CA1258687A - Assembly system for seamed articles - Google Patents

Assembly system for seamed articles

Info

Publication number
CA1258687A
CA1258687A CA000476008A CA476008A CA1258687A CA 1258687 A CA1258687 A CA 1258687A CA 000476008 A CA000476008 A CA 000476008A CA 476008 A CA476008 A CA 476008A CA 1258687 A CA1258687 A CA 1258687A
Authority
CA
Canada
Prior art keywords
selectively
region
curvilinear
limp
assembly
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
CA000476008A
Other languages
French (fr)
Inventor
Arthur Ciccolo
George A. Wood
Donald C. Fyler
Daniel E. Whitney
F. Keith Glick
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Charles Stark Draper Laboratory Inc
Original Assignee
Charles Stark Draper Laboratory Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Charles Stark Draper Laboratory Inc filed Critical Charles Stark Draper Laboratory Inc
Application granted granted Critical
Publication of CA1258687A publication Critical patent/CA1258687A/en
Expired legal-status Critical Current

Links

Classifications

    • DTEXTILES; PAPER
    • D05SEWING; EMBROIDERING; TUFTING
    • D05BSEWING
    • D05B33/00Devices incorporated in sewing machines for supplying or removing the work
    • DTEXTILES; PAPER
    • D05SEWING; EMBROIDERING; TUFTING
    • D05DINDEXING SCHEME ASSOCIATED WITH SUBCLASSES D05B AND D05C, RELATING TO SEWING, EMBROIDERING AND TUFTING
    • D05D2305/00Operations on the work before or after sewing
    • D05D2305/02Folding

Landscapes

  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Sewing Machines And Sewing (AREA)
  • Treatment Of Fiber Materials (AREA)
  • Air Bags (AREA)
  • Details Of Garments (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)

Abstract

ABSTRACT

A limp material handling system includes a manipulating apparatus for selectively manipulating one or more layers of limp materiel on a support table. Folding is accomplished by lifting a curvilinear region of the material, reshaping that lifted region as desired, and lowering that lifted region to a curvilinear region on the support table.
A seamed article assembly system incorporates the manipulating apparatus, a seam joining apparatus and a multiple parallel endless belt system for tactile presentation of the limp material to the seam joining apparatus. An optical sensing system provides information representative of the position of the limp material being handled. A programmable computer, or controller, coordinates and controls the operation of the manipulating apparatus, seam joining apparatus, belt assembly, and optical sensing system to provide automatic assembly of seamed articles.

Description

.~5~ 7 ASSEMBLY SYSTEM FOR SEAMED ARTICLES

REFERENCE TO RELATED APPLICATIONS
_ The subject matter of this application is related to that of U.S. Patent No. 4,401,044, entitled 5"5ystem and Method for Man~facturing Seamed Articles", and U.S. Patent No. 4,457,243 entitled "Automated Seamed Joining Apparatus", filed February 4, 1983, and U.S. Patent ~o. 4,512,269, entitled " Automated Assembly System For 10Seamed Articles", filed July l9, 1983.

BACKGROUND OF THE INVENTION

This invention relates to the assembly of seamed articles made from limp material, such as fabric. In particular, the invention relates to 15systems for automated, or computer-controlled, assembly of seamed articles from limp material~

Conventional assembly line manufacture of seamed articles constructed of limp fabric consists of a series of manually contxolled assembly operations.
20Generally tactile presentatiOn and control of the fabric-to-be-joined is made to the joining, or ~ewing, head under manual control. One drawback of this appli-cation technique is that the techniqu is labor intensive; tha~ is, a large portion of the cost or 25manufacture is spent on labor. To reduce cost, auto-mated or computer-controlled manufacturing techniques have been proposed in the prior art.

An automated approach to fabric presentation and control is disclosed in U.S. Patent No. 4,457,243.
As there disclosed, pairs of belt .1~5~ 7
-2-assemblies are positioned on either side of a planar fabric locus. The respective belt assemhlies are dri-ven to selectively provide relative motion along a reference axis to layers of fabric lying in the fabric 510cus. A joining, or sewing, head is adapted for motion adjacent to the abric locus along an axis per-pendicular to the reference axis. The respective belts maintain control of the limp fabric in the region tra-versed by the sewing head, with the respective belts lObeing selectively retracted, permitting passage there-between of the sewing head as it advances along its axis of motion. Wi~h this approach, control of the limp fabric is permitted in the regions which are to be joined.

Systems for the manufact~re of seamed articles from a strip of limp fabric disclosed in U.S.
Patent No. 4,512,269 provide more precise "near field" control of limp fabric, that is fabric control in regions clo~e to the sewing head.
20Those systems include a feeder for selactively feeding these strips of limp fabric in the direction of a first (Y) reference axis. Control of presentation may also be maintained in a second (X) axis perpendicular to and intersecting the Y axis.

In some forms, a folding apparatu~ controls the position of the fabric 60 ~hat the strip of fabric is folded onto itself along a fold axis offset from the axis of feed (Y axis) so that there is a folded portion having an upper layer overlying a lower layer. A sup-30port is used to position the upper and lower layers ofthe folded portion in a substantially planar fabric locus.

In one form of those systems, the support includes a frame member, a support assembly coupled to `:

~ 2 S~3~

the feeder, and a drive motor and an associated linkage for selectively positioning the frame member with respect to the support assembly in the direction of the X axis. A pair of lower belt assemblies is coupled to 5the frame member, where each lower belt assembly inclu-des a plurality of continuous loop lower belts underlying the fabric locus. The lower belts are adapted on their outer, uppermost surface for fric-tional coupling with the lower layer of the folded por lOtion. The lower belt assemblies are adjacently positioned along the X axis, with each assembly including an associated driver for ~electively driving the lower belts so that the lower fabric layer coupled to those belts is positionable in the direction of the 15X axis.

A pair of upper belt assemblies is coupled to the frame member as well. The upper belt assemblies are adapted to be positioned to overlie the lower belt assernblies. Each of the upper belt assemblies includes 20a plurality of upper belts (which may be positioned opposite the respective lower belts). The upper belts have planar lowermost portions spaced apart from the uppermost of the lower belts. The upper belts are adapted on their outer, lowermost surface for fric-25tional coupling with the upper layer of the folded por-tion. Each of the upper belt assemblies has an associated driver for selectively driving those upper belts so that the lower layer coupled to those belts is positionable in the direction of the X axis. The 30region between the lowermost portions of the upper belts and the uppermost portions of the lower belts defines the fabric locus, so that the fabric locus is substantially parallel to the plane formed by the intersecting X and Y axes.

