AU607311B2 - Resilient polypropylene fibers and preparation thereof - Google Patents
Resilient polypropylene fibers and preparation thereof Download PDFInfo
- Publication number
- AU607311B2 AU607311B2 AU30781/89A AU3078189A AU607311B2 AU 607311 B2 AU607311 B2 AU 607311B2 AU 30781/89 A AU30781/89 A AU 30781/89A AU 3078189 A AU3078189 A AU 3078189A AU 607311 B2 AU607311 B2 AU 607311B2
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- AU
- Australia
- Prior art keywords
- fiber
- fibers
- range
- temperature
- residence time
- 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.)
- Ceased
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Classifications
-
- D—TEXTILES; PAPER
- D02—YARNS; MECHANICAL FINISHING OF YARNS OR ROPES; WARPING OR BEAMING
- D02G—CRIMPING OR CURLING FIBRES, FILAMENTS, THREADS, OR YARNS; YARNS OR THREADS
- D02G1/00—Producing crimped or curled fibres, filaments, yarns, or threads, giving them latent characteristics
- D02G1/12—Producing crimped or curled fibres, filaments, yarns, or threads, giving them latent characteristics using stuffer boxes
-
- D—TEXTILES; PAPER
- D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
- D01F—CHEMICAL FEATURES IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS; APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OF CARBON FILAMENTS
- D01F6/00—Monocomponent artificial filaments or the like of synthetic polymers; Manufacture thereof
- D01F6/02—Monocomponent artificial filaments or the like of synthetic polymers; Manufacture thereof from homopolymers obtained by reactions only involving carbon-to-carbon unsaturated bonds
- D01F6/04—Monocomponent artificial filaments or the like of synthetic polymers; Manufacture thereof from homopolymers obtained by reactions only involving carbon-to-carbon unsaturated bonds from polyolefins
- D01F6/06—Monocomponent artificial filaments or the like of synthetic polymers; Manufacture thereof from homopolymers obtained by reactions only involving carbon-to-carbon unsaturated bonds from polyolefins from polypropylene
-
- D—TEXTILES; PAPER
- D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B2401/00—Physical properties
- D10B2401/06—Load-responsive characteristics
- D10B2401/061—Load-responsive characteristics elastic
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- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Yarns And Mechanical Finishing Of Yarns Or Ropes (AREA)
- Artificial Filaments (AREA)
- Multicomponent Fibers (AREA)
Description
AUSTRALIA
Patents Act 607311 COMPLETE SPECIFICATION
(ORIGINAL)
Class Int. Class Application Number: Lodged: Complete Specification Lodged: Accepted: Published: .Priority This document contains the amendments made under S...'tion 49 and is correct for 0,r~ Related Art: APPLICANT'S REFERENCE: Case 32489 Name(s) of Applicant(s): Phillips Petroleum Company SAddress(es) of Applicant(s): Bartlesville, State of Oklahoma, UNITED STATES OF AMERICA.
Address for Service is: PHILLIPS ORMONDE FITZPATRICK Patent and Trade Mark Attorneys 367 Collins Street Melbourne 3000 AUSTRALIA Complete Specification for the invention entitled: RESILIENT POLYPROPYLENE FIBERS AND PREPARATION THEREOF j: Our Ref 123583 POF Code: 1422/50647 The following statement is a full description of this invention, including the best method of performing it known to applicant(s): 6003q/1 1
F,;
4 r* t L.
t If Ii I I II The invention relates to highly resilient polypropylene fibers which are particularly useful in carpeting and upholstering.
In another aspect, the invention pertains to a process for producing highly resilient polypropylene fibers.
Polypropylene is an ideal fiber to be used in carpeting and upholstering, limited only by its poor resiliency. Resiliency is a measure of the ability of a fiber to recover fully its original dimensions upon release of a stress which is compressing it. With polypropylene carpet, this poor resiliency is best demonstrated by the 10 "walking out" of a sculptured carpet in a highly trafficked area, or by the matting which occurs on the walked on areas of level pile carpets.
Upholstery containing polypropylene fibers will also exhibit this matting phenomenon.
Thus it is desirable to produce a polypropylene fiber having a sufficiently high resiliency to resist "walking out" when used in sculptured carpeting, or to resist matting when used in level pile carpeting and upholstering.
