US3350030A - Fiberglass reinforced textile bobbin - Google Patents

Fiberglass reinforced textile bobbin Download PDF

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US3350030A
US3350030A US498375A US49837565A US3350030A US 3350030 A US3350030 A US 3350030A US 498375 A US498375 A US 498375A US 49837565 A US49837565 A US 49837565A US 3350030 A US3350030 A US 3350030A
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strands
fiberglass
helix angle
fiberglass strands
bobbin
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US498375A
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Alfred J Green
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NVF Co
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NVF Co
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H75/00—Storing webs, tapes, or filamentary material, e.g. on reels
    • B65H75/02—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks
    • B65H75/18—Constructional details
    • 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

  • the textile bobbin includes a tubular core of resinilnpregnated fibrous material having a strengthening layer of fiberglass strands concentrically sandwiched between inner and outer layers of fibrous material.
  • the fiberglass layer includes strands wound at a high helix angle at about 50 to 70 sandwiched between strands wound at a low helix angle at about 1 to 20 with a major portion of the fiberglass strand being at the low helix angle.
  • This invention relates to textile bobbins and their manufacture and more particularly to such bobbins which are used as tensioning spools for nylon thread and the like.
  • Textile thread such as nylon and the like are for some uses such as tire cording and the like wound during processing on bobbins to stretch the thread and maintain it under tension. This is done for example by rotating the bobbin at a faster rate than the thread is fed to it. Wrapping the thread at the desired tension or prestretching however creates a dilema with conventional bobbins. For example, if on the one hand, the thread is wrapped under the desired extremely high tension, the bobbin will crack or otherwise fail. On the other hand, if the thread is not wrapped so tight, the proper amount of tension or prestretching is not attained.
  • An object of this invention is to provide an effective, non-metallic bobbin which can withstand the tremendous force applied by tightly wrapping textile thread, such as nylon, thereon for tensioning purposes.
  • a further object is to provide an economical and reliable method of manufacturing such bobbins.
  • the resin-impregnated core of the bobbin is made of relatively inexpensive compressed fibrous material such as paper with fiberglass reinforcing strands wrapped or reaved thereon. It has been found that when the fiberglass strands are wrapped at a relatively low helix angle, the resultant bobbin is made resistant to longitudinal cracking caused by lateral inward forces. The bobbin, however, even with superior hoop strength would still tend to crack laterally. It has also been found, however, that bobbins can be made resistant to this lateral cracking by wrapping the fiberglass strands at a relatively high helix angle to thus impart longitudinal strength to the bobbin.
  • the bobbins of this invention are thus made by wrapping or reaving the fiberglass strands at both high and low helix angles until the core is sufficiently covered.
  • these high and low angles may vary, but experience indicates that between 50 and 70 and between 1 and 20, respectively, and preferably approximately 60 and respectively, provide superior results.
  • FIG. 1 is an end view of a bobbin in accordance with one embodiment of this invention
  • FIG. 2 is a cross-sectional view taken through FIG. 1 along the line 22;
  • FIGS. 3-5 are side views in elevation of a bobbin during different phases of manufacture.
  • the bobbin 10 includes a cylindrical compressed resin-impregnated fibrous core 12 made for example of phenolic paper.
  • the core 12 has for example a layer 14 of epoxy resin coated fiberglass filaments thereon.
  • the fiberglass layer 14 in turn has another layer of resin-impregnated phenolic paper thereon, upon which the nylon or other material is wound for tensioning during use.
  • a supporting ring 18 may be pressed into each end of the bobbin 10 to support the bobbin on the centering collet of the textile tensioning machine.
  • Fiberglass layer 14 is formed by reaving fiberglass strands around core 12. As indicated in FIG. 3 strands 20 are disposed at a relatively low helix angle of between about 1 and 44, and preferably between about 1 and 20, with the most advantageous angle being 10. The strands 20' are helically applied back and forth across the entire length of the core 12. A second set of fiberglass strands 22 is then reaved back and forth across the entire length of the core 12 at a relatively high helix angle of between about 46 and 89, and preferably between about 50 and 70, with the most advantageous being 60. The reaving of the fiberglass strands at these angles is continued until the desired thickness is obtained. As indicated in FIG. 3 strands 20 are disposed at a relatively low helix angle of between about 1 and 44, and preferably between about 1 and 20, with the most advantageous angle being 10. The strands 20' are helically applied back and forth across the entire length of the core 12. A second set of fiberglass strands 22 is then reaved back and forth across the entire length
  • the resultant assembly includes a number of partially completed bobbins 24 comprising fiberglass strands coating core 12. Outer sleeve 16 is then applied to this assembly and the assembly is cut to the required sizes. Rings 18 are then secured in place to form the completed bobbins.
  • the fiberglass strands may be applied at a much higher feed rate and thus more economically, and with a greater packing effect, at a low helix angle, than at a high helix angle. Accordingly, it is very desirable to initially apply the fiberglass at a low helix angle directly on the core 12 until about one-third of the desired fiberglass layer has been built up. The high helix angle strands are then ap plied, until about another one third of the fiberglass layer has been built up. A final application of the fiberglass strands at the low helix angle builds up the remaining one-third of the core. This arrangement is particularly advantageous because the high helix angle strands are sandwiched between layers of very tightly packed low helix strands.
  • the strands are later ground or otherwise machined to attain a higher degree of smoothness before applying the outer fiber layer, it is a portion of the less expensively applied low helix strands which are sacrificed. Further, the low helix strands comprise from about to of all the fiberglass strands without adversely affecting the resistance to lateral cracking.
  • the bobbins 10 are made by first winding the resin coated fibrous material such as phenolic paper in sheet form around a central mandrel to form an inner layer or core 12.
  • the desired fiberglass layer 14 is then applied, as noted above. In certain operations, it may be desirable to machine the outer surface of the fiberglass layer at this stage to improve this surface for the next operation.
  • the outer resin coated fibrous material 16, such as phenolic paper is next applied in sheet form, and external mechanical pressure and heat are utilized, such as a line chanical hot press, to cure the resin impregnating the materials. Finally, the mandrel is withdrawn and the ends of the tubular laminated member (comprising layers 12, 14 and 16) are machined to form the finished textile bobbin.
  • a textile bobbin comprising a generally tubular core of compressed, resin-impregnated fibrous material including a strengthening layer of fiberglass strands, a portion of the fiberglass strands being helically arranged to impart lateral strength and another portion of the fiberglass strands being helically arranged to impart longitudinal strength to the bobbin, said fiberglass strands arranged to impart lateral strength being positioned at a relatively low helix angle of about 1 to 20, said fiberglass strands arranged to impart longitudinal strength being positioned at a relatively high helix angle of about 50 to 70, said layer of fiberglass strands being concentrically sandwiched between inner and outer layers of fibrous material, a major portion of said fiberglass strands being positioned at said low helix angle, said high helix angle strands being sandwiched between low helix angle strands, and textile thread under tension being wound on said core.

