US3875625A - Apparatus for interlacing filaments of multifilament yarns - Google Patents

Apparatus for interlacing filaments of multifilament yarns Download PDF

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Publication number
US3875625A
US3875625A US438684A US43868474A US3875625A US 3875625 A US3875625 A US 3875625A US 438684 A US438684 A US 438684A US 43868474 A US43868474 A US 43868474A US 3875625 A US3875625 A US 3875625A
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United States
Prior art keywords
fluid
yarn
treatment zone
interlacing
axis
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Expired - Lifetime
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US438684A
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English (en)
Inventor
Charles Blanc
Christian Delarue
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Rhone Poulenc Textile SA
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Rhone Poulenc Textile SA
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Publication date
Application filed by Rhone Poulenc Textile SA filed Critical Rhone Poulenc Textile SA
Priority to US05/532,238 priority Critical patent/US3958310A/en
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Publication of US3875625A publication Critical patent/US3875625A/en
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Expired - Lifetime legal-status Critical Current

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Classifications

    • DTEXTILES; PAPER
    • D02YARNS; MECHANICAL FINISHING OF YARNS OR ROPES; WARPING OR BEAMING
    • D02JFINISHING OR DRESSING OF FILAMENTS, YARNS, THREADS, CORDS, ROPES OR THE LIKE
    • D02J1/00Modifying the structure or properties resulting from a particular structure; Modifying, retaining, or restoring the physical form or cross-sectional shape, e.g. by use of dies or squeeze rollers
    • D02J1/08Interlacing constituent filaments without breakage thereof, e.g. by use of turbulent air streams