The resiliency of the fiber is determined by a compression recovery test, a non-ASTM test that determines the percent height recovery of a compressed wad of carded fiber in a specified time.
I
1 i"l -r t- Sooo o o o 9e 0 0 0 00 9 0 0 9 e 9 9 0 .9 99 In accordance with the present invention there is provided a highly resilient fiber of polypropylene, said fiber having a nea-helia Acrimp with an average crimp count in the range of about 4 to about 20 crimps per inch; and a compression recovery of at least 250%.
In accordance with the present invention there is also provided a method of making a highly resilient polypropylene fiber which comprises: imparting a ano hlie&alecrimp to a drawn polypropylene fiber; and heat setting the product of step at a temperature sufficient and a residence time sufficient to allow the crimp imparted during step to be permanently set into the fiber so that the fibers have a compression recovery of at least 250%. A 15 sharp edge angular or so-called two dimensional type crimp is usually imparted to the fibers. Optionally one cuts the filaments to staple, which may be done before or after heat treating.
Brief Description of the Drawings In the drawings, forming a part hereof: Figure 1 shows compression recovery data for various heat treating temperatures at a constant residence time of three minutes; and Figure 2 shows compression recovery data for various residence times for a constant heat treating temperature of 295°F.
Detailed Description of the Invention The polypropylene which is used in the present invention may be any essentially linear highly crystalline isotactic polypropylene which has a high molecular weight. Generally such polymers have a melting point of about 165 0 C (329 0 Such polymers are commercially available.
Although any method can be used in the manufacture, the polypropylene used in the present invention is generally prepared using a coordination polymerization method. This polymerization method uses a reduced transition metal catalyst, generally in the form of a slurry of a very
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iia 3 small solid particle in an iner-t medium. This method is well known in the art.
Various additives including such dye receptors as polyamines, polyvinyl pyridines, polyamides, organic pigments such as phthalocyanine etc., inorganic pigments such as cadmium salt series, carbon black etc., and stabilizers, plasticizers, flame retardants, etc., may be incorporated into the polypropylene to modify the properties thereof.
The conversion of the bulk polypropylene to fiber form is accomplished by any of the usual spinning methods. Since polypropylene can be melted under reasonable temperature conditions, the production of the fibers is preferably done by melt spinning as opposed to solution Sprocesses. The fibers are melt spun at a temperature in the range of a' 'about 420 0 F to about 640 0 F, with a temperature in the range of about ;,fg i 450 0 F to about 625°F preferred.
In the process of melt spinning, the polymer is heated in an extruder to the melting point and the molten polymer is pumped at a constant rate under high pressure through a spinnerette containing a number of holes. The liquid polymer streams emerge downward, or in other directions, from the face of the spinnerette usually into a cooling 20 stream of gas, generally air. The streams of molten polymer are solidified as a result of cooling to form filaments and are brought together and are wound up on bobbins. If desirable, the polymer melt in the extruder may be protected from oxygen by blanketing it with steam or an inert gas such as carbon dioxide, nitrogen etc.
The size of the filaments will be in the range of about 1 denier/filament to about 130 denier/filament, with a filament size in the range of about 1.8 denier/filament to about 18 denier/filament preferred.
After the fiber has been prepared, a drawing step is performed to orient the molecular structure of the fibers. The drawing step may be carried out in any convenient mannerusing techniques well known in the art such as the use of heated rolls, heated circulating gas oven, steam oven, radiant panel heater, a heated plate, heated liquids, or the like.
The methods are not critical but the temperature should be sufficient to impart crystallinity during drawing. Although any draw ratio
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itt eet i te 4 *i i Ce
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drawn length/undrawn length) can be employed, a draw ratio above about 3.0:1 is used, preferably 3.5:1 to 6:1.
The spinning and drawing steps are done in a manner to produce sufficient crystallinity so that the fibers can withstand the heat treating step. This requires avoiding excessive heat in spinning for a given polymer and providing sufficient heat in drawing.
The drawn fiber can have any tenacity, but will generally have a tenacity measured on single fibers in the range of about 3 grams/denier to about 4.5 grams/denier, with a tenacity in the range of about 10 grams/denier to about 4.4 grams/denier being preferred.
