US3210451A - Spinnerettes - Google Patents

Spinnerettes Download PDF

Info

Publication number
US3210451A
US3210451A US72999A US7299960A US3210451A US 3210451 A US3210451 A US 3210451A US 72999 A US72999 A US 72999A US 7299960 A US7299960 A US 7299960A US 3210451 A US3210451 A US 3210451A
Authority
US
United States
Prior art keywords
section
cylindrical portion
jet
less
spinnerette
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
Application number
US72999A
Inventor
Jr John Albert Manning
Bishop Clarence Edward
Kight Vernon Glenn
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.)
Celanese Corp
Original Assignee
Celanese Corp
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
Priority to BE634685D priority Critical patent/BE634685A/xx
Application filed by Celanese Corp filed Critical Celanese Corp
Priority to US72999A priority patent/US3210451A/en
Priority to GB41758/61A priority patent/GB1006830A/en
Priority to DE19611435393 priority patent/DE1435393A1/en
Priority to FR880726A priority patent/FR1307243A/en
Priority to US415219A priority patent/US3227009A/en
Application granted granted Critical
Publication of US3210451A publication Critical patent/US3210451A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • DTEXTILES; PAPER
    • D01NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
    • D01DMECHANICAL METHODS OR APPARATUS IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS
    • D01D4/00Spinnerette packs; Cleaning thereof
    • D01D4/02Spinnerettes