In general, a computer-controller is used to selectively control the drivers for the respective ~ ~'3~ ~ ~'7 belts so ~hat the upper and lower layers may be substantially independently positioneA in the direction of the X axis along the fabric locus. In alternative for~s of those systems, the respective belt assemblies 5may be controllable in the Y axis direction as well, so that the upper and lower layers may be substantially indepsndently positioned in the direction of both the X
and Y axes along the fabric locus, thereby permitting control motion of the respective layers in those direc-lOtions.

A fabric joiner, or sewing head, includes anupper assembly and a lower assembly. These upper and lower assemblies are adapted for tandem motion along the direction parallel to the Y axis between the upper 15belt assemblies and the lower belt assemblies. An associated driver provides control of the position of the upper and lower assemblies of the joiner along its axis of motion. The joiner is selectively operable to orm seams in ~abric in the fabric locus under the 20control of a computer-controller.

In one form of the systems of those systems, at least one pair of the pairs of the adjacent belt assemblies includes opposing pairs of closed loop belts and an associated controller adapted 50 that the pairs 250f the closed loop belts are selectively rstractable in the X direction to permit passage of the joining head therebe~ween in ~he Y diracti~n, for example, in the manner disclosed in ~.S. Patent ~o. 4,457,243.

- 30 The joining head may include a needle assembly having a thread-carrying, elongated needle extending along a needle reference axi~ perpendicular to the ~abric locu~. In operationf the needle is driven through the fabric 10CUB in a reciprocal motion - - -1'~5~

aiong the needle reference axis. The need]e assembly f~rther includes an upper feed dog assembly which is responsive to an applied upper dog drive signal for selectively driving the uppermost layer of fabric in 5the region adjacent to the needle in the direction of an upper axis ~hich is perpendicular to the needle reference axis.

A bobbin assembly is generally used in those systems and is adapted for interaction with the needle loassembly to form the stitches of the seam. The bobbin assembly includes a lower feed dog assembly which is responsive to a lower dog drive signal for selectively driving the lowermost layer of fabric in the region adjacent to the needle in the direction of a lower axis 15which is perpendicular to the needle reference axis.

In one form of those systems, a controller generates a part assembly signal representative of the desired position of the junction of the layers of fabric relative to those layers. Registration sensors 20provide signals representative of the current position of the respective uppermost and lowermost fabric layers. A controller provides overall control for the belt assemblies as well as the feed dogs and needle and bobbin assembly rotational and feed dog control, in 25Order to achieve coordinated motions of the respective assemblies. With this configuration, the respective belt assemblies provide far field, or global, position control for the upper and lower fabric layers. The feed dogs provide near field, or local, position 30control for the upper and lower layers of fabric in the regions near the needle of the joining head~

While the above-referenced systems do effec-tiv21y provide approaches for the automated assembly of seamed articles, there are limitations in those opera-~S~
--6--tions, particularly regarding the positioning, orienting an~ folding of limp fabric in preparation for joining of seams. Further, automated assembly systems require a feedback control system in order to 5accomplish these preparatory operations. In all such operations, it is important that accurate and repeated edge positioning of fabric be achieved in order to assure uniform quality of garment assembly. Moreover, these aspects are particularly important in view of 10desired high volume, and in Vi2W of the prior art requirement of specialized assemblies, requiring pattern- and size- dependent clamps or fixtures.
Another factor for such automated assembly systems is that such systems must ~e cost effective compared with 15the existing approaches.

Accordingly, it is an object of the present in~ention to provide an improved system for automatic assembly o' seame~ articles.

An~ther object is to provide an improved 20automated assembly system for seamed articles including a relatively low cost optical feedback system controlling fabric location and orientation.

Yet another object is to provide an improved folding apparatus for folding fabric in automated 25seamed article assembly systems.

S~MMARY OF THE INVENTION

Briefly, the present invention is directed to a limp material handlin~ system including a manipu-lating system for selectively manipulating one or more 301ayers of limp material. The manipulating system includes a support assembly adapted to support the material on a reference surface. The manipulating system further includes a selectively operable fold asse~ly which includes a gripping apparatus for mecha-nically coupling to (or grapping or gripping) a cur-vilinear r~gion of at least an uppermost layer of smaterial on the support surface, anA an apparatus for contour controlling and positioning for that gripped region of material, and for releasing that gripped region. In forms of the inventon adapted for folding limp material, the fold assembly further includes lOapparatus for selectively lifting and lowering a gripped region of material, so that a lifted region may be lowered down to the reference surface or the next uppermost layer of material overlying that reference surfac2. The gripping and releasing apparatus, the 15contour controlling and positioning apparatus and the lifting and lowering apparatus are all selectively operable under control of a control a~paratus, which is generally controlled by a microcomputer in the pre-ferred forms of ~he invention.

Generally, the fold assembly is operative to grip a curvilinear region of the material, then to control the curvature of that gripped curvilinear region so that the region has a selected contour, and to selectively translate and rotate that gripped region 25to a selected location overlying an associated cur-vilinear region of the reference surface, and then the material is releasedO To fold the material, a lifting o~eration for the gripped region is interspersed with these operations. Then, that translated and/or rotated 30and/or reconfigured curvilinear region is lowered to the underlying associated curvilinear region of the reference surface, or onto material overlying that associated curvilinear reyion on the reference surface.

Particularly, in article assembly systems in 3saccordance with the invention, the system further l~S13~

inclu~es a seam joining apparatus, such as a sewing machine, which is selectively positioned along a reference axis. The seam joining apparatus is adapted to selectively join adjacent regions of one or more Slayers of the limp material elements passing through that reference axis. The assembly system urther includes a multiple parallel endless belt assembly, which is adapted to selectively transport and align the limp material in order to present that material to the lOseam joining apparatus at points on the first reference axis.

This belt assembly also provides selective orientation of the limp material elements to be joined.
The respective belts of the belt assembly are selec-15tively controllable to provide a desired tension in thelimp material elements in regions of the limp material adjacent to and including the first reference axis, so that seam joining occwr under controlled tension.
Furt'nermore, the belts may be selectively driven in 20~rder to reposition upper and lower layers of a multi-layer material at the sewing head in order to accomplish relative positioning of ~hose layers, and further to provide capability to achieve aasing and the generation of three dimensional seams.

