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l1l1US006198983B3(12)United States Patent(io)Thrash et al.(45)(54)TABLE-DRIVEN SOFTWAREARCHITECTURE FOR A STITCHINGSYSTEM(75)Inventors: Patrick J. Thrash, Huntington Beach;Jeffrey L. Miller, Hermosa Beach; KenPallas, Lakewood, all of CA (US);Robert C. Trank, Belvedere, IL (US);Rhoda Fox, Cherry Valley, IL (US);Mike Korte, Rockford, IL (US);Richard Codos, Warren, NJ (US);Alexandre Korolev, Scotch Plains, NJ(US); William Collan, Englishtown, NJ(US)(73)Assignee: McDonnell Douglas Corporation, St.Louis, MI (US)( * ) Notice:Subject to any disclaimer, the term of thispatent is extended or adjusted under 35U.S.C. 154(b) by 0 days.(21)Appl. No.: 08/995,843(22)Filed:Dec. 22, 1997Int. Cl? .D05C 5/02U.S. C1. .700/138; 7001136; 7001137;7001181; 7001182; 7001183; 1121470.05;1121475.18; 1121254(58) Field of Search . 7001137, 138,7001183, 182, 136, 181, 184; 1121470.05,281, 475.18, 475.01, 254, 470.13, 302,155. 475.08(51)(52)(56)References CitedU.S. PATENT DOCUMENTS3,312,184411967 Cash .11211181121470.133,515,080611970 Ramsey .3,765,349 * 1011973 Gerber .112125411212204,067,276111978 Mohilo et al. .4,092,938611978 Coughenour .11214571121470.024,104,976811978 Landau, Jr. .Patent No.:US 6,198,983 B1Date of Patent:Mar. 4 Maruyama et al. . 70011374,446,520511984 Shigeta et al. .70011374,481,507 1111984 Takuguchi et al. . 34016494,503,788311985 Giannuzzi et al. . 1121470.064,506,611112179311985 Parker et al. .4,702,185 * 1011987 Hanyu et al. . 1121121.144,776,291 10119884,786,343 11119884,798,152111989 Simons et al. . 1121470.051121470.014,815,404311989 Ellermann et al.11211034,825,784 * 511989 Nomoto .1121163711989 Kozuka et al. .4,843,986(List continued on next page.)OTHER PUBLICATIONSChen et al., A new generation of intelligent punching environment for computerized embroidery Tools with ArtificialIntelligence, Proceedings., Sixth International Conferenceon, pp. 692-695, 1994.*Carvalho et al., “Measurements And Feature Extraction InHigh-speed Sewing”, IEEE., pp. 961-966, 1997.*Primary Examiner-William GrantAssistant E x a m i n e r a c D i e u n e l Marc(74) Attorney, Agent, or Firm-Westerlund & Powell, P.C.;Robert A. Westerlund; Raymond H. J. Powell, Jr.(57)ABSTRACTNative code for a CNC stitching machine is generated bygenerating a geometry model of a preform; generating toolpaths from the geometry model, the tool paths includingstitching instructions for making stitches; and generatingadditional instructions indicating thickness values. Thethickness values are obtained from a lookup table. When thestitching machine runs the native code, it accesses a lookuptable to determine a thread tension value corresponding tothe thickness value. The stitching machine accesses anotherlookup table to determine a thread path geometry valuecorresponding to the thickness value.24 Claims, 7 Drawing Sheets44/36

US 6,198,983 B1Page 2U.S. PATENT 4411994511994811994811994Takagi et al. . 1121470.01Marrache et al. . 1121470.13Hulshoff et al.7001136Cahuzac et al.15614294281102Chess et al. .1121302Iimuro et al. .1121102.5Kurono et al. .7001138Hayakawa .7001137Shigeta et al. 1199651199671199681199610119961211997611999* c ited by examlinerShigeta .70011371121278Norrid .Kurono et al. .1121102.57001138Shigeta et al. .Mizuno et al. . 1121102.5Sugihara et al. . 1121470.06Monget et al.1561937001138Futamara et al. .7001182Dundorf .1121470.13Thrash et al.

