GB823509A - Spinning jets and the production thereof - Google Patents

Spinning jets and the production thereof

Info

Publication number
GB823509A
GB823509A GB6399/58A GB639958A GB823509A GB 823509 A GB823509 A GB 823509A GB 6399/58 A GB6399/58 A GB 6399/58A GB 639958 A GB639958 A GB 639958A GB 823509 A GB823509 A GB 823509A
Authority
GB
United Kingdom
Prior art keywords
insert
diameter
face
plate
hole
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB6399/58A
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.)
Glanzstoff AG
Vereinigte Glanzstoff Fabriken AG
Original Assignee
Glanzstoff AG
Vereinigte Glanzstoff Fabriken AG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Glanzstoff AG, Vereinigte Glanzstoff Fabriken AG filed Critical Glanzstoff AG
Publication of GB823509A publication Critical patent/GB823509A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/16Making specific metal objects by operations not covered by a single other subclass or a group in this subclass plates with holes of very small diameter, e.g. for spinning or burner nozzles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/24Making specific metal objects by operations not covered by a single other subclass or a group in this subclass dies
    • 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
    • D01D4/027Spinnerettes containing inserts
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49428Gas and water specific plumbing component making
    • Y10T29/49432Nozzle making
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49945Assembling or joining by driven force fit

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Textile Engineering (AREA)
  • Spinning Methods And Devices For Manufacturing Artificial Fibers (AREA)

Abstract

A spinneret or spinning jet for melt-spinning comprises a relatively thick face-plate drilled with holes consisting of an inlet portion with a cylindrical wall, an intermediate portion of smaller diameter with a cylindrical wall and an outlet portion of smaller diameter than the intermediate portion, the three cylindrical portions being connected by two frusto-conical intermediate portions having walls tapering in the outlet direction, each hole in the face-plate being provided with a pre-drilled insert member the length of which is much less than the thickness of the face-plate and which has a cylindrical outlet end portion with an external diameter somewhat smaller than the diameter of the outlet portion of the hole in the faceplate, the remaining or inlet portion of the insert having externally a frusto-conical shape which narrows towards the outlet portion with <PICT:0823509/IV (a)/1> <PICT:0823509/IV (a)/2> <PICT:0823509/IV (a)/3> <PICT:0823509/IV (a)/4> <PICT:0823509/IV (a)/5> <PICT:0823509/IV (a)/6> <PICT:0823509/IV (a)/7> a very slight taper and ha mean external diameter equal to that of the intermediate cylindrical portion of the hole in the face-plate, the hole drilled in the insert having a greater diameter in the inlet portion of the insert than that of the outlet portion of the insert, these two portions of the insert bore, if desired being joined by an intermediate frusto-conical portion of the bore tapering towards the outlet portion of the bore. As shown in Figs. 1 and 2, inserts comprising a lower cylindrical portion 1 and an upper cylindrical portion 2 with a slight taper in a downward direction have a pre-drilled jet aperture 3 communicating with an inlet bore 4. The external diameter of the portion 1 is 1 mm. and the diameters of the portion 2 at the top and bottom are 1.65 and 1.60 mm. respectively. As shown in Fig. 3, the hole or bore 5 drilled in a face-plate 6 has a diameter d of 3 mm., a diameter e of 1.625 mm. and a diameter f of 1.05 mm. Since the diameter of the portion f is slightly larger than the external diameter a of the portion 1 of the insert, the portion 1 is a sliding fit in the portion of the hole 5 in the face-plate having a diameter f. Therefore no deformation of the extrusion orifice 3 drilled in the insert occurs when the insert is pressed into the hole 5 in the face-plate. Since the diameter of the portion e of the hole 5 is the same as the mean diameter of the tapered portion of the insert, a good seal is established between the insert and the face-plate when the insert is pressed into the hole 5 in the face-plate. Fig. 4 shows an insert 7 in position after having been pressed into the drilled hole 5 of the face-plate 6 by a punch. The portion 8 of the latter (see Fig. 5) is a sliding fit in the inlet portion d of the hole 5 in the face-plate 6, while the portion 9 of the punch is a cylindrical round-edged protuberance which is a sliding fit in the inlet bore 4 of the insert 7 and thus functions as a guide to prevent tilting of the insert when it is pressed into position. Fig. 7 shows a form of punch by means of which the insert is additionally sealed into the spinneret face-plate in which the guide protuberance 10 is not cylindrical but is rounded, and the adjoining portion 11 does not have a flat horizontal lower surface but has an inclined surface 12 which is designed to promote flow of the material of the face-plate surrounding the hole 5 to the top of the insert when the latter is driven home by the punch as shown in Figs. 8 and 9. The diameter g of the portion 11 of the punch shown in Fig. 7 is somewhat larger than the diameter c of the portion of the insert shown in Fig. 1, e.g. g = 2 mm. and c = 1.65 mm. The inserts of the invention can be pressed into the holes in the thick face-plates of melt-spinning spinnerets from the inlet side without deformation of the extrusion orifices pre-drilled in the inserts and are thus particularly suitable when the extrusion orifices are of ultra-small diameter, i.e. below 125 mm .
GB6399/58A 1957-03-02 1958-02-27 Spinning jets and the production thereof Expired GB823509A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEV12068A DE1098155B (en) 1957-03-02 1957-03-02 Spinneret with inserts and device to push the inserts into the nozzle