Definitions

  • a further object of the invention is to provide novel jets and processes for the extrusion of particular solutions through said jets to achieve improved results.
  • the meeting angle is twice the angle between the orifice axis and a tangent to the divergent section at a location spaced interiorly of the interior end of the cylindrical portion by a distance equal to 100% of the diameter of the cylindrical portion.
  • jet thicknes is significantly greater than specified it becomes exceedingly difiicult to produce the orifices since the punching or drilling bits are so small that they break easily; since a jet for spinning even a very light weight, i.e., low denier, yarn contains dozens of orifices it will be appreciated that a jet production operation which results in frequent breakage will be quite costly.
  • the orifice is not cylindrical adjacent the outlet side of the spinnerette, it will then be essential that a tapered drill, for example, penetrate the face of the jet by an exact distance since variations in the extent of penetration will result in variations in the hole diameters; by utilizing a cylindrical outlet greater latitude in manufacture is permitted since the exact depth to which the non-cylindrical element enters the metal of the jet is not critical because the size and shape of the orifice is the same all along the cylindrical portion. This, of course, applies whether the cylindrical portion has a circular cross-section, i.e., a
  • the properties of the resulting cellulose triacetate filaments will be affected adversely, i.e., the tenacity and elongation will be lower. Even when spinning 10w denier fibers the linear speed of extrusion can exceed about 450 and often 550 meters per minute.
  • the novel jet permits the spinning speed to be increased at least 25% and usually in excess of 50% as contrasted with jets having meeting angles greater than about 65; the capacity of the equipment is thus increased with obvious advantage. Equally important, both wear and corrosion of the jet are reduced, the life of a jet being multiplied several times.
  • cellulose triacetate has reference to cellulose acetate having fewer than about 0.29 and preferably fewer than about 0.12 free hydroxyl group per anhydroglucose unit of the cellulose molecule, i.e., an acetyl value calculated as combined acetic acid by weight of at least about 59% and preferably at least about 61%.
  • its intrinsic viscosity ranges from about 1.5 to 2.5 and is preferably about 2 and it is present in the dope to a concentration ranging from about 20 to 25
  • the dope solvent may comprise other halogenated lower alkanes such as ethylene dichloride or propylene chloride.
  • the dope solvent comprises a lower alkanol such as methanol, ethanol, isopropanol, etc.
  • the preferred dope solvent is methylen chloride-methanol in the proportions of -10 by weight.
  • the shape of the divergent section no longer has such a marked effect on yarn properties, spinning speed and jet life.
  • the section of small meeting angle is preferably spaced from the jet inlet face by a section of larger meeting angle which can be produced with less breakage.
  • the sequence in which the sections are formed in the metal is from largest diameter to smallest diameter.
  • the most pointed, weakest tools need operate upon a minimum thickness of metal.
  • a conical punch of wide angle e.g., about 30 to and preferably about 50 to 60" is pressed into the metal.
  • the narrower angle punch is pressed into the metal to the requisite distance so that the subsequently produced cylindrical section will be of the desired height.
  • each depression serves as a seat to ensure proper positioning of the tool for producing the next depression.
  • This technique is applicable even for orifices with relatively Wide meeting angles; advantageously the difference between the meeting angles of successive sections is at least about 20 although close spacing of holes may sometimes render it impractical to observe this preference.
  • two or more of these steps may be performed simultaneously by employing a suitably profiled tool, e.g., a tool having a frusto-conical portion surmounted by a smaller angle conical portion and/ or a cylindrical portion.
  • a suitably profiled tool e.g., a tool having a frusto-conical portion surmounted by a smaller angle conical portion and/ or a cylindrical portion.
  • a curved portion having, for example, a hyperbolic or parabolic profile.
  • This curved portion could also be surmounted by a cylindrical portion, if desired. It will be appreciated that where two or more portions are included on a single tool, the leading portion necessarily will have to penerate a greater thickness of metal than when individual tools are employed with the tools applied in sequence starting with the widest.
  • the jet life is increased if the customary plating step is omitted. Omission of the plating step obviously also effects a considerable saving in the cost of manufacturing jets.
  • the jet can be made of any of the usual materials, conventional stainless steels such as 304 and particularly 316 being especially satisfactory.
  • FIG. 1 is a plan view of a spinnerette in accordance with the present invention
  • FIG. 2 is a sectional view taken along line 22 of FIG. 1;
  • FIGS. 3, 4, and 5 are sectional views showing the sequence in forming the orifices in the spinnerette of FIG. 1;
  • FIGS. 6 and 7 are sectional views showing how to determine the meeting angle for countersinks which are not conical.
  • FIG. 8 isa schematic illustration of a dry spinning operation.
  • FIG. 1 there is shown a spinnerette or jet 11 comprising a stainless steel cup 12 provided with orifices or apertures 13.
  • the apertures are formed by punching or drilling a conical countersink 14 to the desired depth in the metal of cup 12 (FIG. 3).
  • a second more pointed countersink 15 is formed (FIG. 4).
  • a cylindrical portion 16 is punched through to the outlet face of the jet 11 (FIG. 5) to produce the orifice 13; the cylindrical portion can also be formed by punching or broaching.
  • countersink 15 in FIG. 4 could extend all the way through the face of the jet 11; the lowermost portion thereof would be eliminated when forming the cylindrical portion 16.
  • the demarcation between countersinks 14 and 15 will generally be spaced from the inlet face of the jet by a distance ranging from about 50 to 90% and preferably about 70 to 85% of the jet thickness; since the apex will be cut away, the depth of countersink 14 in FIG. 3 will be somewhat greater than these ranges, e.g. about 60 to 100% and preferably about 75 to 95% of the metal thickness.
  • the height of section 15 in FIG. 5 generally ranges from about 5 to 30% and preferably from about 10 to of the jet thickness; its exact height will be somewhat dependent on the diameter of portion 16, generally being at least 0.5 and preferably about 2 to 4 times the diameter of portion 16.
  • FIGS. 6 and 7 show how the meeting angles are measured for non-conical countersinks, whether hyperbolic (FIG. 6)
  • FIG. 7 The elevation A at which the orifices ceases to be cylindrical is marked.
  • the width of the orifice at elevation A is determined and 100% of this width is marked above A as plane B perpendicular to the axis of the orifice. Tangents are drawn at the two points where B intersects the outline of the orifice and the meeting angle a is the angle between these tangents.
  • FIG. 8 there is shown a dry spinning cabinet 17 to which dope is supplied through a pipe 18, being extruded through spinnerette 11 of FIG. 5 with no intervening plating of the spinnerette.
  • Hot air is admitted to the cabinet 17 at 19 and is exhausted at 20 along with vapors of the dope solvent.
  • the filaments 21 leaving spinnerette 11 pass about a guide 22 and leave the cabinet at 23 being pulled as a yarn 24 by draw rolls 25.
  • the yarn 24 passes through a guide 26 and is twisted and taken up on a bobbin 27 by a conventional collector such as ring spinner 28.
  • Example A 22% solution of cellulose triacetate, acetyl value 61% and intrinsic viscosity of 2, in 919 methylen-chloride methanol is extruded through a 316 stainless steel spinnerette having 15 orifices as shown in FIG. 5.
  • Cup 12 is 790 microns thick
  • frusto-conical countersink 14 has an angle of 65 and extends into the metal a distance of 680 mircons
  • frusto-conical countersink 15 has an angle of 33 and is microns high and cylindrical portion 16 has a diameter of 36 microns and a height of 25 microns.
  • the resulting filaments pass through air at 74 C., are withdrawn from the cabinet at a linear speed of 550 meters per minute and are taken up on a bobbin.
  • the novel yarn has a 5% greater tenacity and a 10% greater elongation; if yarn is spun at about 300 meters per minute with the novel jet, the physical properties are further improved.
  • the life of the jet is increased several thousand percent. Similar results are achieved with variations in the shape of countersink 14 but the orifices are more difficult to produce.
  • An article of manufacture comprising a spinnerette less than about 1000 microns thick and provided with at least one orifice extending therethrough, said orifice including a cylindrical portion adjacent the outlet face of said spinnerette having a height ranging from about 0.25 to 5 times its diameter, a first frustoconical section divergent toward the inlet face of said spinnerette and communicating with said cylindrical portion, said first frustoconical section having an apex angle of less than about 60 and ranging in height from about 5 to 30% of the thickness of said spinnerette, and a second frustoconical section divergent toward the inlet face of said spinnerette and communicating with said first frustoconical section, said second frustoconical section having an apex angle of at least about greater than said first frustoconical section and ranging in height from about 50 to 90% of the thickness of said spinnerette.
  • a first frustoconical portion divergent toward the upstream end of said confined section and communicating with said cylindrical portion, said first frustoconical portion having an apex angle less than about 60 and ranging in length from about 5 to 30% of the thickness of said confined section, and a sec- 0nd frustoconical portion divergent toward the upstream end of said confined section and communicating with said first frustoconical portion, said second frustoconical portion having an apex angle of at least about 20 greater than that of said first frustoconical portion and ranging in length from about to 90% of the length of said confined section, the linear extrusion speed of said solution being at least about 450 meters per minute.
  • An article of manufacture comprising a spinnerette having a thickness of less than about 1000 microns and provided with at least one orifice extending therethrough, said orifice including a cylindrical portion adjacent the outlet face of said spinnerette having a height ranging from about 0.5 to 1.5 times its diameter, a first frustoconical section divergent toward the inlet face of said spinnerette and communicating with said cylindrical porton, said first frustoconical section having an apex of less than about 35 and ranging in height from about 10 to 20% of the thickness of said spinnerette, and a second frustoconical section divergent toward the inlet face of said spinnerette and communicating with said first frustoconical section, said second frustoconical section having an apex angle at least about 20 greater than said first frustoconical section and ranging in height from about to of the thickness of said spinnerette.