U S . PatentMar. 6,2001US 6,198,983 B1Sheet 1 of 7STITCHING MACHINELGGG-1STAT10Nk L18MOTORGROUP22Y-71BOBBINMATERIAL SUPPORT TABLEFIG. 144FIG. 2r20/14fl12

U S . PatentMar. 6,2001Sheet 2 of 7FIG. 3US 6,198,983 B1

U S . PatentMar. 6,2001Sheet 3 of 7US 6,198,983 B1-----60FIG. 4

U S . PatentMar. 6,2001US 6,198,983 B1Sheet 4 of 7CONTROL STATIONJ-16COMPUTER MEMORYICNC FILE b 7 291sT L/UTOSOLENOIDSTOMOTORS1/0 CARD-//,MOTION CONTROLLERCARD86b 7 4 7ICONSOLEb 8 01PERIPHERALb 8 2flG.56

U S . PatentMar. 6,2001Sheet 5 of 7104-US 6,198,983 B1LOOK UP THREADPATH GEOMETRYVALUEGENERATE STEPPER1 0 6 MOTOR COMMANDFIG.6

U S . PatentMar. 6,2001Sheet 6 of 7US 6,198,983 B1212216-I ZONE202ICAD204CAMCANNEDCYCLES206M EDIT1POST661TENSION200// I210/LIBRARY1 1 SIMULATE I214\FIG.7THlCKNESS86

U S . PatentMar. 6,2001Sheet 7 of 7flG.8ICOMPUTER SYSTEM3024-1I-I ,34plPROCESSOR300-SIMULATOR210IFIG.9US 6,198,983 B1

US 6,198,983 B112TABLE-DRIVEN SOFTWAREARCHITECTURE FOR A STITCHINGSYSTEMmust constantly stop the stitching machine when a newregion is about to be stitched, adjust the thread tension andpossibly the thread path geometry, and restart the stitchingmachine. Of course, the CNC stitching machine has multiplestitching heads. At any given time, two or more stitchingheads might be stitching different regions having differentthicknesses. Whenever one of the stitching heads enters anew region, the stitching machine must stopped and thethread tension and perhaps the thread path geometry Of thehead entering the new region must be adjusted.Resulting is a large number of instances in which thestitching machine must be stopped, the thread tension andthread path geometry adjusted, and the stitching machinerestarted.Additionally, the 'perator mustwhen to stop themachine and make the adjustments, Or the Operator must beprompted to stop themachine and make the adjustments. Either way, the Operator must pay constant attentionwhile the wing preform is being stitched. That too isdifficult, considering the large number of stitches that mustbe made'Moreover, generating the code for the CNCtake a programmer thousands Of hours. NotmachineOnlygenerating the code take a long time, but itbe subject to human error.The mmd labor increases the time and cost of manufacturing the wing Preform, and it Potentially reduces damage tolerance. Based on the foregoing, it can be appreciatedthat there presently exists a need for a software architecturethat allows for complete operation, from path generation tocontrol of the stitching Process. As Will become apparenthereinafter, the present invention fulfills this need.This invention was made under contract no. NASI18862 awardedNASA. The Government has certainrights in this invention.sBACKGROUND OF THE INVENTIONThis invention relates to textile manufacturing, Morespecifically, this invention relates to a software architecture lofor a computer numerically controlled stitching system.Large aircraft structures such as wing covers are nowbeing fabricated from textile composites. The textile composites are attractive because of their potential for loweringthe cost of fabricating the large aircraft structures. Cuttingpieces of fabric and stitching the fabric pieces together havethe potential of being less expensive then cutting sheets ofaluminum, drilling holes in the aluminum sheets, removingexcess metal and assembling metal fasteners.20The wing cover can be made from a carbon-fiber textilecomposite. Sheets of knitted carbon-fiber fabric are cut outinto pieces having specified sizes and shapes. Fabric pieceshaving the size and shape of a wing are laid out first. Severalof these pieces are stacked to form the wing cover. Additional pieces are stacked to provide added strength in high 25stress areas. After the fabric pieces are arranged in theirproper positions, the pieces are stitched together to form awing