All of these operations are provided under the control of an assembly controller which establishes the selected positioning, folding and joining of the limp material to assemble seamed articles.

In some forms of the invention, an optical 30sensing system provides optical feedback to the controller in order to sense the current position and various characteristics of the material which is being assembled into articles. The optical sensing system provides information representative o the edges of ~'~S~8~7 g such materials as well, so that the olding apparatus may ~perate to accomplish the desired manipulations and~or folds by controlling the positioning of the ed~es of the material in such a manner to achieve the 5desired manipulation and/or folding.

In one form of the invention, a particularly cost effective optical sensing system is provided by incorporating a television camera for generating video signals using a common axis illumination system. This 10configuration provides video signals representative of an image along the camera's optical axis of the reference surface and any limp material on that surface within the field of view of the camera. The reference surface provides a relatively high contrast optical 15reflectivity with respect to material positioned on that surface.

With this configuration, the article assembly system may construct seamed articles, such as garments, in a manner providing accurate and repeatable edge 20positioning, thereby leading to highly uniform quality of garment assembly. Particularly, ~he folding appara-tus is well adapted to attaching to the limp material, picking that edge up, reshaping that edge as desired, and moving it and placing it down elsewhere on the sur~
25face with substantially high accuracy. The reshaping of the edge permits matching to another edge of m2terial already on the surface, so that the overlying edges may be then joined to form a desired seam, thereby permitting joining of dissimilarly-shaped 30edges.

BRIEF DESCRIPTION OF THE DRAWINGS

The foregoing and other objects of this invention, the various features thereof, as we~l as the ~25~8'~

invention itself, may be more fully understood from the following description, when read together with the accompanying drawings in which:

Fig. 1 shows an isometric representation of 5the principal elements of an exemplary embodiment of the present invention;

Fig. 2 shows a partially cutaway view of a support table for the system of Fig. l;

Fig. 3 shows schematically the upper endless l0beltS of the system of Fig. l;

. Figs. 4A and 4B illustrate the operation of the retractable belts of the system of Fig. l;

Fig. 5 shows an isometric representation of an exemplary fabric folding system for use with the 15system of Fig. l;

Figs. 6A-6F illustrate the ~olding and sewing operations performed during the automated assembly of a sleeve by the system of Fig. l;

Fig. 7 illustrates the television camera and 200n-axis light source for the system of Fig. l; and Fig. 8 shows in block diagram form an e~:e:?.~?lary configuration for generating the position signals for use with the system in Fig~ 1.

~s~
--ll--_E_ _PTION OF T~IE PREFERRED F.MBODIMENT

Fig. 1 shows an isometric representation of principal elements of a preferred form of an assembly system 110 together with a set of intersecting 5reference coordinate axes X, Y and Z. The system 110 includes two support tables 112 and 114 and a seam joining assembly 116. The system 110 further includes an optical sensor system overlying table 112 and including a television camera 117 and a common-axis loillumination 5ystem 118. In alternative embodiments, an additional optical sensor system may similarly overlie table 114, for use in loading or unloading and orienting limp material elements, for example.

Each of the support tables 112 and 114 inclu-15des a respective one of planar upper surfaces 112a and114a. In alternative e~b~diments, other or both of the surfaces 112a and 114a may differ from planar. For example, those surfaces may be cylindrical about an axis parallel to the Y axis.

A set of parallel endless belts (120 an 122) is affixed to each of tables lI2 and 114. Each set of belts 120 and 122 is pivotable ahout a respective one of axes 120a and 122a each of which is parallel to the Y axis from a position substantially parallel to one of 25surfaces 112a and 114a (closed) to a position substan-tially perpendicular to one of those surfaces (open), In Fig. 1, belt set 120 is shown in a partially open position, and belt set 122 is shown in a closed posi-tion substantially parallel to the top surface 114a of 30table 114.

Fig. 2 shows a partially cutaway view of the support table 112. That support table 112 as shown includes a perforated retro-reflective surface which ~;~5~

forl~s the surface 112a. In the present embodiment, the surface ll~a is formed by retro-reflective material type for example as manufactured by 3~ Corporation, where that re~ro-reflective material forming the sur-5face 112a includes a rectangular array of holes, eachhole having a diameter equal to 1/32 inches, with the array having a center-to-center spacing of 1/16 inches.
In alternate embodiments, the array may be other than rectangular, for example, hexagonal or spiral or cir-lOcular with holes having a sufficient diameter and theadjacent holes of the array having center-to-center spacing appropriate to permit sufficient air mass flow therethrough to provide a suitable vacuum for holding limp material down to the surface. By the way of 15example, the array of holes in surface 112a may be established using a commercial laser.

In the presently described embodiments, the upper surface 112a overlies an aluminum plate having an array of holes which substantially matches the array of 20holes in the surface 112a. That aluminum plate 130 overlies a composite beam honeycomb table top 132 which includes an array of honeycomb tubular structures extending in the direction of the Z axis~ That honeycomb table top 132 is supported over a multiple 25plenum valve module which provides selectively operable rows of valves~ In Fig. 2, there are eight rows of valves shown, with six of those rows in the open posi-tion and two of those rows in the closed position. The valve module 134 is coupled to a vacuum blower 136 30which in turn is driven by a motor 138. With this con-figuration, a vacuum is selectively provided to various regions at surface 112a. The vacuum is particularly useful in holding various layers of material in a desired position on surface 112a. The positionin may 35 be accomplished by a material folding or by a material manipulator, for example. The surface 112a also has ~'~S~ 3'7 r~tro-reflective optical prope.rties so that with top lighting, reflectiv~ light is directed in the Z direc-tion tc provide a high contrast back.ground against any cloth object placed on surface 112a. The latter 5feature is particularly useful in systems having opti-cal sensors which can identify the location and orien-tation of material on surface 112a.

The sewing assembly 116 includes a sewing machine 140 adapted for linear motion along the Y axisO
lOThe sewing machine is also pivotable about its needle axis as driven by control 124 by way of motor 142 and gear assembly 144. The sewing assembly 116 urther includes an interlocking belt asselnbly including a first set of parallel endless belts 150 and a second 15set of parallel endless belts 152. The belts of sets 150 and 152 are adapted so that their lower surface may frictionally drive material between those lower sur-faces and an underlying support surface 160 which is generally in continuous with surfaces 112a and 114a, 20under the control of the controller 124.