Description

United States Patent 3,210,451 SPINNERETTES John Albert Manning, Jr., Charlotte, N.C., Clarence Edward Bishop, Narrows, Va., and Vernon Glenn Kight, La Vale, Md., assignors to Celanese Corporation of America, New York, N.Y., a corporation of Delaware Filed Dec. 1, 1960, Ser. No. 72,999 6 Claims. (Cl. 264-200) The present invention relates to novel jets or spinnerettes for the spinning of synthetic filaments.
In the wet or dry spinning of synthetic filaments, viscous solutions of filament-forming material are. extruded through a jet or spinnerette provided with extremely fine capillary orifices having diameters of less than a few dozen microns. The manufacure of such jets requires great care and precision and is quite costly.
It is accordingly an object of the present invention to provide an improved process for the manufacture of jets provided with fine capillary orifices.
A further object of the invention is to provide novel jets and processes for the extrusion of particular solutions through said jets to achieve improved results.
Other objects and advantages of the invention will become apparent from the detailed description of the invention which follows taken in conjunction with the appended claims, wherein all parts are by weight unles otherwise specified.
In accordance with one aspect of the present invention, it has been found that when spinning solutions of cel lulose triacetate in a solvent principally comprising a halogenated hydrocarbon such as methylene chloride through a jet having orifices less than about 0.02 mm. in minimum area, best results are achieved if the jet thickness is small, e.g., desirably less than about 1500 microns and preferably less than about 1000 microns, if the orifice adjacent the outlet side of the spinnerette is cylindrical, i.e. generated by a line parallel to the axis, advantageously for a distance ranging from about 0.25 to 5 and preferably from about 0.5 to 1.5 times the diameter of the outlet, and if the cylindrical portion merges smoothly with a section divergent toward the inlet side and meeting the cylindrical portion at a small angle, advantageously less than about 60 and preferably less than about 35 The meeting angle is twice the angle between the orifice axis and a tangent to the divergent section at a location spaced interiorly of the interior end of the cylindrical portion by a distance equal to 100% of the diameter of the cylindrical portion. By so selecting the location at which the meeting angle is measured, account is taken of changes in curvature of the divergent section, as where it is hyperbolic or parabolic.
If the jet thicknes is significantly greater than specified it becomes exceedingly difiicult to produce the orifices since the punching or drilling bits are so small that they break easily; since a jet for spinning even a very light weight, i.e., low denier, yarn contains dozens of orifices it will be appreciated that a jet production operation which results in frequent breakage will be quite costly. If the orifice is not cylindrical adjacent the outlet side of the spinnerette, it will then be essential that a tapered drill, for example, penetrate the face of the jet by an exact distance since variations in the extent of penetration will result in variations in the hole diameters; by utilizing a cylindrical outlet greater latitude in manufacture is permitted since the exact depth to which the non-cylindrical element enters the metal of the jet is not critical because the size and shape of the orifice is the same all along the cylindrical portion. This, of course, applies whether the cylindrical portion has a circular cross-section, i.e., a
3,210,451 Patented Oct. 5, 1965 right-circular cylinder, a triangular cross-section, a square cross-section, etc.
If the meeting angle is increased beyond the indicated values the properties of the resulting cellulose triacetate filaments will be affected adversely, i.e., the tenacity and elongation will be lower. Even when spinning 10w denier fibers the linear speed of extrusion can exceed about 450 and often 550 meters per minute. For a given level of physical properties and Wear of the jet the novel jet permits the spinning speed to be increased at least 25% and usually in excess of 50% as contrasted with jets having meeting angles greater than about 65; the capacity of the equipment is thus increased with obvious advantage. Equally important, both wear and corrosion of the jet are reduced, the life of a jet being multiplied several times. Not only does this effect a saving in jets but it reduces the number of times the equipment must be shut down to change jets. That the meeting angle has this effect is most surprising since in spinning acetone dopes, e.g., conventional secondary cellulose acetate, it makes relatively little difference whether the meeting angle is large or small and large angles have accordingly been preferred commercially because of the greater likelihood of breaking sharply tapered bits and punches needed for making the small angles.
As employed herein cellulose triacetate has reference to cellulose acetate having fewer than about 0.29 and preferably fewer than about 0.12 free hydroxyl group per anhydroglucose unit of the cellulose molecule, i.e., an acetyl value calculated as combined acetic acid by weight of at least about 59% and preferably at least about 61%. Advantageously its intrinsic viscosity ranges from about 1.5 to 2.5 and is preferably about 2 and it is present in the dope to a concentration ranging from about 20 to 25 In place of methylene chloride, the dope solvent may comprise other halogenated lower alkanes such as ethylene dichloride or propylene chloride. Advantageously, up to about 15% by weight of the dope solvent comprises a lower alkanol such as methanol, ethanol, isopropanol, etc. The preferred dope solvent is methylen chloride-methanol in the proportions of -10 by weight.
In accordance with another aspect of the present invention, it has been found that beyond the point at which the meeting angle is determined, the shape of the divergent section no longer has such a marked effect on yarn properties, spinning speed and jet life. In addition, if it is desired to employ a constant narrow angle all the way from the cylindrical portion to the inlet face of the jet, experiments have shown that the necessarily sharply pointed tool breaks frequently in penetrating the full metal thickness. Accordingly, the section of small meeting angle is preferably spaced from the jet inlet face by a section of larger meeting angle which can be produced with less breakage.