preform. Secondary details such as spar caps, stringersand intercostals are then stitched onto the wing preform,Such a wing preform might have a thickness varying 30between 0.05 inches and 1.5 inches. The wing preform isquite large, and its surface is very complex, usually acompound contoured three-dimensional surface.SUMMARY OF THE INVENTIONThe stitched wing preform is transferred to an outer mold 35line tool that has the shape of an aircraft wing. Prior to theThe invention can be regarded as a method of using atransfer, a surface of the outer mold line tool is covered withcomputer to generate native code for a stitching machine.a congealed epoxy-resin. The tool and the stitched wingThe method comprises the steps of using the computer topreform are placed in an autoclave. Under high pressure andgenerate a geometry model; using the computer to generatetemperature, the resin is infused into the stitched preform 4o tool paths from the geometry model, the tool paths includingand cured. Resulting is a cured wing cover that is ready fora first plurality of instructions for making stitches; and usingthe computer to generate a second plurality of instructionsassembly into a final wing structure.F textile composite technology to be successfu , twoindicating thickness values. The instructions of the secondbarriers must be addressed: cost and damage tolerance,plurality are inserted between the instructions of the firstDamage tolerance is achieved by making high quality, 45 Plurality.closely-spaced stitches on the wing preform. The highThe invention can also be regarded as a computer systemquality, closely-spaced stitches add a third continuous colfor generating native code for a CNC stitching machine. Theumn of material to the wing preform. If thread tension is notsystem comprises means for generating a geometry model;means for generating tool paths from the geometry model,proper, a large number of stitches on the preform will not beof sufficient quality and will reduce the damage tolerance. so the tool paths including a first plurality of instructions forImproper thread path geometry might also degrade themaking stitches; a zone table for determining thicknessquality of the stitches and, therefore, reduce the damagevalues; and means for accessing the zone table to generatea second plurality of instructions indicating the thicknesstolerance.Even though the stitches are made by a stitching machinevalues. The instructions of the second plurality are insertedthat is computer numerically controlled ("CNC"), it is 5s between the instructions of the first Plurality.difficult to make stitches having the high quality required forThe invention can also be regarded as a method of usingthe wing preform. On a compound, contoured threea processor to automatically adjust thread tension in adimensional surface, thread tension and thread path geomstitching head of a stitching machine. The stitching headetry must be constantly adjusted for an exceedingly largeincludes a servo for setting the thread tension. The methodnumber of stitches. The CNC stitching machine might make 60 comprises the steps o f using the processor to access dataeight to ten stitches per inch, in rows that might be spacedindicating a thickness value; using the processor to deter0.1 inches to 0.5 inches apart, over a surface that might bemine a thread tension value corresponding to the thicknesslonger than forty feet and wider than eight feet. The totalvalue; and commanding the servo to the thread tensionnumber of stitching points on the wing preform mightvalue.exceed 1.5 million.65The invention can also be regarded as an article ofmanufacture comprising computer memory; and dataMuch manual labor is required. Because the wing preformhas many regions of differing thickness, a machine operatorencoded in the computer memory. The data includes instruc-

