 500 ofFIG. 5 b can be interpreted by noting that at the moment at which thetip 28 ofpin tool 22 comes into contact with the workpiece, corresponding to position 510 ofFIGS. 5 a and 5 b, the force is at or near zero. As the pin tool is plunged through the material of the workpiece so that the tapered tip portion 28 t of the pin tool enters the material of the workpiece, the force represented byplot 500 increases, and eventually reaches a level A. The level A is reached as the plunge depth is such as to bring the upper surface of the workpiece to the position indicated as 512. Further plunging of thetool 222 into the workpiece, represented by those positions between position 512 and 514 of FIG. S, cause a slight increase in the force necessary to produce further penetration, because a portion of the cylindrical portion of the pin tool lies within the workpiece, and its sides are in contact with workpiece, and tend to resist axial motion. At some level of penetration, illustrated as level 516, the upper surface 14 u of the workpiece begins to contact theleading edge 524 ofshoulder 224, and the force required for further penetration increases sharply. The corner is designated 501, and the corresponding force is designated B. The maximum force C illustrated inplot 500 represents a condition in which the upper surface 14 u of theworkpiece 14 is even withouter portion 524 r of theshoulder 224 at its maximum radius from theaxis 28. - It should be understood that in the
plot 500 ofFIG. 5 b, the actual pressure exerted on the underlying material of the workpiece may differ from the force illustrated, because in the range between penetrations 510 and 512, and between 514 and 516, the area of contact is increasing at a rate greater than the rate of increase of the force. Thus, the forces and the pressures may not track each other exactly in these plots. - Considering the characteristics of
plot 500 ofFIG. 5 b, it will be understood that the plotted forces tending to resist further penetration of the rotating pin tool increase in a monotonic manner with increasing penetration, although with different slopes for different penetrations.FIG. 6 is a simplified diagram of a feedback control arrangement, which may be implemented byprocessor 460 ofFIG. 4 , for control of lead-screw motor 450 in such a manner as to tend to maintain constant pressure or force on thepin tool 222. InFIG. 6 ,processor 460 includes a source ofsignal 610 which represents the desired pressure or force which is to be applied to the pin tool. The signal representing the desired pressure or force is applied to the noninverting (+) input port of a summingcircuit 612. Summing circuit also receives at an inverting (−) input port a signal representing the actual force applied to theload cell 418. The force applied to theload cell 418 is the reaction force arising from the force applied by thelead screw 430 to thehead 440 to drive the head, and the pin tool with it, toward theworkpiece 14. Summingcircuit 612 acts as an error signal generator, and subtracts the actual-pressure or actual-force signal from the desired-pressure or desired-force signal, to thereby produce an error signal. The error signal is applied to control the lead-screw motor 450 in a bidirectional manner. The motor is connected by way of mechanical elements, illustrated as ablock 614, to theload cell 418. The connections as described in conjunction withFIG. 6 , together with the mechanical arrangements discussed in conjunction withFIG. 4 , make it clear to those skilled in the art that the system as so far described constitutes a degenerative feedback loop which tends to maintain the desired pressure or force on the pin tool. The pressure or force applied to the pin tool by the feedback arrangement can readily be changed by simply changing the reference signal produced byblock 610. - The feedback arrangement as described in conjunction with
FIGS. 4 and 6 tends to maintain the pressure or force on thespindle 18 and thepin tool 22 at a constant, selected target level. According to an aspect of the invention, the target pressure or force is selected to be that pressure or force represented by B ofFIG. 5 b, which corresponds to thecorner 501, where there is a marked change from a relatively low rate of increase of force or pressure to a relatively high rate of increase as a function of penetration depth. This selection makes it easy for moderate pressures or forces (those lying between A and B ofFIG. 5 b) to cause penetration to depth 510, but any error in the feedback which gives a value of error signal greater than that required to reach depth 510 results in a relatively small additional penetration. - The arrangement of
FIGS. 4 and 6 may tend to apply forces larger than desired to the pin tool at the beginning of penetration, before the pin tool has reached its full operating depth. According to an aspect of the invention, thereference signal source 610 ofFIG. 6 produces a ramp voltage at initial start-up, which ramps from zero to the desired value, and then remains at the desired maximum value.FIG. 7 is aplot 710 of reference signal versus time according to this aspect of the invention. Inplot 710, the amplitude of the error signal ramps from zero value at zero time to the desired steady-state value at a time t1, and remains at the steady-state value thereafter (or until a new plunge is undertaken). -
FIG. 8 is a simplified illustration of a stir friction hot-working or welding arrangement similar to that ofFIG. 4 , but including a measuring device or sensor in the form of a linear variable differential transformer (LVDT) 710, which produces signals on asignal path 712 for application to thecontroller 460.FIG. 9 is a simplified block diagram of the control system of the arrangement ofFIG. 8 . Elements ofFIG. 9 corresponding to those ofFIG. 6 are designated by like reference numerals. InFIG. 9 , motion of the pin tool caused by movement ofmotor 450 is coupled toLVDT 710, which produces a signal representing pin tool position relative to the surface. The position signals are applied to an encoder 912, which may be as simple as a differentiator, for determining the rate of change of position. The rate of change of position signal is applied to a modulator ormultiplier 910, which couples more or less of the pressure error signal fromerror detector 612 to the motor, depending upon the rate of change signal. The purpose of this arrangement is to prevent application of excessive force to the pin tool during initial penetration, which might damage the system. - Other embodiments of the invention will be apparent to those skilled in the art. For example, while a general-purpose computer processor has been described as controlling the feedback, a dedicated processor could also be used, and might even be advantageous, by virtue of simplicity and reliability. While the term “motor” has been used to describe a transducer from electricity to mechanical energy, other devices than a conventional rotary motor may be used, as for example piezoelectric or magnetic devices, or linear motors. While the feedback loops have shown simple feedback schemes, but many types of feedback control may be used, including proportional-integral-derivative (PID) control.