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  • Laminated Bodies (AREA)
  • Moulding By Coating Moulds (AREA)

Description

- Oct. 31, 1967 A. J. GREEN FIBERGLASS REINFORCED TEXTILE BOBBIN Filed 001;. '20, 1965 g4 IVENTOR 149 7661 J Green United States Patent 3,350,030 FIBERGLASS REINFORCED TEXTILE BOBBIN Alfred J. Green, Yorklyn, Del., assignor to NVF Company, a corporation of Delaware Filed Oct. 20, 1965, Ser. No, 498,375 2 Claims. (Cl. 242-118.32)
ABSTRACT OF THE DISCLOSURE The textile bobbin includes a tubular core of resinilnpregnated fibrous material having a strengthening layer of fiberglass strands concentrically sandwiched between inner and outer layers of fibrous material. The fiberglass layer includes strands wound at a high helix angle at about 50 to 70 sandwiched between strands wound at a low helix angle at about 1 to 20 with a major portion of the fiberglass strand being at the low helix angle.
This invention relates to textile bobbins and their manufacture and more particularly to such bobbins which are used as tensioning spools for nylon thread and the like.
Textile thread such as nylon and the like are for some uses such as tire cording and the like wound during processing on bobbins to stretch the thread and maintain it under tension. This is done for example by rotating the bobbin at a faster rate than the thread is fed to it. Wrapping the thread at the desired tension or prestretching however creates a dilema with conventional bobbins. For example, if on the one hand, the thread is wrapped under the desired extremely high tension, the bobbin will crack or otherwise fail. On the other hand, if the thread is not wrapped so tight, the proper amount of tension or prestretching is not attained.
An object of this invention is to provide an effective, non-metallic bobbin which can withstand the tremendous force applied by tightly wrapping textile thread, such as nylon, thereon for tensioning purposes.
A further object is to provide an economical and reliable method of manufacturing such bobbins.
In accordance with this invention, the resin-impregnated core of the bobbin is made of relatively inexpensive compressed fibrous material such as paper with fiberglass reinforcing strands wrapped or reaved thereon. It has been found that when the fiberglass strands are wrapped at a relatively low helix angle, the resultant bobbin is made resistant to longitudinal cracking caused by lateral inward forces. The bobbin, however, even with superior hoop strength would still tend to crack laterally. It has also been found, however, that bobbins can be made resistant to this lateral cracking by wrapping the fiberglass strands at a relatively high helix angle to thus impart longitudinal strength to the bobbin. The bobbins of this invention are thus made by wrapping or reaving the fiberglass strands at both high and low helix angles until the core is sufficiently covered. Advantageously, these high and low angles may vary, but experience indicates that between 50 and 70 and between 1 and 20, respectively, and preferably approximately 60 and respectively, provide superior results.
Novel features and advantages of the present invention will become apparent to one skilled in the art from a reading of the following description in conjunction with the accompanying drawings wherein similar reference characters refer to similar parts and in which:
FIG. 1 is an end view of a bobbin in accordance with one embodiment of this invention;
FIG. 2 is a cross-sectional view taken through FIG. 1 along the line 22; and
FIGS. 3-5 are side views in elevation of a bobbin during different phases of manufacture.
Patented Oct. 31, 1967 "ice As most clearly shown in FIG. 2, the bobbin 10 accordmg to the preferred embodiment of this invention includes a cylindrical compressed resin-impregnated fibrous core 12 made for example of phenolic paper. The core 12 has for example a layer 14 of epoxy resin coated fiberglass filaments thereon. The fiberglass layer 14 in turn has another layer of resin-impregnated phenolic paper thereon, upon which the nylon or other material is wound for tensioning during use.
A supporting ring 18 may be pressed into each end of the bobbin 10 to support the bobbin on the centering collet of the textile tensioning machine.
