US2545919A - Method of loading cops - Google Patents
Method of loading cops Download PDFInfo
- Publication number
- US2545919A US2545919A US781225A US78122547A US2545919A US 2545919 A US2545919 A US 2545919A US 781225 A US781225 A US 781225A US 78122547 A US78122547 A US 78122547A US 2545919 A US2545919 A US 2545919A
- Authority
- US
- United States
- Prior art keywords
- cop
- shuttle
- chamber
- thread
- cops
- 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 - Lifetime
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H54/00—Winding, coiling, or depositing filamentary material
- B65H54/02—Winding and traversing material on to reels, bobbins, tubes, or like package cores or formers
- B65H54/10—Winding and traversing material on to reels, bobbins, tubes, or like package cores or formers for making packages of specified shapes or on specified types of bobbins, tubes, cores, or formers
- B65H54/14—Winding and traversing material on to reels, bobbins, tubes, or like package cores or formers for making packages of specified shapes or on specified types of bobbins, tubes, cores, or formers on tubes, cores, or formers having generally parallel sides, e.g. cops or packages to be loaded into loom shuttles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H2701/00—Handled material; Storage means
- B65H2701/30—Handled filamentary material
- B65H2701/31—Textiles threads or artificial strands of filaments
Definitions
- This invention relates to a universally wound co-p suchas is used in the art of weaving and a method of adjusting the same in a shuttle, and more particularly to a coreless cop used in weaving textile fabrics woven fro-m twisted paper threads, as for example seat covering materials and summer rugs.
- - Coreless cops that is cops having an air space or air core have heretofore been wound in progressively overlapping layers extending for but a relatively small portion of the length of the cop.
- a cop sowound is'o-f' fixed'length and diameter and canonly be inserted in a shuttle for efiective use if said copdimensions-correspond substantially t'o'thedimensions of the shuttle chamber.
- One object of this invention is a coreless' or air core cop which will not break when subjected to either longitudinal tension or to lateral strain.
- Another object is a careless cop which can be adjusted either longitudinally or cross-sectionally' without breaking. the cop.
- Another object is a method of. adjusting a, cop to the chamber of a, shuttle.
- Fig. 1 is a side view of a coreless cop showing the manner in which the thread is wound;
- Fig. 2 is a side View showing the cop in full lines in normal position and in dot-and-dash lines to indicate the cop when adjusted;
- Fig. 3 is an end view of the cop shown in Fig. 1.
- the cop is Wound of a twisted thread of the type desired.
- the thread may be made by twisting paper ribbon into a thread in any known manner.
- the thread 25 is arranged in layers 2!, 22, 23, and 24 wound with a winding machine which is capable of producing a universal type winding such as is shown generally in Fig. 1 wherein the turns of which each layer is made up, are spirally wound, crisscrossed or interlaced throughout said layer.
- each turn of thread of a particular layer spirals around the length of the cop'arid spirals back again to the starting 4 Claims. (01. 242161) point, the return spiral of thread crisscrossing the initial spiral of thread at a plurality of pointsalong the layer.
- the inner end 26 of the innermost layer 24' may constitute the feed end of the cop 2B, and the end 21 may constitute the outer end of the cop, although if desired the outer end 21- may be used as the feed end.
- the cop 20 when so extended is indicated in broken lines as cop 30.
- the cop 30 maybe returned to its original length by compressing the cop ends.
- the full lines in Fig. 2 substantially representv the normal external dimensions of cop 20; and the dot-and-dash lines the: changed external dimensions of said cop when its opposite ends are drawn in opposite directions.
- the size of the cop may be adjusted to: fit shuttle chambers of various sizes.
- Shuttle chambers tend to vary in width and cross-sectional area, and the cops themselves tend to vary in outside diameter-,hence when the overall diameter of the cop, indicated by the full lines in Fig. 2, is larger than the width of the shuttle chamber, the opposite ends of the cop may be pulled in opposite directions to reduce the diameter of the cop substantially as indicated by the dot and dash lines in Fig. 2 until the outside diameter or overall cross-section of the cop has been sufficiently reduced so that the cop is small enough crosswise to pass between the inner faces of the side walls of the shuttle chamber.
- the opposite ends of the cop When the cop has been thus inserted in the shuttle chamber, the opposite ends of the cop may be compressed or pushed towards each other to 'expand the cop cross-sectionally thereby automatically adjusting the cop to fit snugly between the side walls of the chamber of the shuttle.
- This method of varying the cross-sectional area and length of the cop effectively compensates for variations in the outside diameters of the cops and variations in size of the cross-sectional areas of the shuttle chambers.
- each cop may be individually and variously adjusted to fit the chamber of the particular shuttle with which it is to be associated without breaking the cop or snarling the thread, and without requiring the removal of one or more outside layers of thread to adapt the outside diameter of the cop to the width of the shuttle chamber, thereby eliminating the discarding and wastage of layers of thread formerly necessarily removed from a cop in fitting it toa shuttle chamber.
- the cop Since the cop is coreless, resembling generally the form of a solenoid, it may be laterally flexed, and because the turns of each layer are spirally wound, such lateral flexing will not break the cop.