The sequence in which the sections are formed in the metal is from largest diameter to smallest diameter. In this manner the most pointed, weakest tools need operate upon a minimum thickness of metal. Thus, for example, a conical punch of wide angle, e.g., about 30 to and preferably about 50 to 60", is pressed into the metal. Then the narrower angle punch is pressed into the metal to the requisite distance so that the subsequently produced cylindrical section will be of the desired height. It will be noted that by proceeding in this manner each depression serves as a seat to ensure proper positioning of the tool for producing the next depression. This technique is applicable even for orifices with relatively Wide meeting angles; advantageously the difference between the meeting angles of successive sections is at least about 20 although close spacing of holes may sometimes render it impractical to observe this preference.
If desired, two or more of these steps may be performed simultaneously by employing a suitably profiled tool, e.g., a tool having a frusto-conical portion surmounted by a smaller angle conical portion and/ or a cylindrical portion. In place of two portions which are straight sided, such as cones, there may be substituted for either or for both, individually or jointly, a curved portion having, for example, a hyperbolic or parabolic profile. This curved portion could also be surmounted by a cylindrical portion, if desired. It will be appreciated that where two or more portions are included on a single tool, the leading portion necessarily will have to penerate a greater thickness of metal than when individual tools are employed with the tools applied in sequence starting with the widest.
In accordance with another aspect of the invention, it has been found that when spinning solutions containing large amounts of corrosive liquids such as methylene chloride, surprisingly the jet life is increased if the customary plating step is omitted. Omission of the plating step obviously also effects a considerable saving in the cost of manufacturing jets. The jet can be made of any of the usual materials, conventional stainless steels such as 304 and particularly 316 being especially satisfactory.
The invention will be further described with reference to the accompanying drawing, wherein:
FIG. 1 is a plan view of a spinnerette in accordance with the present invention;
FIG. 2 is a sectional view taken along line 22 of FIG. 1;
FIGS. 3, 4, and 5 are sectional views showing the sequence in forming the orifices in the spinnerette of FIG. 1;
FIGS. 6 and 7 are sectional views showing how to determine the meeting angle for countersinks which are not conical; and
FIG. 8 isa schematic illustration of a dry spinning operation.
Referring now more particularly to the drawing, in FIG. 1 there is shown a spinnerette or jet 11 comprising a stainless steel cup 12 provided with orifices or apertures 13. As shown in FIGS. 3, 4 and 5, the apertures are formed by punching or drilling a conical countersink 14 to the desired depth in the metal of cup 12 (FIG. 3). With the apex of countersink 14- as a guide, a second more pointed countersink 15 is formed (FIG. 4). With the apex of countersink 15 as a guide, a cylindrical portion 16 is punched through to the outlet face of the jet 11 (FIG. 5) to produce the orifice 13; the cylindrical portion can also be formed by punching or broaching.
The exact depths to which the apices of countersinks 14 and 15 project are not the controlling features since it is the location of the demarcation zones in FIG. 5 which is important. Thus, for example, countersink 15 in FIG. 4 could extend all the way through the face of the jet 11; the lowermost portion thereof would be eliminated when forming the cylindrical portion 16. The demarcation between countersinks 14 and 15 will generally be spaced from the inlet face of the jet by a distance ranging from about 50 to 90% and preferably about 70 to 85% of the jet thickness; since the apex will be cut away, the depth of countersink 14 in FIG. 3 will be somewhat greater than these ranges, e.g. about 60 to 100% and preferably about 75 to 95% of the metal thickness. The height of section 15 in FIG. 5 generally ranges from about 5 to 30% and preferably from about 10 to of the jet thickness; its exact height will be somewhat dependent on the diameter of portion 16, generally being at least 0.5 and preferably about 2 to 4 times the diameter of portion 16.
Where the countersinks 14 and 15 are conical their meeting angles are obviously easy to measure. FIGS. 6 and 7 show how the meeting angles are measured for non-conical countersinks, whether hyperbolic (FIG. 6)
or parabolic (FIG. 7). The elevation A at which the orifices ceases to be cylindrical is marked. The width of the orifice at elevation A is determined and 100% of this width is marked above A as plane B perpendicular to the axis of the orifice. Tangents are drawn at the two points where B intersects the outline of the orifice and the meeting angle a is the angle between these tangents.
In FIG. 8 there is shown a dry spinning cabinet 17 to which dope is supplied through a pipe 18, being extruded through spinnerette 11 of FIG. 5 with no intervening plating of the spinnerette. Hot air is admitted to the cabinet 17 at 19 and is exhausted at 20 along with vapors of the dope solvent. The filaments 21 leaving spinnerette 11 pass about a guide 22 and leave the cabinet at 23 being pulled as a yarn 24 by draw rolls 25. The yarn 24 passes through a guide 26 and is twisted and taken up on a bobbin 27 by a conventional collector such as ring spinner 28.
The invention will be further described in the following illustrative example.