Fiberglass layer 14 is formed by reaving fiberglass strands around core 12. As indicated in FIG. 3 strands 20 are disposed at a relatively low helix angle of between about 1 and 44, and preferably between about 1 and 20, with the most advantageous angle being 10. The strands 20' are helically applied back and forth across the entire length of the core 12. A second set of fiberglass strands 22 is then reaved back and forth across the entire length of the core 12 at a relatively high helix angle of between about 46 and 89, and preferably between about 50 and 70, with the most advantageous being 60. The reaving of the fiberglass strands at these angles is continued until the desired thickness is obtained. As indicated in FIG. 5 the resultant assembly includes a number of partially completed bobbins 24 comprising fiberglass strands coating core 12. Outer sleeve 16 is then applied to this assembly and the assembly is cut to the required sizes. Rings 18 are then secured in place to form the completed bobbins.
The fiberglass strands may be applied at a much higher feed rate and thus more economically, and with a greater packing effect, at a low helix angle, than at a high helix angle. Accordingly, it is very desirable to initially apply the fiberglass at a low helix angle directly on the core 12 until about one-third of the desired fiberglass layer has been built up. The high helix angle strands are then ap plied, until about another one third of the fiberglass layer has been built up. A final application of the fiberglass strands at the low helix angle builds up the remaining one-third of the core. This arrangement is particularly advantageous because the high helix angle strands are sandwiched between layers of very tightly packed low helix strands. Additionally, if as is useful in some operations, the strands are later ground or otherwise machined to attain a higher degree of smoothness before applying the outer fiber layer, it is a portion of the less expensively applied low helix strands which are sacrificed. Further, the low helix strands comprise from about to of all the fiberglass strands without adversely affecting the resistance to lateral cracking.
The bobbins 10 are made by first winding the resin coated fibrous material such as phenolic paper in sheet form around a central mandrel to form an inner layer or core 12. The desired fiberglass layer 14 is then applied, as noted above. In certain operations, it may be desirable to machine the outer surface of the fiberglass layer at this stage to improve this surface for the next operation. The outer resin coated fibrous material 16, such as phenolic paper, is next applied in sheet form, and external mechanical pressure and heat are utilized, such as a line chanical hot press, to cure the resin impregnating the materials. Finally, the mandrel is withdrawn and the ends of the tubular laminated member (comprising layers 12, 14 and 16) are machined to form the finished textile bobbin.
Obviously, many modifications and variations of the present invention are possible in the light of the above teachings.
It is therefore to be understood that within the scope of the appended claims the invention may be practiced otherwise than as specifically described.
What is claimed is:
1. A textile bobbin comprising a generally tubular core of compressed, resin-impregnated fibrous material including a strengthening layer of fiberglass strands, a portion of the fiberglass strands being helically arranged to impart lateral strength and another portion of the fiberglass strands being helically arranged to impart longitudinal strength to the bobbin, said fiberglass strands arranged to impart lateral strength being positioned at a relatively low helix angle of about 1 to 20, said fiberglass strands arranged to impart longitudinal strength being positioned at a relatively high helix angle of about 50 to 70, said layer of fiberglass strands being concentrically sandwiched between inner and outer layers of fibrous material, a major portion of said fiberglass strands being positioned at said low helix angle, said high helix angle strands being sandwiched between low helix angle strands, and textile thread under tension being wound on said core.
2. A textile bobbin as in claim 1 wherein said core is essentially cylindrical, and approximately from /3 to of said fiberglass strands being positioned at a relatively low helix angle of approximately 10, and approximately from A to /3 of said fiberglass strands being positioned at a relatively high helix angle of approximately 60.
References Cited UNITED STATES PATENTS 1,312,780 8/1919 Fenn 138-144 2,847,786 8/1958 Hartley et al. 2,854,031 9/1958 Donaldson 138141 X 3,105,786 10/1963 Anderson 156-l73 3,152,804 10/1964 Costopoulos 156-172 X FRANK I. COHEN, Primary Examiner.
GEORGE F. MAUTZ, Examiner.