- the body of the cop is hollow the layer by layer spiralled construction of the turns of thread which constitute the cop body impart sufiicient rigidity to the cop body to make the cop self-supporting without resort to auxiliary stiffening means, the use whereof would impair the adjustability of the cop.
- a cop having a selfsupporting winding including an innermost layer consisting of a series of convolutions wound universally to define a self-supporting flexible tubular shell, the interior of said tubular shell being hollow and defining an air-core of appreciable cross-section, the free end of said innermost layer constituting the feed end of the cop, and a plurality of other layers each consisting of a series of convolutions universally coaxially successively wound upon and around said innermost layer and one above another to form in conjunction a flexible self-supported cop having a winding structure which can be stretched and compressed and between the side walls of the chamber of; the shuttle, and feeding the cop from the free end of the innermost layer of the winding through the core of the cop.
Description
March 20, 1951 F. FODERARO METHOD OF LOADING COPS Filed Oct. 21, 1947 INVENTOR. F-QA/VK' P0050120 BY yuan/00111011101111 Patented Mar. 20, 1951 METHOD OF LOADING COPS Frank Foderaro, Lawrence, Mass,
Patchogue-Plymouth Mills Corporation,
assignor to New York, N. Y., a corporation of New York Application October 21, 1947, Serial No. 781,225
I This invention relates to a universally wound co-p suchas is used in the art of weaving and a method of adjusting the same in a shuttle, and more particularly to a coreless cop used in weaving textile fabrics woven fro-m twisted paper threads, as for example seat covering materials and summer rugs.
- Coreless cops, that is cops having an air space or air core have heretofore been wound in progressively overlapping layers extending for but a relatively small portion of the length of the cop. When so wound a cop is easily broken if subjected to" longitudinal tension or lateral strain and when so broken is relatively useless. Furthermore, a cop sowound is'o-f' fixed'length and diameter and canonly be inserted in a shuttle for efiective use if said copdimensions-correspond substantially t'o'thedimensions of the shuttle chamber.
One object of this invention is a coreless' or air core cop which will not break when subjected to either longitudinal tension or to lateral strain.
Another object is a careless cop which can be adjusted either longitudinally or cross-sectionally' without breaking. the cop.
Another object is a method of. adjusting a, cop to the chamber of a, shuttle.
Other objects will appear from the detailed description which follows.
In the drawings comprising but a single sheet of three figures, numbered Figs. 1 to 3 inclusive, one embodiment of the invention is illustrated.
1 Fig. 1 is a side view of a coreless cop showing the manner in which the thread is wound;
Fig. 2 is a side View showing the cop in full lines in normal position and in dot-and-dash lines to indicate the cop when adjusted; and
Fig. 3 is an end view of the cop shown in Fig. 1.
Like reference characters designate corre- -sjponding parts throughout the several figures of the drawings.
The cop is Wound of a twisted thread of the type desired. For weaving seat covering materials and summer rugs, the thread may be made by twisting paper ribbon into a thread in any known manner. The thread 25 is arranged in layers 2!, 22, 23, and 24 wound with a winding machine which is capable of producing a universal type winding such as is shown generally in Fig. 1 wherein the turns of which each layer is made up, are spirally wound, crisscrossed or interlaced throughout said layer.
As best shown in Fig. 1 each turn of thread of a particular layer spirals around the length of the cop'arid spirals back again to the starting 4 Claims. (01. 242161) point, the return spiral of thread crisscrossing the initial spiral of thread at a plurality of pointsalong the layer.
Since the cop has an open or air core and is otherwise coreless, the inner end 26 of the innermost layer 24' may constitute the feed end of the cop 2B, and the end 21 may constitute the outer end of the cop, although if desired the outer end 21- may be used as the feed end.
Since the cop does not contain a rigid core, the spiralled, crisscrossed or interlaced turns of thread allow thev various layers to be extended in. unison, as by pulling the opposite ends of the cap in opposite directions, without breaking the cop. In Fig. 2' the cop 20 when so extended is indicated in broken lines as cop 30. The cop 30 maybe returned to its original length by compressing the cop ends. The full lines in Fig. 2 substantially representv the normal external dimensions of cop 20; and the dot-and-dash lines the: changed external dimensions of said cop when its opposite ends are drawn in opposite directions. Thus by extending and compressing the. cop, its cross-sectional area and length may be varied as desired without breaking the cop.