Example A 22% solution of cellulose triacetate, acetyl value 61% and intrinsic viscosity of 2, in 919 methylen-chloride methanol is extruded through a 316 stainless steel spinnerette having 15 orifices as shown in FIG. 5. Cup 12 is 790 microns thick, frusto-conical countersink 14 has an angle of 65 and extends into the metal a distance of 680 mircons, frusto-conical countersink 15 has an angle of 33 and is microns high and cylindrical portion 16 has a diameter of 36 microns and a height of 25 microns. The resulting filaments pass through air at 74 C., are withdrawn from the cabinet at a linear speed of 550 meters per minute and are taken up on a bobbin. As contrasted with yarn spun at about 300 meters per minute from a jet in which countersink 15 is omitted, the novel yarn has a 5% greater tenacity and a 10% greater elongation; if yarn is spun at about 300 meters per minute with the novel jet, the physical properties are further improved. In addition, the life of the jet is increased several thousand percent. Similar results are achieved with variations in the shape of countersink 14 but the orifices are more difficult to produce.
It is to be understood that the foregoing detailed description is given merely by way of illustration and that many variations may be made therein without departing from the spirit of our invention.
Having described our invention what we desire to secure by Letters Patent is:
1. The process which comprises extruding a solution of cellulose triacetate in a solvent principally comprising a halogenated hydrocarbon in the form of a stream having a confined section less than about 1500 microns long and including a cylindrical portion adjacent its downstream end and a section divergent toward its upstream end and communicating with said cylindrical portion, the meeting angle of said divergent section being less than about 60 and the cross-sectional area of said cylindrical portion being about 0.02 mm.
2. The process which comprises extruding a solution of cellulose triactaete in a solvent principally comprising a halogenated hydrocarbon in the form of a stream having a confined section less than about 1500 microns long and including at its downstream end a cylindrical portion having a cross-sectional area of less than about 0.02 mm. and about 0.25 to 5 times its diameter in length and a section divergent toward the upstream end of said confined section and communicating with said cylindrical portion at a meeting angle of less than about 60, the linear extrusion speed of said solution being at least about 450 meters per minute.
3. The process which comprises extruding a solution of cellulose triacetate in a solvent comprising methylene chloride and up to about 15% by weight of a lower alkanol in the form of a stream having a confined section less than about 1000 microns long having at its downstream end a cylindrical portion having a cross-sectional area of less than about 0.02 mm. and about 0.5 to 1.5 times its diameter in length and a section divergent toward the upstream end of said confined section and communicating with said cylindrical portion, the meeting angle of said divergent section being less than about 35 and the linear extrusion speed of said solution being at least 450 meters per minute.
4. An article of manufacture comprising a spinnerette less than about 1000 microns thick and provided with at least one orifice extending therethrough, said orifice including a cylindrical portion adjacent the outlet face of said spinnerette having a height ranging from about 0.25 to 5 times its diameter, a first frustoconical section divergent toward the inlet face of said spinnerette and communicating with said cylindrical portion, said first frustoconical section having an apex angle of less than about 60 and ranging in height from about 5 to 30% of the thickness of said spinnerette, and a second frustoconical section divergent toward the inlet face of said spinnerette and communicating with said first frustoconical section, said second frustoconical section having an apex angle of at least about greater than said first frustoconical section and ranging in height from about 50 to 90% of the thickness of said spinnerette.
5. The process which comprises extruding a solution of cellulose triacetate in a solvent comprising methylene chloride and up to about 15% by weight of a lower alkanol in the form of a stream having a confined section less than about 1000 microns long including at its downstream end a cylindrical portion with a cross-sectional area of less than about 0.02 mm. and about 0.5 to 1.5 times its diameter in length, a first frustoconical portion divergent toward the upstream end of said confined section and communicating with said cylindrical portion, said first frustoconical portion having an apex angle less than about 60 and ranging in length from about 5 to 30% of the thickness of said confined section, and a sec- 0nd frustoconical portion divergent toward the upstream end of said confined section and communicating with said first frustoconical portion, said second frustoconical portion having an apex angle of at least about 20 greater than that of said first frustoconical portion and ranging in length from about to 90% of the length of said confined section, the linear extrusion speed of said solution being at least about 450 meters per minute.
6. An article of manufacture comprising a spinnerette having a thickness of less than about 1000 microns and provided with at least one orifice extending therethrough, said orifice including a cylindrical portion adjacent the outlet face of said spinnerette having a height ranging from about 0.5 to 1.5 times its diameter, a first frustoconical section divergent toward the inlet face of said spinnerette and communicating with said cylindrical porton, said first frustoconical section having an apex of less than about 35 and ranging in height from about 10 to 20% of the thickness of said spinnerette, and a second frustoconical section divergent toward the inlet face of said spinnerette and communicating with said first frustoconical section, said second frustoconical section having an apex angle at least about 20 greater than said first frustoconical section and ranging in height from about to of the thickness of said spinnerette.
References Cited by the Examiner UNITED STATES PATENTS 2,266,363 12/41 Graves 18-8 2,618,989 11/52 Cupler 76-107 2,742,667 4/56 Clouzeau et al. 18-8 2,879,676 3/59 Burkhardt et a1. 76107 2,982,598 5/61 Downing 18--54 ALEXANDER H. BRODMERKEL, Primary Examiner.
WILLIAM J. STEPHENSON, MICHAEL V. BRINDISI,
Examiners.