Fig. 3 shows the belt assemblies 120 150, 152, and 122, in schematic form, together with the sewing machine 140, wherein the belt sets 150 and 152 include alternating sets of three roller endless belts 25and two point continuous belts. In operation, the controller 124 controls the belts adjacent to ~he sewing head of sewing machine 140 to be retracted from the locus of the needle while that needle is in the region between the belts. Otherwise, the belts of the 300pposed sets 150 and 152 are adjacent to each other.
The belts may be driven by controller 124 in a manner providing controlled fabric tension for fabric between the lower surface of the belts of sets 150 and 152 and the upper surface 158. In various embodiments of the 35invention, the surface 158 may also include multiple ~2~ 7 en~less belt assemblies underlying respective belts of sets 150 and 152. The latter belt sets are also controlled by the controller 124 in order to achieve substantially independent control of upper and lower slaYers of fabric positioned between the sets of belts 150 and 152 and those sets underlying sets 150 and 152.

By way of example, the belts may be 0.03 to 0.04 inches thick, 3/8 inch wide neoprene toothed timing belts with polyester fiber reinforcement sup-lOported by toothed roller assemblies. A layer ofpolyurethane foam is attached to the outer belt sur-faces with adhesive. With this configuration, the foam provide substantial frictional contact with material adjacent to the belts so that as the belt moves, it 15positions the fabric adjacent thereto in the corresponding manner. For the upper belts the layer is
3/8 inches thick and for the lower belts the layer is 1/4 inches thick. The thicker layer provides increased adapability for materials characterized by varying thicknPsses, ~ ig. 4A shows two interlocking belts of the sets 150 and 152, where the sewing machine head 140a is positioned other than between these two belts. Fig. 4B
shows those same interlocking belts when the sewing 25head 140a is positioned between those two belts 150a and 152a. With the present ernbodiment, as limp fabric to be sewn is adjustably positioned between the belts of sets of 150 and 152 and the surface 160, the sewing machine 140 may be selectively controlled to traverse 30the gaps established by the retracting belts along axis parallel to the Y axis of machine 140 so that selective stitching may be accomplished on that fabric, under the control of controller 124.

The system 110 further includes a material 35manipulation system for fabric on t~e support table 5~

112. That manipulation system includes the controller 1~4, and a folding assembly 160. ~he folding assembly 160 includes a controllable arm portion 162 which is selectively movable in the Z direction and selectively 5rotatable about the axis 170~ The folding assembly 160 includes a hinged, linearly segmented assembly 174.
That assembly includes three elongated segments 180, 182, and 184. Each of the segments 182 and 184 is selectively rotatable with respect to segment 180 about lOone of axes 190 and 192, so that the orientation of those segments 182 and 184 are selectively controlled with respect to the angular orientation of segment 180, all under the control of controller 124. The segment 180 is rotatable about the axis 186 under the control 15Of controller 124. Each of segments 180, 182 and 184 includes a plurality of gripping elements distributed along the principle axis of that segment.

The gripping elements are denoted in Fig. 1 by reference designation 180a, 182a and 184a. Each of 20the gripping ele,~ents is adapted for selectively gripping regions of any fabric underlying those ele-ments. The arm portion 162 is selectively controllable in the Z direction. As a result, when the gripping elaments are affixed to a portion of the material, that 25portion may be selectively lifted and then lowered (in the Z direction) with respect to the surface 112a. In the present embodiment, the elements 180a, 182a and 184a =r~ a;so each selectively movable in a direction parallel to the X-Y plane in the direction perpen-30dicular to the principle axes of the respective ones ofsegments 180, 182 and 184. The gripping elements 180a, 182a and 184a are also selectively rotatable about an axis 186~

With this configuration, the folding assembly 3~160 may be used as a material manipulator for material r~ i8~7 ~n surface 112a, whereby s~lective curvilinear por-ti~ns of that m~terial may be sequentially grabbed by the grippin~ elements, and then translated and/or rotated and/or reshaped, and then released. The folding 5asse~bly 160 may also be used as a material folder by selectively performing the operations described for the manipulator, interspersed with lifting and lowering operations, particularly as described in configuration Figs. 6A-6F.

In one form of the invention, each o the gripping elements may comprise a substantially tubular member coupling a vacuum thereto, which may be selec-tively applied. Alternatively, each of the gripping elements may include a grabber which comprises an 15elongated member extending along an axis perpendicular to the Z axis having a barb extending from the ti2 clo-ses~ to the surface 112a. In the latter embodiment~
the elongated member, or barbed needles, may be selec-tively reciprocated in the Z direction under the 20control of controller 124.

Fig. 5 shows an alternative embodiment 160' for the assembly 160 of Fig. 1. In that Fig. 5, corresponding elements are identified with identical reference designations. In Fig. 5, assembly 160 inclu-25des an elongated carrier assembly 210 having a cur-vilinear central axis 212 extending along its length.
Axis 212 is substantially parallel to surface 112a. In other embodiments, for example, where surface 112a is not planar, the axis 212 may not be parallel to surface 33112a. In ~he present embodiment, the carrier assembly 210 includes a hinged housing (including sections 214, 216 and 217~ and a 1exible member 218 which is coaxial with axis 212. One end of flexible member 218 is fixed to housing segment 214 at point 220 and the other end 3sis slidably coupled to housing segment 218 at point ~'~5~ 7 222~ Forcers 230 and 232 are adapted to applying trans~erse forces to member 218 at po.ints between the end points to control the curvature of axis 212. As the forcers 230 and 232 control the orientation of the 5axis 212, each of the gripping elements may be selec-tively displaced to provide the desired orientation of the gripping elements. I~is embodiment in effect pro-vides a cubic spline. In other embodiments, differing numbers of forcers may be used. In the assembly 160, lOflexible cubic (or higher order) splines may be used to position the gripping elements in any or all of segments 180, 182 and 184.