Definitions

  • ABSTRACT Multifilament yarn is interlaced by passing the yarn through an apparatus which impinges four streams or jets of fluid upon the yarn.
  • the jets or streams of fluid are given a rotational component by auxiliary streams of air which impinge on the jets or streams with a tangential attitude.
  • the yarn and impinging streams of fluid converge in a cavity located within an interlacing chamber wherein the height of the cavity is no greater than the smallest diameter of the cavity and wherein the inlet of the interlacing chamber is wider than the diameter of the cavity and the outlet of the interlacing chamber is narrower than the cavity.
  • the instant invention relates to methods of and apparatus for the manufacture of multifilament yarns having interlaced filaments. More particularly, the instant invention relates to methods and apparatus for the manufacture of multifilament yarns having interlaced filaments wherein the filaments are interlaced by impinging at least one stream of fluid on the yarn.
  • the filaments of multifilament yarns are cohered together by processes such as twisting, sizing or interlacing.
  • the present invention is directed to interlacing wherein a yarn formed of continuous multifilaments is interlaced or tangled in a generally random way to form pseudo burls which cooperate to form a yarn that has a total twist which may be substantially zero.
  • interlaced yarn The prior art suggests several processes for the man ufacture of interlaced yarn. These processes include subjecting the yarn, while under slight tension, to the action of at least one fluid jet which is generally created by compressed air. Generally the jet is directed in a plane that is substantially normal to the direction in which the yarn advances and is impinged on the yarn as the yarn traverses what is generally known as an interlacing nozzle" or interlace nozzle.”
  • the patent literature. especially the French patent literature. contains many examples of interlacing methods and apparatus for utilization in interlacing the fibers of multifiber yarn.
  • No. 68,429 to French Pat. No. 1,108,890 a strand of multifiber yarn is advanced between a delivery tube which impinges fluid against the strand and a resonance box.
  • An improvement to this invention is disclosed in French Pat. No. 1,334,130 in which the impinging fluid is recycled from the outlet of the resonance box and again impinged on the yarn.
  • French Pat. No. 1,492,945 discloses a process in which a multifilament strand of yarn is subjected simultaneously to impingement from pairs of primary fluid jets and at least one secondary jet which impinges fluid on the yarn from a direction opposite that of the primary jets in a zone between the points of impact of the primary jets.
  • French Pat. No. 2,094,232 discloses a process in which yarn is passed through a conduit and subjected to impingement from two fluid jets which are substantially aligned with the conduit but are oppositely directed.
  • U.S. Pat. No. 2,191,791 discloses a yarn guide composed of a cavity, the height of which is at most equal to the diameter thereof. As the yarn passes through the cavity, a plurality of radial jets impinge fluid streams upon the yarn and as a result of the action of radial streams, the yarn is interlaced.
  • the present invention contemplates an apparatus for interlacing the filaments of a multifilament yarn under the influence of an expanding pressurized fluid by advancing the yarn through an interlacing chamber havmost equal to its diameter.
  • the present invention also contemplates methods utilizing the features of the aforedescribed apparatus.
  • FIG. 1 is a side view of a nozzle according to the instant invention taken in section to show an interlacing chamber and fluid conduits;
  • FIG. 2 is a top view of the nozzle in FIG. 1 taken in section along line 2-2 of FIG. 1 showing four conduits registering with the interlacing chamber;
  • FIG. 3 is a half view taken in section along line 3-3 of the nozzle shown in FIG. 2 illustrating how a fluid supply line is registered with the nozzle;
  • FIG. 4 is a side view in section showing a plate which is utilized for partial closure of the outlet end of the interlacing chamber shown in the previous figures;
  • FIG. 5 is a top view of the plate shown in FIG. 4;
  • FIG. 6 is another embodiment of a plate which is used for partial closure of the outlet of the interlacing chamber.
  • FIG. 7 is a top view of an embodiment of the nozzle according to the invention which can be pivoted to an open position to receive multifilament yarn therethrough in a convenient manner.
  • FIG. 1 there is shown a nozzle, designated generally by the numeral 10, which is the apparatus for performing the process of the instant invention.
  • the nozzle 10 has an interlacing chamber, designated generally by the numeral 11, through which passes a multifilament strand of yarn l2 and in which the filaments of the yarn 12 are interlaced to form a unified strand of yarn.
  • the interlacing chamber is a generally cylindrical bore formed in a block 13.
  • the interlacing chamber 11 maintains its cylindrical configuration for a certain distance and then tapers with a conical portion 14 to form what is herein described as a treatment zone 16. Downstream of the treatment zone 16, the interlacing chamber 11 expands through another beveled portion 17 and continues to an outlet 18.
  • a plate 19 is bolted by screws 21 (see FIG. 3) to the block 13.
  • the plate 19 has a projecting portion 22 which extends therefrom to form a converging outlet 24 therein, the purpose of which will be explained hereinafter.