Claims (1)

1. THE PROCESS WHICH COMPRISES EXTRUDING A SOLUTION OF CELLULOSE TRIACTEATE IN A SOLVENT PRINCIPALLY COMPRISING A HALOGENATED HYDROCARBON IN THE FOMR O F A STREAM HAVING A CONFINED SECTION LESS THAN ABOUT 1500 MICRONS LONG AND INCLUDING A CYLINDRICAL PORTION ADJACENT ITS DOWNSTREAM END AND A SECTION DIVERGENT TOWARD ITS UPSTREAM END AND COMMUNICATING WITH SAID CYLINDRICAL PORITON, THE MEETING ANGLE OF SAID DIVERGENT SECTION BEING LESS THAN ABOUT 60* AND THE CROSS-SECTIONAL AREA OF SAID CYLINDRICAL PORTION BEING ABOUT 0.02 MM.2.
US72999A 1960-12-01 1960-12-01 Spinnerettes Expired - Lifetime US3210451A (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
BE634685D BE634685A (en) 1960-12-01
US72999A US3210451A (en) 1960-12-01 1960-12-01 Spinnerettes
GB41758/61A GB1006830A (en) 1960-12-01 1961-11-22 Spinnerets for artificial filament manufacture
DE19611435393 DE1435393A1 (en) 1960-12-01 1961-11-30 Spinneret
FR880726A FR1307243A (en) 1960-12-01 1961-12-01 Production of synthetic filaments
US415219A US3227009A (en) 1960-12-01 1964-11-05 Spinnerettes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US72999A US3210451A (en) 1960-12-01 1960-12-01 Spinnerettes

Publications (1)

Publication Number Publication Date
US3210451A true US3210451A (en) 1965-10-05

Family

ID=22111074

Family Applications (1)