With either configuration 160 or 160', the gripping elements may be selectively driven to form a 15desired curvilinear contour over a portion of material on the table 112a. The ~ripping elements 180a, 182a and 184a may be selectively lowered to the material on the table 112a so that those gripping elements may be activated to couple to (or "grab") the material at a 20corresponding curvilinear region of at least an upper-most layer of the fabric on the surface 112a. To par-tially accomplish folding, the assembly 160 (or 160'~
may then be raised in the Z d.irection in a manner lifting that uppermost layer of the material.

The gripping elements may then be translated and/or rotated, and repositioned (to modify the cur-vature of axis 212) so that the grabbed region of the uppermost layer of material is repositioned to a selec-tive location overlying a predetermined location over 30the surface 112a. The assembly 160 ~or 160') may then be lowered so that the lifted material is adjacent to the surface 112a or overlying the material on surface on 112a. All of this operation is under the control of controller 124. The vacuum at surface 112a holds the 35material in position when that material is adapted to surface 112a.

~'~SB~

By selectively performing this operation over desired curvilinear regions of the material, a desired folding operation of the material may be attained.
Figs. 6~-6F show an exemplary folding sequence for 5assembling a sleeve. In that figure, a multilayer fabric assembly is first sewn (with easing) along the dotted line designated 240 in Fig. 6A. That assembly includes an in-sleeve portion 242 and an out-sleeve portion 244. Initially, the gripping elements 180a, 10182a and 184a may be positioned along the heavy lined portion of in-slee~e 242 denoted X in Fig. 6A. That contour may be then picked up and translated, reshaped and lowered (and held with vacuum at the surface 112) so that the contour X is reshaped and positioned at the 151Ocation shown in Fig. 6B. With this configuration, the in-sleeve portion 242 has been folded about the axis A-A. The elements 180a, 182a and 184a may then release the material and the gripping elements may be rearranged to match the contour denoted Y in Fig. 6B.
20That portion of the material may then be picked up by the gripping elements and the contour xeshaped so that it is then repositioned and shaped as shown in Fig. 6C, with contour X overlapping contour Y. As a result, the material assembly is then folded along line B-B. Then, 25contour Y is released and the elements 180a, 182a and 184a are controlled to grip the contour Z on portion 244 shown in Fig. 6C. That contour is then lifted and folded about line C-C as shown in Fig. 6D. Then con-tour Z is released and the gripping elements are con-30figured to grip contour W shown in Fig. 6D. Thatgripped contour is then folded about line D-D, as shown in Fig. 6E. The sleeve assembly is then presented to sewing head 140a.

By performing a tacking operation, the sewing 35head 140a as shown in Fig. 6F, the sleeve may be par-tially assembled. The material may then be translated .

ba~k out to the surface 112a, and the contour T ~f the out-sleeve ~44 may be lited by the assembly 160 lor 160') including elements 180a, 182a and 184a, and transferred and reconfigured to unfold about line C-C
5and match the contours X and Y as shown in Fig. 6F.
The out-sleeve is then released from elements 180a, 182a and 184a, and the folded assembly is then trans-ferred by way of belts 120 and 150 to the sewing head 140a, where the elbow seam 240 is then joined. Thus, lOwith this configuration, the sleeve shown in Fig. 6F is assembled automatically under the control of controller 124. In all of these operations, the vacuum at surface 112a serves to hold material adjacent to that surface in place.

Figs. 7 and 8 show the components of the optical sensor system of the present emboaiment. Fig.
7 includes an optical sensor 117, and an illumination system 118. In the present embodiment, the sensor 117 is in the form of a conventional television camera, 20althouyh other image signal generating devices may be used. The television camera 117 is supported so that its optical axis 117a is substantially normal to the surface 112a o the tabla 112. The illumination system 118 includes a light source 260 and an associated beam 25splitter 262. The beam splitter is positioned on the axis 117a between the camera 117 and 6urface 112a.
That beam splitter 262, for example a mirror type beam splitter, is adapted to receive incident light from the light source 260 along path 260a, reflect a portion of 30that light along optical axis 117a to the surface 112a, and then to pass a portion of light reflected from sur-face 112a (or material positioned on that surface) back along the axis 117a to the television camera 117.

With this illumination arrangement, common 35axis illumination is achieved for the system for use 125~ 7 with the r~tro-reflector configuration on surface 112a.
Th~ surface 112a may alternatively be formed by a translucen~ material which is backlit, or by a flu~rescent surface (with appropriate filters for 5camera 117), although the retro-reflective common axis illumination appr~ach is the preferred form for the present embodiment.

In operation, the camera 117 provides video signals representative of the image along the optical lOaxis 117a of the surface 112 and any material thereon.
The retro-reflective surface 112a in effect provide a high contrast background with respect to any material on surface 112.

At the controller 124, these video signals 15are processed to provide the position signals for use with the automatic seam joining and folding control portions of controller 1240 Fig. 8 shows a bl~ck diagram of a portion of controller 124 which performs this function, in conjunction with the surface 112a, 20camera 117, and illumination source 118 and a video monitor 266. In the present embodiment, the controller 124 includes a type LSI-11/23 microcomputer, manuac-tured by Digital Equipment Corporation, Maynard, Massachusetts~ Fig. 8 also shows the interface between 25the camera and illumination system and the LSI-11/23 computer.

In operation, the functional block of controller 124 in FigO B performs edge detection of the material against the background provided by surface 30112a. The edge detection is performed by differen-tiating, or thresholding, the video signal generated by the camera 117 as the camera scanning beam sweeps across the image, marking the times within the sweep at which there i5 a predetermined change in video signal , . - , ,.

~'~58~

intensity These vari~us "edge" times for each scan line are provided ~o the computer upon request. By way of e~ample, where the camera 117 is an RCA type TC1005/C49 camera, the image of the table may be 5scanned in two seconds, and the edge information pro-vided to the microcomputer, together with some data checks and fil~ering on the raw data. Also within this time frame, the microcomputer computes the area of a material element in the field of view, the center of lOthat area, and the angle the principal axis of that material with respect to the a reference axis on sur-face 112a. Appendices A and B show an exemplary technique for performing these data processing operations.