US 6,198,983 B334tions for instructing a computer to access a lookup table forthickness values, access thread tension values correspondingto the thicknesses values, and generate servo commandscorresponding to the thread tension values.FIGS. 2, 3 and 4 show the stitching head 18 in greaterdetail. The stitching head 18 includes a needle 24, a needlebar 26, and a needle drive mechanism 28 such as a slidercrank mechanism for vertically extending and rotating theneedle bar for positive and negative reciprocation of theneedle 24. The needle drive mechanism 28 is driven by amotor 30. A presser foot 32 applies pressure to the preformand guides the needle 24. A constant-velocity mechanism(not shown) allows the needle 24 to move relative to thepreform. If the stitching head 18 is being moved relative tothe preform at a fixed feedrate, the constant velocity mechanism effectively adjusts the velocity of the needle 24 withrespect to the preform, decreasing the relative velocity whenstitches are being made in thicker regions and increasing therelative velocity when stitches are being made in thinnerregions. The constant velocity mechanism could be a walking needle mechanism including springs that push againstthe needle 24 in the x- and y-directions. Or, the constantvelocity mechanism could be an active control for movingthe needle according to a predetermined profile. Constantvelocity could even be achieved by providing the needlewith flexibility.Thread 34 is drawn from a spool 36 and threaded throughan eye of the needle 24. Under control of the control station16, the motor group 22 positions the needle 24 over astitching point on the preform, and the needle 24 is plungedinto the preform. The bobbin 20, which is on the undersideof the preform, grabs the thread 32 and forms a loop. Theneedle 24 is withdrawn from the preform and, under controlof the control station 16, it is repositioned over the nextstitching point. Once again, the needle 24 is plunged into thepreform, the bobbin 20 grabs the thread 28, forms anotherloop, and also locks a stitch. The needle 24 is withdrawnfrom the preform and moved to the next stitching point. Thestitching process is repeated.In addition to reciprocating the needle 24, the stitchinghead 18 performs a number of automated functions. Thestitching head 18 includes a thread gripper 38 for holding thethread at the start of the stitching process and for facilitatingthread-cutting; a thread cutter 40 having a ceramic cuttingelement for automatically cutting the thread 34; and a needlecooler such as a venturi which expands a stream of pressurized air and a hose 42 for directing the expanded, cooledair onto the needle 24. The thread gripper 38, thread cutter40 and the needle cooler 42 can all be off-the-shelf components that are provided with servomechanisms for automaticcontrol by the control station 16.The stitching head 18 also includes a thread tensioningmechanism 44 for automatically adjusting the thread tension. The thread tensioning mechanism 44 includes a pair oftension discs 46 mounted on a shaft 50. A spring 52 biasesone tension disc 46 against the other to apply tension to thethread 24. Distance between the discs 46 is controlled by acam 54, which is rotated by a stepper motor 56. The threadtensioning mechanism 44 also includes a pneumatic cylinder58 that quickly separates the discs 46 to release threadtension.The thread tensioning mechanism 44 can be operated in aclosed loop mode, an open loop or a manual mode. When thethread tensioning mechanism 44 is operated in the closedloop mode, the stepper motor 56 is commanded to move toa position based on a value in a lookup table. The value inthe lookup table indicates a thread tension value based onthickness of the preform region being stitched. The threadtension value is compared to a measurement of the threadtension, and an error signal results when the thread tensionvalue does not equal the thread tension measurement. TheBRIEF DESCRIPTION OF THE DRAWINGSSThe above and other objects, features and advantages ofthe present invention will become apparent from the following detailed description taken in conjunction with the10accompanying drawings, in which:FIG. 1 is a block diagram of a stitching system includinga stitching machine and a control station;FIG. 2 is a perspective view of a stitching head for thestitching machine;1sFIG. 3 is a side view of the stitching head;FIG. 4 is a different side view of the stitching head;FIG. 5 is a block diagram of the control station;FIG. 6 is a flowchart of a method of operating the stitching20head;FIG. 7 is diagram of a software architecture for generatingcode for the stitching system;FIG. 8 is a schematic diagram of a preform havingvariable thickness; and2sFIG. 9 is a block diagram of a computer system forgenerating the code.DETAILED DESCRIPTION OF THEINVENTION30While the present invention is described herein withreference to the illustrative embodiments for particularapplications, it should be understood that the invention is notlimited thereto. Those having ordinary skill in the art andaccess to the teachings provided herein will recognize 3sadditional modifications, applications, and embodimentswithin the scope thereof and additional fields in which thepresent invention would be of significant utility.FIG. 1 shows an automated stitching system 10 includinga material support table 12, a stitching machine 14 and a 40control station 16. The material support table 12 provides asurface for supporting a preform. The surface of the materialsupport table 12 can be tailored to the desired shape of thepreform. For example, the material support table 12 canprovide a flat two-dimensional surface, a contoured three- 4sdimensional surface, or a compound, contoured threedimensional surface.The stitching machine 14 includes a stitching head 18 andbobbin 20 operable to make a plurality of stitches in thepreform. The stitching machine 14 further includes a motor sogroup 22 for moving the stitching head 18 and the bobbin 20with respect to the material support table 12. The motorgroup 22 includes a first servo-controlled motor for positioning the stitching head 18 with respect to an x-axis and asecond servo-controlled motor for positioning the stitching 5shead 18 with respect to a y-axis. The motor group 22 couldalso include a third servo-controlled motor for positioningthe stitching head 18 with respect to a z-axis and a fourthservo-controlled motor for positioning the stitching head 18with respect to a rotational c-axis. The third and fourth 60servo-controlled motors would allow the stitching machine14 to stitch a preform having a compound, contouredthree-dimensional surface. The motor group 22 also includesservo-controlled motors for moving the bobbin 20 synchronously with the stitching head 18. Of course, the motor 65group 22 could include additional servo-controlled motors ifadditional degrees of freedom are desired.