Application Number Title Priority Date Filing Date
US72999A Expired - Lifetime US3210451A (en) 1960-12-01 1960-12-01 Spinnerettes

Country Status (1)

Country Link
US (1) US3210451A (en)

Cited By (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3303530A (en) * 1965-01-13 1967-02-14 Du Pont Spinnerette
US3846377A (en) * 1971-11-12 1974-11-05 Allied Chem Method of producing polyethylene terephthalate fibers
US3925525A (en) * 1973-08-10 1975-12-09 Celanese Corp Spinning method
US4015924A (en) * 1973-08-10 1977-04-05 Celanese Corporation Spinning apparatus providing for essentially constant extensional strain rate
US4054468A (en) * 1976-09-07 1977-10-18 E. I. Du Pont De Nemours And Company Process of making a laminated spinneret
US4133620A (en) * 1976-08-27 1979-01-09 Didier Engineering Gmbh Polymer filament manufacturing device having reduced vertical size
US4225299A (en) * 1978-04-04 1980-09-30 Kling-Tecs, Inc. Apparatus for extruding yarn
US4282533A (en) * 1980-02-22 1981-08-04 Celanese Corporation Precision orifice nozzle devices for ink jet printing apparati and the process for their manufacture
US4430784A (en) * 1980-02-22 1984-02-14 Celanese Corporation Manufacturing process for orifice nozzle devices for ink jet printing apparati
US4724109A (en) * 1983-12-28 1988-02-09 Denki Kagaku Kogyo Kabushiki Kaisha Process for production of continuous inorganic fibers and apparatus therefor
US5066215A (en) * 1988-08-29 1991-11-19 Corning Incorporated Extrusion die for forming thin-walled honeycomb structures
US5259753A (en) * 1988-11-18 1993-11-09 E. I. Du Pont De Nemours And Company Spinneret capillaries
WO1994012703A1 (en) * 1992-12-03 1994-06-09 The Dow Chemical Company Method for spinning a polybenzazole fiber
US5330348A (en) * 1992-08-05 1994-07-19 E. I. Du Pont De Nemours And Company Spinneret for the production of hollow filaments
EP0656433A1 (en) * 1993-12-02 1995-06-07 Filtration Systems Inc. Nozzle plate for spinning
US5652001A (en) * 1993-05-24 1997-07-29 Courtaulds Fibres Limited Spinnerette
WO1997041284A1 (en) * 1996-04-29 1997-11-06 Akzo Nobel N.V. Process for producing a cellulose mould body
US6527532B1 (en) * 1995-12-27 2003-03-04 Trex Company, L.L.C. Apparatus for making a wood-plastic profile
US20060210666A1 (en) * 2003-03-12 2006-09-21 Boris Ouriev Die for forming extrudates of viscoelastic materials
US20070134478A1 (en) * 2003-12-20 2007-06-14 Corovin Gmbh Polyethylene-based, soft nonwoven fabric
US7410687B2 (en) 2004-06-08 2008-08-12 Trex Co Inc Variegated composites and related methods of manufacture
US20220010458A1 (en) * 2018-11-16 2022-01-13 Teknoweb Materials S.R.L. Spinneret block with unitary spinneret body and nozzles for use in the manufacturing of spun-blown fibers

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2266363A (en) * 1938-11-10 1941-12-16 Du Pont Apparatus for the production of filaments
US2618989A (en) * 1948-06-01 1952-11-25 John A Cupler Method of manufacturing orificed members
US2742667A (en) * 1951-11-08 1956-04-24 Rhodiaceta Spinnerets
US2879676A (en) * 1952-03-01 1959-03-31 Heraeus Gmbh W C Manufacture of spinning nozzles
US2982598A (en) * 1955-12-12 1961-05-02 British Celanese Manufacture of cellulose triacetate textile materials

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2266363A (en) * 1938-11-10 1941-12-16 Du Pont Apparatus for the production of filaments
US2618989A (en) * 1948-06-01 1952-11-25 John A Cupler Method of manufacturing orificed members
US2742667A (en) * 1951-11-08 1956-04-24 Rhodiaceta Spinnerets
US2879676A (en) * 1952-03-01 1959-03-31 Heraeus Gmbh W C Manufacture of spinning nozzles
US2982598A (en) * 1955-12-12 1961-05-02 British Celanese Manufacture of cellulose triacetate textile materials