With this configuration, the television camera 117 provides an output signal from its video amplifier circuitry and uses a separately genera~ed vertical sweep signal generated by a digital-to-analog converter controlled by the microcomputer in controller 20124. With this arrangement, the D/A controlled ver-tical sweep provides capability to increase a number of scan lines and also to correct for non-linearity in a rela~ively inexpensive camera yokeO The timing and control portion of the controller 124 converts the 25event detectors put into a series of digital words that contain a time of the event and the scan line number in which the event occurred. With this type system, a relatively high degree of edge resolution can be achieved without requiring the conventional type pixel-30image processing approach, and associated substantialcomputation cost and time. In alternative embodiments of the invention, the overall seamed article assemblies system may be configured with conventional type optical sensing system, although at relatively high cost com-35pared with the particularly cost ef fective system shownin Figs~ 7 and 8.

The invention may be embodied in other speci-fic forms without departing from the spiri-t or essen-tial characteristics thereof. The present embodiments are therefore to be considered in all respects as 5illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all change w~ich come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein.

,r~ 37 APPENDIX A

Workpiece Recognition A. Sensor Information The camera scans the workpiece with respect to X-Y
5coordinates with the workpiece lying between X-coordinates O and XN with upper and lower limits XL and XH, respectively. Scan lines run parallel to Y-axis, separated by ~x. Scan information consists of y-values for background-fabric transitions in the y-lOdimension, ~here Yl is the left edge transition andY2 is the right edge transition in a scan lineD The distance between left edge and right edge transitions for the ith scan line, ~Yi, is equal to Y21-yli. The differential area for the ith scan line, dAi equals 15~Xi~Yi' or (Y2i-yli3 dx, or dydx.

B. Computation Area A= J¦dA

X2~ Y2(X3 = ¦ I dydx ~1 (X) XN
Jo [Y2(X3 - yl(x3] dx XN
~_o[~2~X~ - yl(x)]

= ~x ~ =0 ~i ~'~5~87 --2~--'`entroid xc- - ¦Ix dA

XN y2(x) - ~ J x dydx A ~0 Yl (x) X~
- l~ X[y2~x)-yllx)3dx A

~x XN
~ x[y2(x) - Yl(X)]
A X=O

~x N
= -- ~ Xi ~Yi A i=O

Centroid Yc = ~ ~y dA
A

XN y2(x) ,/' y dydx A O Yl(X) XN r y2 ~y2(x3~
- ~ _ ~ dx A ~0 2 Yl(X)J

:1 3N ~ y22(x) yl2(x)l dx ~I x XN
lD ~ Y22(x) ~ yl2(x)3 2A X=O

~x N
(y2~i - Y~li 2A i=O

5~

MomentIXX - ~Jy2 dA

XN Y2(X) ,f ~ y2 dydx O 'yl(X) N ~ Y3 ¦ Y2( o l3 Iyl(x)J

3 ~ ~ ~ y~ ] dx ~x XN
= -- ,~ [Y23(x) - yl3(x) ]
3 X=O

"~,x N 3 3 -- ~ (Y2i ~ ~li) 3 i=O

MomentIyy - JJX2 dA

XN Y2~X) r x2 dydx O *l(X) XN
= Oç; x2 [y2(x~-yl(x)] dx = ~ X2 ~y2(X) - yl(X)~
X-o ~X ~ X2i~yi ~ o 8~3'7 M~:~er~t I xy =J~XY dA

XN Y2(X) J r xy dydx ~1 (X) XN ~Y2 ¦ Y2~X~
J ~_2 ~Yl(X~d XN Y22~X) -- yl2(X)l dx = Jo X[--2----1 _ ~ x~y;~2(x) - ~12(x)]
2 X=O

~x N
- -- ~ Xi ~y22i - Y21i) 2 i=O

~51 3~3'7 C. Principal Axis with Respect to Centroid Coordinate Frame The next step is to convert the moments from the measurement into centroid frame, w~ich is parallel to 5the original frame, but offset by the coordinates of the computed centroid. The converted moments are:

xx = Ixx ~ ycA

Iyy = Iyy - xcA

Ixy = Ixy - XcycA

lo e tan 2 IXX - Iyy where a' corresponds to the angular offset ~f the worX-piece centroid with respect to the principal axes.

D. Algori m in BASIC

Below is shown all the BASIC language statements 15that are necessary to implement the "moment calculations". Only eigh~ multiplications and nine additions or subtractions are required in the high-frequency loop. YL and YR represent the values for the left and right profile, respectively, of the workpiece 20for each scan line.

la0 ~OR X = O TO XMAX STEP DX

200 READ YL, YR

. ,~

~25~

210 DY = YR - YL
220 YRSQ = YR * YR
230 YLSQ = YL * YL
240 DYSQ = YRSQ - YLSQ
250 YRCUB = YRSQ * YR
260 YLCUB = YLSQ * YL
2~0 300 SUMl = SUMl + DY
310 SUM2 = SUM2 ~ X * DY
320 SUM3 = SUM3 ~ DYSQ
330 SUM4 = SUM4 ~ YRCUB - YLCUB
340 SUM5 = SUM5 ~ X ~ X * DY
350 SUM6 = SUM6 ~ X * DYSQ

3~0 400 A = DX * SUMl ~10 XC = DX * SUM2/A
420 YC = DX * SUM3/(2 * A) ~30 440 IXX = DX ~ SUM4 / 3 450 IYY = DX * SUM5 460 IXY = DX ~ SUM6 /

480 IXX = IXX - YC * YC * A
490 IYY - IYY - XC * XC * A
500 IXY = IXY - XC * YC ~ A
510 Theta = O.5 * ATAN((-2*IXY)/(IXX-IYY)) APPENDIX B
Sleeve Data Base The following information forms the "data base" for the machine, before each sewing or folding operation, for each sleeve size and style. tOnly the right or 35left sleeve need be defined~:
1~ Nominal visual Area ~f workpiece ~A~

-2~-2. Reasonable Tolarance for computed area (~ A) 3. Centroid correction as function of area variation ( ~xc/~A ~ ~ yc/~A )
4. With respect to a "sleeve" coordinate system (i.e., origin at centroid, x-axis along longitudinal principal axis):

A. Checkpoints (e.g. to identify left-vs. right-hand piece, verify measure-ment - expected coordinates of intercept of centroid axes (~xc,Yc) and workpiece reasonable tolerance or any detected edge t-~x, ~ ~y~

B. Seam "trajectory"

- coordinates ~f first stitch ~eOg. off leading edgej - number of individual stitches - individual stitch segments - ~x, ~y from previous stitch -maximum sewing machine speed over se~ment -easing rate over segment ~standard material~
-gap stretching xate over segment (standard material) -feeddogs up-down flag -presser foot up-down fla~