  • the treatment chamber 16 has an axial length which is substantially equal to its diameter. However, the axial length of the treatment chamber may, if desired, be less than the diameter.
  • Registered with the treatment chamber 16 are pairs of opposed jets 26 and 27 extending I along one axis, and 28 and 29 extending along another axis, positioned normal to the first axis.
  • the axes of the jets are all included in the same plane, which plane is perpendicular to the longitudinal direction of advance assumed by the yarn 12. Through these jets 26, 27, 28 and 29, fluid is passed to impinge on the yarn 12. All fluid flowing through these jets flows into the treatment zone 16.
  • the jets 26, 27, 28 and 29 have vortex chambers 31, 32, 33 and 34 respectively associated therewith. These vortex chambers are axially aligned with the jets. In order to generate vertices within the vortex chambers 31, 32, 33 and 34, each vortex chamber has a tangential jet 36 registered therewith in a direction which is tangent to the axes of the vortex chambers and the jets 26, 27, 28 and 29.
  • each vortex chamber Connected to each vortex chamber is a principal fluid supply conduit 41 which supplies the fluid stream that expands through the jets 26, 27, 28 and 29, to impinge upon the yarn 12.
  • the tangential jets 36 supply an auxiliary fluid in a direction which is tangential to the flow of the principal fluid. This causes the principal fluid to rotate and form vertices which generally rotate about the axes of the jets 26-29 and the vortex chambers 31-34.
  • the auxiliary fluid is applied via conduits 42 (see FIGS. 1 and 3) that register with bores 43 and 44 in the block 13.
  • the bore 43 communicates with vortex chambers 31 and 33 through tangential jets 36 while the bore 44, which is diagonally spaced from the bore 43, communicates with vortex chambers 32 and 34 through tangential jets 36.
  • the bores 43 and 44 By configuring the bores 43 and 44 in this way, it is possible to rotate the vortices in vortex chamber 31 in the opposite direction from the vortices generated in the vortex chamber 32.
  • the vortices in vortex chamber 33 are rotated in the opposite direction from the vortices in the vortex chamber 34. This, of course, occurs because the tangential jets communicating with opposed vortex chambers 31, 32 and 33, 34 are directed in opposite directions.
  • the block 13 has threaded holes 47 machined therein through which may be introduced valves 51 that may be registered with the jets 36 to constrict the inlet ends of the jets to throttle the amount of fluid entering the jets and thereby control the the intensity of vortices generated in the vortex chambers 31-34.
  • valves 51 By utilizing the valves 51, the vortices in selected ones of the chambers 31-34 may be varied selectively so that fluid impinging on the yarn 12 through the jets 26-29 may have varying rotation components. This produces different variations in interlacing configurations given to the multifilament yarn 12. If desired, of course, selected ones of the jets 36 may be cut off completely by the valves 51 so that the principal fluid stream applied through the associated vortex chamber will have no rotational component.
  • the bores 47 may also be used upon removal of the valves 51 to inject auxiliary fluids, such as dyes or other processing fluids, into the principal'fluid. Furthermore, the bores 47 are, or may be, created as a convenient access for boring the jets 36 through the block 13.
  • FIGS. 4, 5 and 6 there are shown two types of plates which are used to partially constrict the outlet 18 of the interlacing chamber 11.
  • the embodiment shown in FIG. 4 has already been described and utilizes a converging portion 24 which is conical to gradually constrict the outlet from the interlacing chamber 11.
  • the embodiment of FIG. 6 shows a different configuration of the plate 19 wherein the outlet 18 of the interlacing chamber 11 may be constricted by an abrupt orifice 52.
  • FIG. 7 there is shown an embodiment of the nozzle 10 wherein the block 13 is divided into a pair of symmetrical portions 13a and 13b so that the block may be conveniently opened for insertion of a multifilament yarn 12.
  • the yarn does not have to be first severed and threaded through the nozzle in order to apply the nozzle 10 to the yarn.
  • the two halves 13a and 13b are pivoted by pins 63 and 64 to a plate 70 so as to swing toward and away from one another.
  • the portion 13a has a handle 65 rigidly secured thereto and a pin 66 projecting therefrom.
  • the pin 66 is engaged by a latch 68.
  • the latch 68 has a curved slot 69 therein which engages the pin 66 and captures as a handle 71 is rotated in the counterclockwise direction.
  • the handle 71 is pivoted offcenter about a pin 72 so as the handle is rotated the pin 66 is drawn progressively closer to the pin 72.
  • an articulated locking system is provided in which absorption of play between the two halves 13a and 13! may be accomplished by auxiliary structures, such as spring washers, positioned to act between the two halves 13a and 13b.
  • the fluid utilized is air. It should be kept in mind that any other gas or liquid or a diphase liquid. such as an emulsion, may be used. In addition, it should be kept in mind that the fluid utilized may contain a dye.
  • interlacing chamber 11 and treatment zone 16 disclosed in the drawings are generally cylindrical in configuration. It should be kept in mind that these portions of the nozzle 10 may have a surface defined by any convenient surface of revolution so that the diameter may vary from one end to the other.