The fibers are then crimped. The type of crimp imparted to the fibers can be described as either a sharp edge angular or non-helical crimp. These are the so-called two- dimensional or sawtooth crimps. The preferred method of imparting such a crimp is a stuffer box assembly.
15 The fiber has an average crimp count in the range of about 4 crimps per inch to about 20 crimps per inch, with an average crimp count in the range of about 6 crimps per inch to about 15 crimps per inch being preferred, 6 to 10 being most preferred.
After a crimp is imposed in the fibers, they are taken from the texturing region and are heated in suitable means at a temperature sufficient and for a time sufficient to allow the crimp imparted in the fiber to be permanently set so that the fibers will have an improved compression recovery.
Generally the fiber is heat treated at a temperature sufficient and for a residence time sufficient to allow the crimp imparted during the crimping step to be permanently set into the fiber so that the fiber will have a compression recovery of at least about 250 percent, although a compression recovery of at least about 275 percent is preferred, and a compression recovery of at least 290 percent being most preferred.
The compression recovery of the fibers after the heat treating step will of course depend upon both the temperature at which it was treated, and the residence time for which the fibers was treated.
Generally the heat treating temperature will be in the range about 280 0 F to just below the softening point of the fibers. The softening point of the fibers is in the range of about 320 0 F to about ;i 'ioi 8~ le i i 6i 1 i; a i *909 0 04 9 99 0t a a 0r so* a 9 O00 0090 so 9909° 0( 99 99 9 99 0 0 99a #9 9 329 0 F. A preferred heat treating temperature is in the range of about 284°F to about 315 0 F, with the most preferred temperature being in the range of about 289 0 F to 311 0
F.
The residence time required to heat treat the fibers depends upon the type of heating device used and the openness of the fiber bundle. With good heat transfer such as with condensing steam or high velocity air, 5 seconds to 1 minute is sufficient, whereas with lower velocity air circulation where fiber is piddled on a conveyer belt, between 1 and 8 minutes could be required. Generally, about 5 seconds to 10 about 8 minutes, preferably 5 seconds to 3 minutes is used, most preferably 5 seconds to 1 minute. Once the fiber reaches the desired temperature, it takes very little time, less than 30 seconds, to obtain the desired resilience properties.
The steps of spinning, drawing, crimping and heat setting can be done as one continuous process if desired, or spinning can be done separately and the remaining steps done continuously, i.e. the steps can be intermittent or continuous or any combination thereof.
The following is a description of the method used to determine compression recovery of staple fibers.
1. Card the sample to thoroughly blend and open it.
2. Weigh three 1 gram samples to the nearest 0.1 gram.
3. Place a single 1 gram sample in a one-inch diameter cavity mold, compress to 10,000 psi, and hold for one minute.
4. Remove the sample from the mold and allow it to recover for 24 hours (if desired, other times or multiple times can be used).
Herein, unless noted, 24 hours is used.
Rest the one inch diameter, 5.5-gram foot of a displacement gauge on the top of the sample. This gauge, Federal Model C81S, is mounted on Custom Scientific apparatus Model CS 55 128.
6. Measure the height of the sample after 30 more seconds this is height B.
7. The height of the sample immediately after one minute's compression at 10,000 psi, height A, is difficult to measure accurately each time. To minimize such measurement error, a standard initial height 09 '9l 9 999 90 0 O 99 99 iB r: i; 6 has been measured as accurately as possible, and this height, 0.167 inches, is used for all samples.
8. Make 3 determinations per sample, and report the average of the three.
9. Calculation.
Percent Compression Recovery B-A x 100
A
Figure 1 shows the relationship between compression recovery as measured after both 24 hours and 60 seconds versus oven heat treating temperatures, at a constant residence time of 3 minutes. This figure clearly shows the sharp increase in the fiber resilience, as measured by O 0 compression recovery at heat treating temperatures above about 280°F.
o e Figure 2 shows the relationship between compression recovery as :o measured after 24 hours and after 60 seconds versus residence time, at a *0 0 15 constant oven heat treating temperature of 295 0 F. This figure clearly 00 0 0 S shows the sharp increase in the fiber resilience, as measured by compression recovery at residence times above about 30 seconds.
a o Example This example is provided to assist one skilled in the art to a 0 20 further understanding of the invention, without limiting the scope of the o invention. Particular reactants, components, ratios, conditions employed, are intended to be exemplary and not limitative of the 0:0" reasonable scpe of the invention herein described, of which these examples are a part of my overall disclosure.