Claims (1)

1. A TEXTILE BOBBIN COMPRISING A GENERALLY TUBULAR CORE OF COMPRESSED, RESIN-IMPREGNATED FIBROUS MATERIAL INCLUDING A STRENGTHENING LAYER OF FIBERGLASS STRANDS, A PORTION OF THE FIBERGLASS STRANDS BEING HELICALLY ARRANGED TO IMPART LATERAL STRENGTH AND ANOTHER PORTION OF THE FIBERGLASS STRANDS BEING HELICALLY ARRANGED TO IMPART LONGITUDINAL STRENGTH TO THE BOBBION, SAID FIBERGLASS STRANDS ARRANGED TO IMPART LATERAL STRENGTH BEING POSITIONED AT A RELATIVELY LOW HELIX ANGLE OF ABOUT 1* TO 20*, SAID FIBERGLASS STRANDS ARRANGED TO IMPART LONGITUDINAL STRENGTH BEING POSITIONED AT A RELATIVELY HIGH HELIX ANGLE OF ABOUT 50* TO 70*, SAID LAYER OF FIBERGLASS STRANDS BEING CONCENTRICALLY SANDWICHED BETWEEN INNER AND OUTER LAYERS OF FIBROUS MATERIAL, A MAJOR PORTION OF SAID FIBERGLASS STRANDS BEING POSITIONED AT SAID LOW HELIX ANGLE, SAID HIGH HELIX ANGLE STRANDS BEING SANDWICHED BETWEEN LOW HELIX ANGLE STRANDS, AND TEXTILE THREAD UNDER TENSION WOUND ON SAID CORE.
US498375A 1965-10-20 1965-10-20 Fiberglass reinforced textile bobbin Expired - Lifetime US3350030A (en)

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Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3451639A (en) * 1966-07-12 1969-06-24 Dyson Kissner Corp Textile tube
US3584922A (en) * 1968-07-23 1971-06-15 Diehl Tubular chain link body
US3897292A (en) * 1972-08-18 1975-07-29 Yamauchi Rubber Ind Co Ltd Method of producing a printing magnetic saddle
US3900048A (en) * 1971-07-20 1975-08-19 Owens Corning Fiberglass Corp Reinforced thermoplastic pipe
US4020202A (en) * 1973-07-07 1977-04-26 Maschinenfabrik Augsburg-Nurnberg Ag Beam and strut girder
US4088282A (en) * 1976-12-03 1978-05-09 Monsanto Company Crushable bobbin package for conjugate yarn
US4345625A (en) * 1977-09-02 1982-08-24 Sekisui Kagaku Kogyo Kabushiki Kaisha Pipe joints of reinforced resin and process for their molding
WO1982003248A1 (en) * 1981-03-20 1982-09-30 Abc Corp Peabody Sound attenuator
US4389269A (en) * 1978-02-21 1983-06-21 Pepsico, Inc. Sports racket
EP0170094A1 (en) * 1984-08-02 1986-02-05 Wibmer & Co. KG Tube in the capacity of a winding core
EP0257461A2 (en) * 1986-08-16 1988-03-02 Norddeutsche Faserwerke GmbH Method and apparatus for the manufacture of spirally wound tubes, bobbins, containers or the like
WO1999008033A1 (en) * 1996-01-30 1999-02-18 Exxon Research And Engineering Company High weeping strength polymer-glass ribbon composite laminates for fluid containment
US6719242B2 (en) 2000-12-01 2004-04-13 Sonoco Development, Inc. Composite core
US20060214049A1 (en) * 2005-03-23 2006-09-28 Sonoco Development, Inc. Non-round profiled pultruded tube
US20170366901A1 (en) * 2016-06-21 2017-12-21 Dongguan Li Yin Technology Limited Multi-strand independent input-output voice coil