C. Folding "trajectory"

The ~ransformation from "plotting" to "centroid" coor-., ~5~

~i~ates involves a (~c~YC) offset, followed by a rota-tion by angle 0:

- - r Cos~3 -sine ~
(X)C= r(x)p-(xcyc)]l ~
sine cO5e The transformation relationship for the stitch segments
5(Si - sj) is slightly different:

cOse -sine ~
(~S)c = ( ~s)p sine Cos~, To provide measurement and a First Reasonableness Test where both the workpiece and table coordinate frame visible within the camera field~o~-view, the scan lOalgorithm is as ollows:

1. For each scan line Yl, Y2~ Yn (n varies with shape~

-If (Y2 ryl) > ~ or (Yn~Yn-l)?~ or if (Y3 -Y2j~ ~ or (Yn-l~Yn-2)~ ~ then - increment a counter and use previous ~Yi -For j = 3 to n 2, step 2 -~Yi = ~Yi ~ (Yj~l ~ Yj) -Accumulate y' 5 for Area computation.

~s~

2. Compute ~rea as ~x ~ ~ Yi i=l 3. Compare Ameas with AD~ ~ ~ ADB

If not in interval, repeat measurement and increment counter. If counter is beyond a threshold, alert operator.

For each scan line, partial sums can be accumulated for the centroid and principal angle:

For i c 1 to N

-Accumulate (i ~x3 A Yi (For XC3 ~i -Accumulate (i~ X)2 ~yi (For Iyy) _ x2i -For j = 3 to n-2, step 2 -Accumulate (y2~ y2j) (For Yc) -Accumulate (y3 ~.
~ ) (For I

-Accumulate (i ~x) (Y j~l - y2;) (For Ixy) Using those par ial sums, the centroid and principle angle can easily be calculated using the algorithm described in Appendix A, that is:

N N n-2 xc = - ~ Xi Yi' Yc = 2- ~ ~~3 Y j+i Y
i=l i=l To provide a Second Reasonableness Test and Right- vs. Left-Piece identification, even if the detected area, centroid, and principal anqle seem reasonable, there may still be some ambiguity whether a lO"righthand" or "lefthand" piece was loaded and scanned.

Unless the piece is exactly symmetrical about its two principal axes, the four predic~ed x, y inter-cepts with the piece edges can be checked to 1) ascer-tain whether a righ~- or left-handed piece was loaded 15and 2) perform a final reasonableness test.
In the present form, only "mirror" loading about the piece longitudinal axis is allowed; i.e., only the y~ and y intercepts str used to determine whether a right- or left~handed piece was loaded. If 20t~e x+, x are not confirmed, the piece is rejected (or centroid corrected). Thus, the piece can not be loaded backwards.

125B~7 ~33-Also, i~ the predicted XC, Yc intercepts are "close" and consistent with a slightly larg~r or smaller area, the centroid and principal angle is adjusted slightly to allow for miscut pieces or unpre-5dictable manual folding variations.

An exemplary algorithm is as follows:

1. Determine if predictable intercepts y+, y can be confirmed with actual camera data.

a. convert the x-cornponents (in table coordinates) of y+ and y to a par-ticular scan line number (i.e.~

b. conver~ the y-components ~in table coordinates) Of y+ and y to a particular camera y-displacement (i.e., ~ y~ y ).

c, Look at the raw camera data (or repeat the scan) for a y~ value (i.e., table-piece transition) along scan line i~
and a y value along scan line i_. Use a reasonable y for success criterion.

d. If concurrence results, proceed to Step 2.
If not, swap y+ and y_ and repeat Steps la-lc (look for concurrence for mirror-image around x axis).

eO IE concurrence results from swapping the y's, then change the sign oE the y-component for all trajectory points (i.e., start-end of seam and y for each stitch).

f. If no concurrence again, then stop and inform operator.

~58~137 -3~-2. Repeat Steps la-lc for x~ and x . If concurrence, preceed to Step 3: if not, stop and inform operator.

3. Correck the trajectory for the small differences between predicted and measured intercept values, using one of the following rules:

a. Xc = Xc + ~XC/
Yc = Yc + ~Yc/ a ~ A
~ = 0 + a~ A

where ~/ a ~ A, etc. are empirical values from the data base.

Then use ~e new XC, Yc~ and e values to retransform the sewing/folding trajectory from centroid to table coordinates.

b. ~se the (X~(a~tual) ~ X~(predict)) value to correct all positive x-coordinates of trajectories ~i.e., beginning and ending of seams and folds, but not ~ x,~y of stitches), This, if the detected x+ point falls further from the centroid than the predicted x+ point, "expand" ~he beginning or end of the trajectory further away from ~he centroid in the ~x direction.

Repeat similarly for the -x, ~y, and -y direstions.

The last step prior to sewing is to transform the 30stitch trajectory from table into ~ewing module (control) coordinates.

.~t~s~ 7 It's preferred t~ define the x sewing axis as ori-ginating from the sewing gap so that the velocity of the workpiece may change as it crosses the gap, due to different main motor and stretching motor rates. In 50rder to simplify sewing "navigation" equations, - (X~S- -YTS) is subtracted from every non-stitch segment ~i.e., non x, y) coordinate of the tra-jectory. This converts the centroid and seam start-end points into sewing coordinates.

- The sewing translator is slewed to the y-coordinate of the start of the seam.

- Simultaneously, the belts (and workpiece3 are moved, continually keeping track of the x-coordinate of the centroid (or the first stitch~
in sewing coordinates as it decreases toward zero (approaches the needle).

(XC) sewing reaChes the value of (51(x3 _ Xc) table or (51(x~sewing) reaches zero~
(i.e., the start of the first stitch pas~es under the needle) r and/or the fabric is detected under the needle, then sewing com~ences by issuing ~x, ~ y commands to the belts and translator from the sewing trajectoryO

- The x-position of the centroid (or first stitch) is continually be updated, so that the piece can be brought back to the original position on the loading table (or taken to the proper position on the folding table) after sewing i5 completed.

- When the centroid (or first stitch) passes across the sewing gap, its speed is goverened by the main motor and the stretching motorO
.