US 6,198,983 B165stepper motor 56 turns the cam 54, changing the distancemotion controller card 76 sends control signals to the stepperbetween the discs 46, until the error signal is nulled.or servo motors of the motor group 22. Or, the processor 66fetches an instruction for turning on needle cooling, andThe thread tension measurement can be derived from asignal generated by a load cell. Positioned in the thread pathsends a axmmd to the 110 card 74, which generates anear the needle 24, the load cell generates a raw signal that 5 control signal that open an air supply valve.is proportional to thread tension at or near the needle 24.The control station 16 further includes an operator console 80 including a display and keyboard for controlling theWhen the thread tensioning mechanism 44 is operated inthe open loop mode, the thread tension value is determinedstitching machine 14, viewing stitching data, and viewingstatus and health of the stitching machine 14. A peripheralfrom the lookup table, and a stepper motor commandcorresponding to the thread tension value is determined from lo device 82 such as a floppy disk drive, CD ROM drive or tapeanother lookup table. The stepper motor 56, in response todrive allows the host program 70 and the file 72 to be loadedinto the computer memory 68. In the alternative, the hostthe stepper motor command, rotates the cam 54, whichprogram 70, the file 72 could be downloaded from a netchanges the distance between the discs 46. The stepperwork. The file 72 could even be entered from the operatormotor 56 stays at the commanded position regardless of the15 console 80.measured tension in the thread 34.When the thread tensioning mechanism 44 is operated inThe processor 66 processes an instruction indicating thethe manual mode, thread tension is adjusted by hand-turningpreform thickness value by accessing a first lookup table 84a screw (not shown) on the discs 46. The pneumatic cylinderto determine proper tension for the corresponding preformthickness value. Then the processor 66 accesses a second58 can also be operated manually.The stitching head 18 also includes a mechanism 60 for 2o lookup table 86 to determine the CorresPonding stepperautomatically adjusting thread path geometry. The threadmotor count for the Proper tension. If the Processor 66 findspath geometry mechanism 60 includes an arm 62 having aan exact match for thread tension in the second lookup tablefirst end pivoted to the stitching head's housing and a second86, it uses the CorresPonding stepper motor count. If noend extending into the thread path, A stepper motor 64 ormatch is found, the processor 66 uses the closest values forthe arm 62 to increaseor decrease the thread 25 thread tension and interpolates a count for the stepper motorpath. The thread path is increased when additional thread is58 of the thread tensioning mechanism 44.needed for stitching through thicker regions, and the threadThe processor 66 also accesses the first lookup table 84 topath is decreased when less thread is needed for stitchingdetermine a count for the stepper motor 64 of the thread paththrough thinner regions. Although the mechanism 60 is 3o geometry mechanism 60.shown as having a pivoting arm 62, another mechanismThe first and second lookup tables 84 and 86 are stored incould have a sliding arm that moves linearly into the path ofthe computer memory 68. Exemplary entries for the first andsecond lookup tables 84 and 86 are shown in Tables 1 andthe thread 34. As with the thread tensioning mechanism 44,the thread path geometry mechanism 60 is table-driven. The2. Preform thickness values are indicated by a stack count.stepper motor 64 is commanded move to a position based on 35a stepper motor count in a lookup table. The stepper motorTABLE 1count in the lookup table corresponds to thread path geomThread Pathetry based on thickness of the preform region being stitched.StackThreadGeometryFIG. 5 shows the control station 16 in greater detail. TheCountTensionMotor Countcontrol station 16 includes a processor 66 and computer 4o175 g230memory 68. Encoded in the computer memory 68 is a host285 g300program 70 and a file 72 including instructions for makingthe stitches, instructions for controlling stitching speed, andinstructions for retracting and extending the stitching head18 to and from the preform. The file 72 also includes 45TABLE 2instructions for commanding the unique functions of theThreadstitching head 18 such as cooling the needle 24, gripping theThreadTensionthread 34, and cutting the thread 34. The instructions can beTensionMotor Countbased on an EIARS-274 format, which is a standard for the75 g300machine tool industry.so90 g37sThe file 72 further includes instructions indicating a valuefor thickness of the preform. The instructions indicating thepreform thickness values are processed by the control stationFIG. 6 shows a method of operating the stitching head 18.16 as described below to generate commands for adjustingThe host program 70 is executed and begins to instruct thethe thread path geometry and the thread tension.55 processor 66 to access the file 72 and fetch instructions (steploo). When an instruction indicating a preform thicknessThe processor 66 executes the host program 70, whichinstructs the processor 66 to fetch the instructions from thevalue is fetched (step 10% the Processor 66 automaticallyadjusts the thread tension and thread Path geometry in thefile 72. When an instruction is fetched, the processor 66stitching head 18. The processor 66 accesses the first lookupgenerates a command that is sent to an I / o card 74 or amotion controller card 76. When the I/O card 74 receives a 60 table 84 to determine the corresponding count for the steppercommand it generates a control signal having an appropriatemotor 64 of the thread Path geometry mechanism 60 (stepvoltage level for an actuator such as solenoid. When the104). The motion control card 76 generates a stepper motormotion controller card 76 receives a command, it generatesCOmmand (step 106), which causes the stepper motor 64 ofa control signal having a appropriate voltage level for anthe thread Path geometry mechanism 60 to move to theactuator such as a stepper motor. For example, the processor 65 stepper motor count.66 fetches an instruction for making a stitch, and sendsThe processor 66 also looks up a thread tension value inposition commands to the motion controller card 76. Thethe first lookup table 84 (step 108). If the open loop mode