Publications (1)

Publication Number Publication Date
GB823509A true GB823509A (en) 1959-11-11

Family

ID=7573725

Family Applications (1)

Application Number Title Priority Date Filing Date
GB6399/58A Expired GB823509A (en) 1957-03-02 1958-02-27 Spinning jets and the production thereof

Country Status (6)

Country Link
US (1) US3006026A (en)
BE (1) BE564637A (en)
CH (1) CH362485A (en)
DE (1) DE1098155B (en)
FR (1) FR1192066A (en)
GB (1) GB823509A (en)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3174183A (en) * 1962-04-16 1965-03-23 Us Rubber Co Spinneret plate
US3141358A (en) * 1962-05-09 1964-07-21 Du Pont Method for forming spinning orifices in spinneret plate structures
US3253301A (en) * 1963-01-14 1966-05-31 Monsanto Co Non-circular spinneret orifices
GB1023482A (en) * 1963-01-24 1966-03-23 Welwyn Plastics 1955 Ltd Improvements in coated fabrics
US3537135A (en) * 1964-01-09 1970-11-03 Celanese Corp Spinning apparatus
GB1096316A (en) * 1964-03-31 1967-12-29 Ici Ltd Improvements in or relating to spinnerets
US3303530A (en) * 1965-01-13 1967-02-14 Du Pont Spinnerette
US3381336A (en) * 1966-06-20 1968-05-07 Stanley C. Wells Melt spinning extrusion head system
GB1302584A (en) * 1970-06-23 1973-01-10
US3836081A (en) * 1973-05-14 1974-09-17 Goss Gas Inc Torch tip and method of fabricating the same
US3925525A (en) * 1973-08-10 1975-12-09 Celanese Corp Spinning method
US3913421A (en) * 1974-06-05 1975-10-21 Du Pont Method for installing a capillary insert in a passage through a spinneret
US4461191A (en) * 1983-02-03 1984-07-24 Ppg Industries, Inc. Method of preparing bushing tips
US5066215A (en) * 1988-08-29 1991-11-19 Corning Incorporated Extrusion die for forming thin-walled honeycomb structures
US5202072A (en) * 1989-02-16 1993-04-13 E. I. Du Pont De Nemours And Company Pitch carbon fiber spinning process
JPH0710471B2 (en) * 1989-09-25 1995-02-08 株式会社日立製作所 Concentric coupling method for precision parts composed of multiple members, and method for assembling fuel injection nozzle using the same
JP2510792B2 (en) * 1991-02-27 1996-06-26 京セラ株式会社 Spinneret
CN103266360A (en) * 2013-05-31 2013-08-28 吉铨精密机械(苏州)有限公司 Spinneret plate of thread casting belt head
CN103831600B (en) * 2014-03-17 2016-04-20 沈阳飞机工业(集团)有限公司 A kind of method of Multi-angle drilling jig processing

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1310509A (en) * 1918-01-12 1919-07-22 Harry Mortimer Specht Apparatus for making filament from viscid or viscous substance.
GB213138A (en) * 1923-04-23 1924-03-27 Leonard Angelo Levy Improvements in the production of artificial filaments
GB301081A (en) * 1927-11-25 1929-09-05 Henri Colomb Improvements in spinning nozzles for use in the manufacture of artificial silk
CH128690A (en) * 1927-11-25 1928-11-16 Henri Colomb Multiple supply chain, in particular for the artificial silk industry.
US2200583A (en) * 1937-05-03 1940-05-14 Cleo E Shepard Method of making bungs
US2464323A (en) * 1946-03-13 1949-03-15 Gen Motors Corp Punch for fluting gun-barrel chambers
US2686963A (en) * 1948-04-27 1954-08-24 Freyssinet Eugene Method of anchoring reinforcements
DE808872C (en) * 1948-10-02 1951-07-19 Degussa Spinneret for the production of fully synthetic threads
NL69191C (en) * 1949-11-23
AT176629B (en) * 1949-11-23 1953-11-10 Onderzoekings Inst Res Spinneret
US2683999A (en) * 1950-10-30 1954-07-20 Cameron Iron Works Inc Forging die
BE509641A (en) * 1951-03-01
US2843875A (en) * 1954-07-12 1958-07-22 Celanese Corp Spinnerette assembly

Also Published As

Publication number Publication date
US3006026A (en) 1961-10-31
DE1098155B (en) 1961-01-26
BE564637A (en)
CH362485A (en) 1962-06-15
FR1192066A (en) 1959-10-23

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