. .
...,...,:, -. ~

Claims (14)

1. A limp material handling system, comprising:

a limp material manipulating system for selectively manipulating one or more layers of limp material, comprising:

A. a support assembly adapted to support said material on a reference surface, B. a fold assembly including selectively operable:

i. means for gripping a curvilinear region of at least an uppermost layer of said material, ii. means for:

(a) controlling the curvature of said gripped curvilinear region whereby said gripped curvilinear region has a selected contour, (b) selectively translating and selectively rotating said gripped curvilinear region to a selected location overlying an associated curvilinear region of said reference surface, and iii. means for releasing said gripped curvilinear region to said associated curvilinear region of said reference surface or the next uppermost layer of said material overlying said associated curvilinear region of said reference surface, and C. a controller including means for selectively controlling said fold assembly, and wherein said gripping means and said curvature modifying means include at least one elongated carrier assembly having a curvilinear central axis extending along its elongated length, including a plurality of gripping elements coupled to said carrier and fixedly positioned with respect to said central axis, said gripping elements being adapted for selectively gripping the regions of said material underlying said gripping elements and wherein said curvature modifying means further includes selectively operable curvature control means for controlling the curvature of said central axis.
2. A limp material handling system according to claim 1 wherein said carrier assembly includes an elongated housing and an elongated flexible member coaxial with said central axis and having one end affixed to said housing and its other end slidingly coupled to said housing, said flexible member including means for supporting said gripping elements, and wherein said carrier assembly further includes selectively operable means for applying forces to said flexible member in directions transverse to said central axis at two or more points between the ends of said flexible member whereby the curvature of said central axis is controlled.
3. A limp material handling system according to claim 2 wherein said fold assembly further includes selectively operable means for selectively lifting and selectively lowering said gripped curvilinear regions of said material.
4. A limp material handling system according to claim 1 wherein said gripping elements each comprise means for selectively coupling a vacuum to said material region underlying said element.
5. A limp material handling system according to claim 1 wherein said gripping elements each comprise a grabber means for selectively attaching to said material region underlying said grabber means.
6. A limp material system according to claim 5 wherein said grabber means comprises an elongated member extending along an axis perpendicular to the underlying portion of said reference surface and having a barb which extends transversely from the tip of said elongated member closest to the underlying portion of said surface, and further comprises means for selectively reciprocating said elongated member in the direction perpendicular to said reference surface.
7. A limp material handling system according to claim 1 wherein said fold assembly further includes selectively operable means for selectively lifting and selectively lowering said gripped curvilinear regions of said material.
8. A limp material handling system, comprising:

a limp material manipulating system for selectively manipulating one or more layers of limp material, comprising:

A. a support assembly adapted to support said material on a reference surface, B. a fold assembly including selectively operable:

i. means for gripping a curvilinear region of at least an uppermost layer of said material, ii. means for:

(a) controlling the curvature of said gripped curvilinear region whereby said gripped curvilinear region has a selected contour, (b) selectively translating and selectively rotating said gripped curvilinear region to a selected location overlying an associated curvilinear region of said reference surface, and iii. means for releasing said gripped curvilinear region to said associated curvilinear region of said reference surface or the next uppermost layer of said material overlying said associated curvilinear region of said reference surface, and C. a controller including means for selectively controlling said fold assembly, and wherein said gripping means and said curvature modifying means include a hinged, linearly segmented assembly, each segment being elongated and including a plurality of gripping elements positioned along the principle axis of said segment, said gripping elements being adapted for selectively gripping the regions of said material underlying said elements, and wherein said curvature modifying means further includes selectively operable means for orienting said segments to establish a predetermined segment-to-segment angular orientation.
9. A limp material handling system according to claim 8 wherein at least one of said segments includes a means for selectively offsetting the position of said gripping elements of said segment in the direction perpendicular to the direction of elongation of said segment and perpendicular to the normal to said reference surface.
10. A limp material handling system according to claim 9 wherein said fold assembly further includes selectively operable means for selectively lifting and selectively lowering said gripped curvilinear regions of said material.
11. A limp material handling system according to claim 8 wherein said gripping elements each comprise means foe selectively coupling a vacuum to said material region underlying said element.
12. A limp material handling system according to claim 8 wherein said gripping elements each comprise a grabber means for selectively attaching to said material region underlying said grabber means.
13. A limp material handling system according to claim 12 wherein said grabber means comprises an elongated member extending along an axis perpendicular to the underlying portion of said reference surface and having a barb which extends transversely from the tip of said elongated member closest to the underlying portion of said reference surface, and further comprises means for selectively reciprocating said elongated member in the direction perpendicular to said reference surface.
14. A limp material handling system according to claim 8 wherein said fold assembly further includes selectively operable means for selectively lifting and selectively lowering said gripped curvilinear regions of said material.
CA000476008A 1984-03-08 1985-03-07 Assembly system for seamed articles Expired CA1258687A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US84/00378 1984-03-08
PCT/US1984/000378 WO1985003956A1 (en) 1984-03-08 1984-03-08 Assembly system for seamed articles

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CA000476008A Expired CA1258687A (en) 1984-03-08 1985-03-07 Assembly system for seamed articles
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IT1234568B (en) * 1988-06-07 1992-05-20 Necchi Spa MACHINE FOR THE FEEDING AND SEWING OF OVERLAPPED FABRIC LAYERS
CN112609340B (en) * 2020-12-11 2022-03-04 合肥华丽纺织制品有限公司 Quilting table for quilting quilt and using method thereof

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BE754603A (en) * 1969-08-19 1971-01-18 Farah Mfg Co Inc APPLIED POCKET STITCHING MACHINE
FR2457920A1 (en) * 1979-05-29 1980-12-26 Anvar INSTALLATION FOR LINEAR PROCESSING OF A CURVED EDGE OF A FLEXIBLE WORKPIECE SUCH AS A TEXTILE WORKPIECE
US4435837A (en) * 1981-03-05 1984-03-06 President And Fellows Of Harvard College Pattern recognition and orientation system
DE3138364A1 (en) * 1981-09-26 1983-04-07 Männel, Friedrich, 7527 Kraichtal "METHOD FOR CONTROLLING AN EMBROIDERY MACHINE"
US4425858A (en) * 1982-02-26 1984-01-17 Amf Incorporated Means for processing sheets of material

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CA1258685A (en) 1989-08-22
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ATE37911T1 (en) 1988-10-15
DK513885A (en) 1985-11-07
CA1258684A (en) 1989-08-22

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