- Thus, a method according to an aspect of the invention for stir-friction hot-working or welding a planar workpiece (14) uses a rotating pin tool (22) which includes a pin or ligament defining a diameter at locations closer to the tip of the pin tool (22) than at a particular location along its length, and also including or defining a shoulder (224) at the location. The shoulder (224) has a larger diameter (D) than the pin diameter (d). The method includes the steps of rotating the tool, and applying pressure or force to the pin tool (22) with the pin tool (22) plunged into one side (14 us) of the workpiece (14), and with at least a portion (524) of the shoulder (224) essentially coincident with the surface (14 us) of the one side of the workpiece (14), so that the rotating pin creates a friction-stirred region. According to an aspect of a method according to the invention, the workpiece (14) and the rotating tool (22) are moved laterally (in a direction orthogonal to the axis of rotation) relative to each other (by
motor 470,rack 472 and gear 474), so that the friction-stirred region (14 b) progresses along the workpiece (14). During the moving step, a signal is generated, which is representative of the pressure or force applied to the pin tool (22). A reference signal is generated (block 610) which is representative of that force (B) which is sufficient to maintain the shoulder (224) against the one surface (14 us) of the workpiece (14). The signal representative of the force applied to the pin tool (22) is compared (in error signal generator 612) with the reference signal, for generating an error signal representative of the difference between the force applied to the pin tool (22) and the force represented by the reference signal. The error signal is used to control the step of applying force in a manner tending to maintain the shoulder (224) in contact with, or essentially coplanar with, the one surface of the workpiece (14), as a result of which, or whereby, the pin maintains substantially constant plunge depth. - In a particularly advantageous mode of practicing a method according to the invention, the step of applying force includes the steps of coupling a lead screw (430) to the pin tool (22) and to a fixed reference point (410), so that rotation of the lead screw (430) applies pressure or force to the pin tool (22). The shaft of a force or lead-screw motor (450) is coupled (by gear 451) to the lead screw (430), for rotating the lead screw (430) in response to rotation of the force or lead-screw motor (450), as a result of which, or whereby, the pressure or force applied to the pin tool (22) is responsive to the rotational position of the force motor (450) shaft (450 s). The shaft (450 s) of the force motor (450) is rotated in response to at least the magnitude of the error signal (generated by error signal generator 612), and preferably in opposite rotational directions in response to the variation of the error signal relative to a particular value of the error signal, which is preferably a zero value. In a most preferred embodiment of the invention, the maximum pressure or force which can be applied to the pin tool (22) is limited.
- The method according to the invention may further include initial steps which cause the pin tool (22) to plunge into the workpiece (14). These steps include positioning the tip of the pin tool (22) adjacent the one surface of the workpiece (14), and generating a signal representing the plunge of the pin tool (22) relative to the one surface of the workpiece (14). Other steps include generating a monotonically changing signal which represents a profile of the desired depth of plunge as a function of time, generating a difference signal representing the difference between the actual plunge of the pin tool (22) and the desired depth of plunge, rotating the pin tool (22), and controlling the force in response to the difference signal in such a manner that the force increases when the actual plunge is less than the desired plunge, and decreases when the actual plunge is more than the desired plunge. The step of moving the workpiece (14) and the rotating tool laterally relative to each other begins when the actual plunge equals the desired plunge.
Claims (10)
1-8. (Canceled)
9. A stir-friction welder, comprising:
a frame;
a lead screw rotatably interconnected with said frame;
a first drive interconnected with said lead screw;
a first sensor located between said frame and said lead screw;
a controller interconnected with said first sensor and said first drive;
a head mounted on said lead screw; and
a pin tool interconnected with said head, wherein rotation of said lead screw by said first drive, responsive to an input by said first sensor to said controller, changes a position of said head along said lead screw, and thereby a plunge depth of said pin tool relative to a workpiece.
10. A stir-friction welder, as claimed in claim 9 , wherein:
said first sensor is a load cell.
11. A stir-friction welder, as claimed in claim 9 , further comprising:
a bearing holder and a bearing mounted in said bearing holder, wherein said lead screw is rotatably supported by said bearing, wherein said first sensor interfaces with said bearing holder.