Cited By (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3303530A (en) * 1965-01-13 1967-02-14 Du Pont Spinnerette
US3846377A (en) * 1971-11-12 1974-11-05 Allied Chem Method of producing polyethylene terephthalate fibers
US3925525A (en) * 1973-08-10 1975-12-09 Celanese Corp Spinning method
US4015924A (en) * 1973-08-10 1977-04-05 Celanese Corporation Spinning apparatus providing for essentially constant extensional strain rate
US4133620A (en) * 1976-08-27 1979-01-09 Didier Engineering Gmbh Polymer filament manufacturing device having reduced vertical size
US4137032A (en) * 1976-09-07 1979-01-30 E. I. Du Pont De Nemours And Company Corrosion-resistant spinneret
US4054468A (en) * 1976-09-07 1977-10-18 E. I. Du Pont De Nemours And Company Process of making a laminated spinneret
US4225299A (en) * 1978-04-04 1980-09-30 Kling-Tecs, Inc. Apparatus for extruding yarn
US4282533A (en) * 1980-02-22 1981-08-04 Celanese Corporation Precision orifice nozzle devices for ink jet printing apparati and the process for their manufacture
DE3105292A1 (en) * 1980-02-22 1982-01-14 Celanese Corp., 10036 New York, N.Y. INK-JET PRINTING DEVICE WITH A NOZZLE AND METHOD FOR PRODUCING THE NOZZLE
US4430784A (en) * 1980-02-22 1984-02-14 Celanese Corporation Manufacturing process for orifice nozzle devices for ink jet printing apparati
US4724109A (en) * 1983-12-28 1988-02-09 Denki Kagaku Kogyo Kabushiki Kaisha Process for production of continuous inorganic fibers and apparatus therefor
US5066215A (en) * 1988-08-29 1991-11-19 Corning Incorporated Extrusion die for forming thin-walled honeycomb structures
US5259753A (en) * 1988-11-18 1993-11-09 E. I. Du Pont De Nemours And Company Spinneret capillaries
US5330348A (en) * 1992-08-05 1994-07-19 E. I. Du Pont De Nemours And Company Spinneret for the production of hollow filaments
WO1994012703A1 (en) * 1992-12-03 1994-06-09 The Dow Chemical Company Method for spinning a polybenzazole fiber
US5652001A (en) * 1993-05-24 1997-07-29 Courtaulds Fibres Limited Spinnerette
EP0656433A1 (en) * 1993-12-02 1995-06-07 Filtration Systems Inc. Nozzle plate for spinning
US6527532B1 (en) * 1995-12-27 2003-03-04 Trex Company, L.L.C. Apparatus for making a wood-plastic profile
WO1997041284A1 (en) * 1996-04-29 1997-11-06 Akzo Nobel N.V. Process for producing a cellulose mould body
US20060210666A1 (en) * 2003-03-12 2006-09-21 Boris Ouriev Die for forming extrudates of viscoelastic materials
US7866973B2 (en) * 2003-03-12 2011-01-11 Buhler Ag Die for forming extrudates of viscoelastic materials
US20070134478A1 (en) * 2003-12-20 2007-06-14 Corovin Gmbh Polyethylene-based, soft nonwoven fabric
US20090136606A1 (en) * 2003-12-20 2009-05-28 Fiberweb Corovin Gmbh Device for the manufacture of polyethylene-based, soft nonwoven fabric
US20090133813A1 (en) * 2003-12-20 2009-05-28 Fiberweb Corovin Gmbh Method for the manufacture of polyethylene-based, soft nonwoven fabric
US8420557B2 (en) 2003-12-20 2013-04-16 Fiberweb Corovin Gmbh Polyethylene-based, soft nonwoven fabric
US7410687B2 (en) 2004-06-08 2008-08-12 Trex Co Inc Variegated composites and related methods of manufacture
US20220010458A1 (en) * 2018-11-16 2022-01-13 Teknoweb Materials S.R.L. Spinneret block with unitary spinneret body and nozzles for use in the manufacturing of spun-blown fibers

Similar Documents

Publication Publication Date Title
US3210451A (en) Spinnerettes
CA1079015A (en) Spinning method and apparatus
US2945739A (en) Process of melt spinning
US2816349A (en) Fibers and fabrics
US2370112A (en) Textile material
US2737831A (en) Process for making a spinneret
US3095607A (en) Spinneret assembly
KR940014934A (en) Polybenzazole Fiber Spinning Method
US3303530A (en) Spinnerette
EP0817873B1 (en) Method of producing cellulose fibres
US2804645A (en) Spinneret plate for melt spinning
US2341555A (en) Extrusion device
US3608041A (en) Spinning process
US3227009A (en) Spinnerettes
US4015924A (en) Spinning apparatus providing for essentially constant extensional strain rate
US4717331A (en) Spinning nozzle
US3397427A (en) Sealed vented insert spinneret
US3537135A (en) Spinning apparatus
US1980234A (en) Apparatus for the production of artificial threads of like products
US2465408A (en) Method and apparatus for spinning artificial fibers
US3839526A (en) Pentagrooved spinnerette orifices and process
US3608040A (en) Spinneret with stream guide
US3362265A (en) Method of making spinnerettes
US2798252A (en) Spinnerette
US3357048A (en) Spinnerette