  • jets 26, 27, 28 and 29 are shown having axes all in the same plane, these jets may be inclined relative to that plane so as to generate a traction on the yarn 12 as the fluid passes through the jets and impinges on the yarn.
  • jets 26, 27, 28 and 29 are illustrated as being positioned at an angle of 90 to one another, it is possible to utilize any number ofjets the angle between which may vary between 0 and 80 and preferably may vary between 30 and 80.
  • the fluid ejected from adjacent jets may rotate in the same direction or in opposite directions. If the fluid from adjacent jets rotates in opposite directions, it is possible to avoid parasitic false twist effects on the multifilament yarn as it is interlaced.
  • jets 26-29 and the vortex chambers 31-34 are shown as having cylindrical side walls, it is also possible to profile these structures to have the form of a Laval nozzle which is convergent and divergent. Such a configuration would enhance the speed of ejection of fluids through these structures while at the same time reducing consumption of fluid to produce the same interlacing effect on the yarn.
  • the configuration of the yarn 12, as it emerges from the interlacing chamber 1 1, may be varied according to whether or not the outlet 18 of the chamber is constricted. If the outlet of the chamber is constricted by, for example, the converging surface 24 shown in FIGS. 1, 3 and'4, or the converging surface 52 shown in FIG. 5, an improvement in yarn cohesion results because the exit speed of the fluid is increased. If the opening 18 is wider than the diameter of the treatment zone, then the yarn, as it exists from the interlacing chamber, will swell creating an effect which might, under some circumstances, be desired.
  • the cohesion factor of the interlacing was measured on an entanglement tester R-2040," Rothschild (Zurich).
  • This entanglement tester works on the principal of automatic detection of the distance between points of interlacing by utilizing a needle that penetrates between the filaments of a moving yarn and retracts as soon as it encounters a point of resistance, the point of resistance being an interlace point.
  • the values of the interlace factor are presented in the following table in which PI is the injection pressure of the principal fluid, P.T. is the injection pressure of the auxiliary fluid used to create the turbulence and V is the yarn speed in meters per minute.
  • EXAMPLE 2 The operating conditions in this example are the same as in Example 1 except that the nozzle functioned without feeding turbulence fluid. In this example, no
  • the interlace factor is directly proportional to the injection pressure
  • the interlace factor varies as a function of the turbulence-causing fluid pressure.
  • There is a minimum interlace factor which, for a given pressure of injection fluid, is the same at the same turbulence causing fluid pressure.
  • By optimizing the pressure of the primary injection fluid and the pressure of the turbulence-causing fluid it is possible to achieve the best nozzle efficiencies by utilizing minimum flow through the nozzle. Consequently. it is possible to enhance cohesion of the interlaced filaments by using a speed resumption device such as the plate 19 at the outlet 18 of the interlacing chamber.
  • the regularity of the interlace may be improved by utilizing the nozzle according to this invention since the nozzle can function using various arrangements such as activating two of the turbulence-causing jets with two nonturbulence causing jets or any symmetrical or asymmetrical mix of activated turbulence-causing jets. Consequently, it is possible to obtain yarns having different configurations of interlace by using a single nozzle 10. It is also possible, with the nozzle 10 of the present invention, to produce effects such as false twist, etc.
  • the nozzle utilized in the instant invention may interlace many types of multifabric yarns such as continuous yarns, spun products of fibers, yarns which are either flat or textured, yarns which are natural or yarns which are made of artificial or synthetic materials.
  • An apparatus for interlacing a multifilament strand of yarn under the influence of an expanding fluid comprising:
  • an interlacing chamber through which the yarn passes as the yarn is interlaced
  • the chamber includes a treatment zone defined by a surface of revolution about an axis, the cavity having a diameter and a height wherein the height is at most equal to the diameter;
  • the means for introducing a rotational component, of motion to the fluid includes a turbulence chamber coaxial with the conduit in which there is an axial intake for a principal stream of fluid and a generally tangential intake for an auxiliary stream of fluid which introduces the rotational component to the principal stream.
  • conduits are distributed in equal spacing about the treatment zone with the axes thereof contained in the same plane which plane extends normal to the axis of the treatment zone.
  • conduits are four in number and the axes of the conduits are spaced apart.
  • the apparatus of claim 15 further including means for inserting the yarn aligned with the inlet.
  • the apparatus is made of two separate parts which are joined along an area which intersects the interlacing chamber so that the yarn may be placed in the interlacing chamber upon separating the two parts and may be surrounded by the interlacing chamber upon joining the two parts.
  • conduits includes means for injecting fluid having nonturbulent flow into the cavity at the same level as the conduits injecting fluid having a rotary component.