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1312780A (en) * 1917-12-06 1919-08-12 William B Fenn Reinforced receptacle, tube, or the like and process of making the same.
US2847786A (en) * 1955-02-07 1958-08-19 Olin Mathieson Composite firearm barrel comprising glass fibers
US2854031A (en) * 1952-04-11 1958-09-30 Donaldson Chase Plastic tubing
US3105786A (en) * 1960-05-05 1963-10-01 Smith Corp A O Method of forming a fiber-reinforced resinous spool
US3152804A (en) * 1961-11-30 1964-10-13 Costopoulos Nick Bowling pin with wound filament reinforcement

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1312780A (en) * 1917-12-06 1919-08-12 William B Fenn Reinforced receptacle, tube, or the like and process of making the same.
US2854031A (en) * 1952-04-11 1958-09-30 Donaldson Chase Plastic tubing
US2847786A (en) * 1955-02-07 1958-08-19 Olin Mathieson Composite firearm barrel comprising glass fibers
US3105786A (en) * 1960-05-05 1963-10-01 Smith Corp A O Method of forming a fiber-reinforced resinous spool
US3152804A (en) * 1961-11-30 1964-10-13 Costopoulos Nick Bowling pin with wound filament reinforcement

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3451639A (en) * 1966-07-12 1969-06-24 Dyson Kissner Corp Textile tube
US3584922A (en) * 1968-07-23 1971-06-15 Diehl Tubular chain link body
US3900048A (en) * 1971-07-20 1975-08-19 Owens Corning Fiberglass Corp Reinforced thermoplastic pipe
US3897292A (en) * 1972-08-18 1975-07-29 Yamauchi Rubber Ind Co Ltd Method of producing a printing magnetic saddle
US4020202A (en) * 1973-07-07 1977-04-26 Maschinenfabrik Augsburg-Nurnberg Ag Beam and strut girder
US4088282A (en) * 1976-12-03 1978-05-09 Monsanto Company Crushable bobbin package for conjugate yarn
US4345625A (en) * 1977-09-02 1982-08-24 Sekisui Kagaku Kogyo Kabushiki Kaisha Pipe joints of reinforced resin and process for their molding
US4389269A (en) * 1978-02-21 1983-06-21 Pepsico, Inc. Sports racket
WO1982003248A1 (en) * 1981-03-20 1982-09-30 Abc Corp Peabody Sound attenuator
US4421202A (en) * 1981-03-20 1983-12-20 Peabody Abc Corporation Sound attenuator
EP0170094A1 (en) * 1984-08-02 1986-02-05 Wibmer & Co. KG Tube in the capacity of a winding core
DE3428466A1 (en) * 1984-08-02 1986-02-13 Wibmer + Co KG, 7417 Pfullingen SLEEVE AS WINDING CORE
EP0257461A2 (en) * 1986-08-16 1988-03-02 Norddeutsche Faserwerke GmbH Method and apparatus for the manufacture of spirally wound tubes, bobbins, containers or the like
EP0257461A3 (en) * 1986-08-16 1989-12-06 Norddeutsche Faserwerke Gmbh Method and apparatus for the manufacture of spirally wound tubes, bobbins, containers or the like
WO1999008033A1 (en) * 1996-01-30 1999-02-18 Exxon Research And Engineering Company High weeping strength polymer-glass ribbon composite laminates for fluid containment
US6719242B2 (en) 2000-12-01 2004-04-13 Sonoco Development, Inc. Composite core
US20060214049A1 (en) * 2005-03-23 2006-09-28 Sonoco Development, Inc. Non-round profiled pultruded tube
US20170366901A1 (en) * 2016-06-21 2017-12-21 Dongguan Li Yin Technology Limited Multi-strand independent input-output voice coil
US10277984B2 (en) * 2016-06-21 2019-04-30 Dongguan Li Yin Technology Limited Multi-strand independent input-output voice coil

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