US 6,198,983 B378is commanded (step llO), the processor 66 accesses thea series of polynomials describing the surface of the presecond lookup table 86 to determine the correspondingform. However, the neutral file format allows the file of thestepper motor count for the stepper motor 56 of the threadgeometric model to be processed by commercially availabletensioning mechanism 44 (step 112). The motion controlCAM software 204.card 76 generates a stepper motor command (step 114), 5Tool paths for the model are generated by the CAMwhich causes the stepper motor 56 of the thread tensioningmechanism 44 to move to the stepper motor count.software 204. Each tool path includes instructions for making the stitching points. The instructions are generatedIf the closed loop mode is commanded (step llO), theprocessor 48 does not access the second lookup table 86 butaccording to a standard format such as ANSI X3.37 forinstead generates an error signal indicating a difference lo Cutting Line Source data. At least one instruction is generbetween the thread tension measurement and the threadated for each stitching point.tension value from the first lookup table 84 (step 116). TheAdditional instructions are manually inserted into the toolerror signal is used to drive the stepper motor 56 of thepaths, between the instructions for making the stitches.thread tensioning mechanism 44 until the thread tensionmeasurement and the thread tension value are about the 15 Programmers use an editor 206 to manually edit the toolsame.paths and insert instructions for retracting and extending theWhen an instruction for making a stitch at a stitchingstitching head 18 and instructions for turning the stitching onpoint is fetched (step llS), the motion controller card 76and off. The programmers add these additional instructionsgenerates position commands for moving the stitching head 2o by working off the geometric model of the preform, iden18 to the x- and y-coordinates indicated in the stitchingtifying constraints on the tool paths, and inserting theinstruction (step 120). The position commands cause theappropriate instructions such that the constraints are notmotor group 22 to position the stitching head 18 over theviolated.For example, a programmer would trace the stitchstitching point. Once the stitching head 18 is positioned overing instructions on a tool path to a stringer, insert anthe stitching point, the processor 66 generates a commandthat causes the needle drive mechanism 28 to reciprocate the 25 instruction for retracting the stitching head 18 so as not to hitthe stringer, and insert an instruction for extending theneedle 24 (step 122).stitching head 18 on a trailing side of the stringer after theWhen an instruction for performing a unique function ofstitching head 18 clears the stringer. Working off the geothe stitching machine is fetched (step 124), the processor 66commands the stitching head 18 to perform the uniquemetric model of the preform, the programmers also manu30function (step 126). For example, the processor 66 fetches aally insert instructions for cutting and gripping the thread 34.command for cooling the needle 24. The I/O card 74, inInstead of cutting, the thread 34, the programmer mightresponse to the needle cooling instruction, sends a controldecide to drag the thread 34.signal commanding a valve to supply air to a venturi. CooledAfter the additional instructions have been added to theair flows from the venturi, through the hose 42, to the needle3s24.tool paths, the tool paths are supplied to a post-processorThe file 72 can also include instructions for performing208. The post-processor 208 converts the instructions in the“canned cycles.” In the alternative, a canned cycle might beANSI X3.37 format to native code that is readable by thecommanded from the operator console 80. If a canned cyclestitching machine 14. Accessing a user-defined library 210,is instructed from the file 72 or commanded from the 40 the post-processor 208 converts user-defined instructionsoperator console 80 (step 128), the processor 66 performs(e.g., needle cooling) into native code. The

I11111 111111ll111 Ill11 Ill11 IIIII IIIII IIIII IIIII IIIII IIIII 111ll1111111ll1111 US006198983B3 (12) United States Patent (io) Patent No.: US 6,198,983 B1 Thrash et al. (45) Date of Patent: Mar. 6,2001 (54) TABLE-DRIVEN SOFTWARE ARCHITECTURE FOR A STITCHINGCited by: 10Publish Year: 1997Author: Patrick J. Thrash, Jeffrey L. Miller, Ken Pallas, Robert C. Trank, Rho

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