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  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Yarns And Mechanical Finishing Of Yarns Or Ropes (AREA)
US438684A 1973-03-05 1974-02-01 Apparatus for interlacing filaments of multifilament yarns Expired - Lifetime US3875625A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US05/532,238 US3958310A (en) 1973-03-05 1974-12-12 Method for interlacing filaments of multifilament yarns

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7308029A FR2220607B1 (de) 1973-03-05 1973-03-05

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US3875625A true US3875625A (en) 1975-04-08

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US (1) US3875625A (de)
JP (1) JPS5046954A (de)
CH (1) CH560260A5 (de)
DE (1) DE2410191A1 (de)
ES (1) ES423912A1 (de)
FR (1) FR2220607B1 (de)
GB (1) GB1436050A (de)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3968638A (en) * 1975-06-09 1976-07-13 E. I. Du Pont De Nemours And Company Product and process
US4295253A (en) * 1978-10-12 1981-10-20 Basf Aktiengesellschaft Process and apparatus for texturizing filament bundles
US4691947A (en) * 1985-01-19 1987-09-08 Barmag Ag Yarn texturing nozzle

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1592646A (en) * 1976-12-01 1981-07-08 Ici Ltd Yarn treatment
DE3019302A1 (de) * 1980-05-21 1981-11-26 Hoechst Ag, 6000 Frankfurt Verwirbelungsduese
JPS6088146A (ja) * 1983-10-17 1985-05-17 帝人株式会社 糸条の流体交絡処理ノズル
DE3661740D1 (en) * 1985-01-19 1989-02-16 Barmag Barmer Maschf Yarn texturing jet
US5091030A (en) * 1985-07-15 1992-02-25 E. I. Du Pont De Nemours And Company Lightly bonded polyamide yarns and process therefor
MX169178B (es) * 1985-07-15 1993-06-24 Du Pont Hilos de poliamida ligeramente ligados y procedimiento para tratar las mismas
DE9307835U1 (de) * 1993-05-25 1993-07-22 Fag Kugelfischer Georg Schaefer Kgaa, 8720 Schweinfurt, De

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2938257A (en) * 1957-07-23 1960-05-31 American Viscose Corp Bulked yarn manufacture
US3167847A (en) * 1961-11-28 1965-02-02 American Enka Corp Treatment of multi-filament yarn
US3364537A (en) * 1965-09-07 1968-01-23 Du Pont Apparatus for interlacing multifilament yarn
US3525133A (en) * 1967-05-10 1970-08-25 Ici Ltd Intermingling jets for multifilament yarn
US3673648A (en) * 1970-09-01 1972-07-04 Firestone Tire & Rubber Co No-twist entanglement of filament and apparatus therefor

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH485049A (de) * 1967-02-01 1970-01-31 Glanzstoff Ag Vorrichtung zur Verwirbelung der Einzelfäden von multifilen Garnen und Fäden
FR1523271A (fr) * 1967-03-10 1968-05-03 Rhodiaceta Nouveau fil, procédé et dispositif pour le fabriquer

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2938257A (en) * 1957-07-23 1960-05-31 American Viscose Corp Bulked yarn manufacture
US3167847A (en) * 1961-11-28 1965-02-02 American Enka Corp Treatment of multi-filament yarn
US3364537A (en) * 1965-09-07 1968-01-23 Du Pont Apparatus for interlacing multifilament yarn
US3525133A (en) * 1967-05-10 1970-08-25 Ici Ltd Intermingling jets for multifilament yarn
US3673648A (en) * 1970-09-01 1972-07-04 Firestone Tire & Rubber Co No-twist entanglement of filament and apparatus therefor

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3968638A (en) * 1975-06-09 1976-07-13 E. I. Du Pont De Nemours And Company Product and process
US4295253A (en) * 1978-10-12 1981-10-20 Basf Aktiengesellschaft Process and apparatus for texturizing filament bundles
US4691947A (en) * 1985-01-19 1987-09-08 Barmag Ag Yarn texturing nozzle

Also Published As

Publication number Publication date
CH560260A5 (de) 1975-03-27
GB1436050A (en) 1976-05-19
FR2220607A1 (de) 1974-10-04
JPS5046954A (de) 1975-04-26
ES423912A1 (es) 1976-05-16
FR2220607B1 (de) 1975-10-31
DE2410191A1 (de) 1974-09-12

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