When the cross-sectional area and length are thus varied, the size of the cop may be adjusted to: fit shuttle chambers of various sizes. Shuttle chambers tend to vary in width and cross-sectional area, and the cops themselves tend to vary in outside diameter-,hence when the overall diameter of the cop, indicated by the full lines in Fig. 2, is larger than the width of the shuttle chamber, the opposite ends of the cop may be pulled in opposite directions to reduce the diameter of the cop substantially as indicated by the dot and dash lines in Fig. 2 until the outside diameter or overall cross-section of the cop has been sufficiently reduced so that the cop is small enough crosswise to pass between the inner faces of the side walls of the shuttle chamber. When the cop has been thus inserted in the shuttle chamber, the opposite ends of the cop may be compressed or pushed towards each other to 'expand the cop cross-sectionally thereby automatically adjusting the cop to fit snugly between the side walls of the chamber of the shuttle. This method of varying the cross-sectional area and length of the cop effectively compensates for variations in the outside diameters of the cops and variations in size of the cross-sectional areas of the shuttle chambers. Thus each cop may be individually and variously adjusted to fit the chamber of the particular shuttle with which it is to be associated without breaking the cop or snarling the thread, and without requiring the removal of one or more outside layers of thread to adapt the outside diameter of the cop to the width of the shuttle chamber, thereby eliminating the discarding and wastage of layers of thread formerly necessarily removed from a cop in fitting it toa shuttle chamber.
Since the cop is coreless, resembling generally the form of a solenoid, it may be laterally flexed, and because the turns of each layer are spirally wound, such lateral flexing will not break the cop.
Although the body of the cop is hollow the layer by layer spiralled construction of the turns of thread which constitute the cop body impart sufiicient rigidity to the cop body to make the cop self-supporting without resort to auxiliary stiffening means, the use whereof would impair the adjustability of the cop.
What is claimed is:
l. The method of loading a cop, having a winding wound universally and in tubular form to form a coaxially disposed hollow core definingan appreciable void, in the chamber of a shuttle, which consists in elongating the cop lengthwise to reduce its overall cross-section until the cop is small enough to pass between the side walls of the chamber of the shuttle, inserting said cop in the chamber of the shuttle, and then compressing the opposite ends of the cop to expand the cop cross-sectionally thereby automatically adjusting the cop to fit between the side walls of the chamber of the shuttle.
2. The method of loading a universally wound tubular cop, having a coaxially disposed hollow core defining an appreciable void, in the chamber of a shuttle, which consists in elongating the cop lengthwise to reduce its overall cross-section until the cop is narrow enough to pass between the side walls of the chamber of the shuttle, inserting said cop while thus elongated in the chamber of the shuttle, pushing the opposite ends of the cop towards each other to expand the cop cross-sectionally thereby automatically adjusting the cop to fit between the side walls of the chamber of the shuttle, and feeding the cop from the free end of the innermost layer of the winding through the hollow core thereof.
3. The method of loading a cop, having a selfsupporting winding including an innermost layer consisting of a series of convolutions wound universally to define a self-supporting flexible tubular shell, the interior of said tubular shell being hollow and defining an air-core of appreciable cross-section, the free end of said innermost layer constituting the feed end of the cop, and a plurality of other layers each consisting of a series of convolutions universally coaxially successively wound upon and around said innermost layer and one above another to form in conjunction a flexible self-supported cop having a winding structure which can be stretched and compressed and between the side walls of the chamber of; the shuttle, and feeding the cop from the free end of the innermost layer of the winding through the core of the cop.
4. The method of loading a universally wound I extensible self-supported open-cored cop in a shuttle which consists in elongating the winding of the cop lengthwise until the cop is narrow enough to pass between the side walls of the chamber of the shuttle, inserting the cop whenthus elongated in the shuttle-chamber, pushing;- the opposite ends of the elongated Winding to wards each other to expand the cop crosswise;
until its further crosswise-expansion is arrestedby engagement with the side walls of the shuttle} thereby automatically securing the cop in the; shuttle-chamber, and feeding the cop from the-- free end of the innermost layer of the winding through the open core thereof.
FRANK FODERARO."
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 360,108 Palmer Mar. 29, 1887 533,688 Wardwell Feb. 5, 1895 1,592,432 Barry July 13, 1926 1,682,777
Damon Sept. 4, 1928
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US781225A US2545919A (en) | 1947-10-21 | 1947-10-21 | Method of loading cops |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US781225A US2545919A (en) | 1947-10-21 | 1947-10-21 | Method of loading cops |
Publications (1)
Publication Number | Publication Date |
---|---|
US2545919A true US2545919A (en) | 1951-03-20 |
Family
ID=25122073
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US781225A Expired - Lifetime US2545919A (en) | 1947-10-21 | 1947-10-21 | Method of loading cops |
Country Status (1)
Country | Link |
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US (1) | US2545919A (en) |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US360108A (en) * | 1887-03-29 | Sewing-machine cop | ||
US533688A (en) * | 1895-02-05 | Yarn-roll and method of making same | ||
US1592432A (en) * | 1924-10-01 | 1926-07-13 | John L Barry | Packaging yarn, thread, and the like |
US1682777A (en) * | 1927-03-10 | 1928-09-04 | Plymouth Cordage Co | Twine package and process for its manufacture |
-
1947
- 1947-10-21 US US781225A patent/US2545919A/en not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US360108A (en) * | 1887-03-29 | Sewing-machine cop | ||
US533688A (en) * | 1895-02-05 | Yarn-roll and method of making same | ||
US1592432A (en) * | 1924-10-01 | 1926-07-13 | John L Barry | Packaging yarn, thread, and the like |
US1682777A (en) * | 1927-03-10 | 1928-09-04 | Plymouth Cordage Co | Twine package and process for its manufacture |
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