12. A stir-friction welder, as claimed in claim 9 , wherein:
said head comprises a second drive interconnected with pin tool, wherein said second drive rotates said pin tool relative to the workpiece.
13. A stir-friction welder, comprising:
a frame;
a lead screw rotatably interconnected with said frame;
a first drive interconnected with said lead screw;
a first sensor that is stationary;
a controller interconnected with said first sensor and said first drive;
a head mounted on said lead screw; and
a pin tool interconnected with said head, wherein rotation of said lead screw by said first drive, responsive to an input by said first sensor to said controller, changes a position of said head along said lead screw, and thereby a plunge depth of said pin tool relative to a workpiece.
14. A stir-friction welder, as claimed in claim 13 , wherein:
said first sensor is located between said frame and said lead screw.
15. A stir-friction welder, as claimed in claim 13 , wherein:
said first sensor is a load cell.
16. A stir-friction welder, as claimed in claim 13 , further comprising:
a bearing holder and a bearing mounted in said bearing holder, wherein said lead screw is rotatably supported by said bearing, wherein said first sensor interfaces with said bearing holder.
17. A stir-friction welder, as claimed in claim 13 , wherein:
said head comprises a second drive interconnected with pin tool, wherein said second drive rotates said pin tool relative to the workpiece.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US10/773,045 US20050006441A1 (en) | 1999-02-12 | 2004-02-05 | Stir-friction hot working control system |
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
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US09/249,680 US6421578B1 (en) | 1999-02-12 | 1999-02-12 | Stir-friction hot working control system |
US10/193,943 US20030028281A1 (en) | 1999-02-12 | 2002-07-12 | Stir-friction hot working control system |
US10/773,045 US20050006441A1 (en) | 1999-02-12 | 2004-02-05 | Stir-friction hot working control system |
Related Parent Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US10/193,943 Continuation US20030028281A1 (en) | 1999-02-12 | 2002-07-12 | Stir-friction hot working control system |
Publications (1)
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US20050006441A1 true US20050006441A1 (en) | 2005-01-13 |
Family
ID=22944529
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US09/249,680 Expired - Lifetime US6421578B1 (en) | 1999-02-12 | 1999-02-12 | Stir-friction hot working control system |
US10/193,943 Abandoned US20030028281A1 (en) | 1999-02-12 | 2002-07-12 | Stir-friction hot working control system |
US10/773,045 Abandoned US20050006441A1 (en) | 1999-02-12 | 2004-02-05 | Stir-friction hot working control system |
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US09/249,680 Expired - Lifetime US6421578B1 (en) | 1999-02-12 | 1999-02-12 | Stir-friction hot working control system |
US10/193,943 Abandoned US20030028281A1 (en) | 1999-02-12 | 2002-07-12 | Stir-friction hot working control system |
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Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4757932A (en) * | 1983-04-07 | 1988-07-19 | Rolls-Royce Plc | Control of friction and inertia welding processes |
US5460317A (en) * | 1991-12-06 | 1995-10-24 | The Welding Institute | Friction welding |
US5718366A (en) * | 1996-05-31 | 1998-02-17 | The Boeing Company | Friction stir welding tool for welding variable thickness workpieces |
US5893507A (en) * | 1997-08-07 | 1999-04-13 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Auto-adjustable pin tool for friction stir welding |
US6050475A (en) * | 1998-05-29 | 2000-04-18 | Mcdonnell Douglas Corporation | Method and apparatus for controlling downforce during friction stir welding |
US6139400A (en) * | 1997-04-22 | 2000-10-31 | Sony Corporation | Polishing system and method with polishing pad pressure adjustment |
US6199745B1 (en) * | 1998-07-09 | 2001-03-13 | Mts Systems Corporation | Welding head |
US6225767B1 (en) * | 1998-06-02 | 2001-05-01 | Emerson Electric Co. | Trajectory controller |
US6421578B1 (en) * | 1999-02-12 | 2002-07-16 | Lockheed Martin Corporation | Stir-friction hot working control system |
US6742696B2 (en) * | 2000-05-01 | 2004-06-01 | General Tool Company | Friction stir welding machine |
-
1999
- 1999-02-12 US US09/249,680 patent/US6421578B1/en not_active Expired - Lifetime
-
2002
- 2002-07-12 US US10/193,943 patent/US20030028281A1/en not_active Abandoned
-
2004
- 2004-02-05 US US10/773,045 patent/US20050006441A1/en not_active Abandoned
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4757932A (en) * | 1983-04-07 | 1988-07-19 | Rolls-Royce Plc | Control of friction and inertia welding processes |
US5460317A (en) * | 1991-12-06 | 1995-10-24 | The Welding Institute | Friction welding |
US5460317B1 (en) * | 1991-12-06 | 1997-12-09 | Welding Inst | Friction welding |
US5718366A (en) * | 1996-05-31 | 1998-02-17 | The Boeing Company | Friction stir welding tool for welding variable thickness workpieces |
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US6421578B1 (en) | 2002-07-16 |
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