25 The fibers of this example were extruded from crystalline 0 polypropylene pellets of eight melt index (Marlex® 9374 polypropylene 0* made by Phillips Petroleum Co.) containing heat and U.V. stabilizers and antioxidants and a combination of organic and inorganic pigments to produce colored fibers. This resin was melted and brought to 520 0 F in a conventional extruder, forced under pressure through spinnerettes with round holes, each hole 0.7 mm diameter, cooled with cross-flow quench air at 60 0 F, 90 feet per minute, and wound onto a tube at 510 meters per minute. Lubricant and antistat were applied during spinning.
Fiber was withdrawn from an array of these tubes to form a tow .35 which, after drawing at 4.8 draw ratio, was one million denier, and each 7 drawn filament was 18 denier. Conventional seven-roll draw stands were used, with rolls of the first and second stands heated to 250 0 F and the third stand not heated. The stand speeds were 31, 125, and 150 meters per minute. Additional fiber finish was applied after drawing. The tow was heated with steam before entering a conventional Fleissner stuffer-box crimper having 5-inch wide water-cooled rolls, where 6 to 8 crimps per inch were imparted.
In a separate step, the crimped tow was piddled (distributed) onto a moving perforated-metal conveyor belt through which heated air circulated in a Proctor and Schwartz oven. The air temperatures and residence times were those indicated in FIGURES 1 and 2. The heat treated tow was cut to make staple of about 3.25 inches with a conventional Lummus cutter.
*t I i. C I 4
Claims (16)
- 2. A fiber according to claim i, wherein said average crimp count is in the range of about 6 to about 10 crimps per inch.
- 3. A fiber according to claim 1 or 2, wherein said fiber has a tenacity in the range of about 3.5 grams/denier to about 4.4 grams/denier.
- 4. A fiber according to any one of the preceding claims, wherein said compression recovery is at least 275%. A fiber according to claim 4, wherein said compression om recovery is at least 290%.
- 6. A fiber according to any one of the preceding claims, Swherein there is a plurality of said fibers in the form of a S tow.
- 7. A method of making a highly resilient polypropylene 0 fiber which comprises: imparting a saw-tooth crimp to a drawn polypropylene fiber; and rrrr heat setting the product of step at a temperature S sufficient and a residence time sufficient to allow the crimp imparted during step to be permanently set into the fiber so that the fibers have a compression recovery of at least 250%.
- 8. A method according to claim 7, wherein the product of step is heat set at a temperature and for a period of 3) time sufficient to allow the crimp imparted in step to be permanently set into the fiber so that the fiber has a compression recovery of at least 275%.
- 9. A method according to claim 8, wherein the fibers have a compression recovery of at least 290%. A method accorCing to any one of claims 7 to 9, wherein the temperature at which the product from step is heat set is in the range of about 280°F to just below the softening point of the fibers, and the residence time is -8- U: CB u seconds to 8 minutes.
- 11. A method according to claim 10, wherein the temperature at which the product from step is heat set is in the range of about 284 F to about 315 and the residence time is about 5 seconds to 3 minutes.
- 12. A method according to claim 11, wherein the temperature at which the product from step is heat set is in the 0 0 range of about 289°F to about 311F, and the residence time is about 5 seconds to 3 minutes.
- 13. A method according to any one of claims 7 to 12, wherein said heat setting is brought about by contact with steam, the temperature is in the range of about 289°F to about 311°F and said residence time is within the range of seconds to 1 minute,
- 14. A method according to any one of claims 7 to 13, wherein said heat setting is brought about by high velocity circulation of hot air through the fibers, said residence time is 5 seconds to 1 minute and the resulting temperature is in the range of about 289°F to 3110F.
- 15. A method according to any of claims 7 to 14, wherein after or before said step said fiber is cut into staple.
- 16. A method according to any one of claims 7 to wherein a tow of the fibers is crimped and heat set.
- 17. A highly resilient fiber substantially as herein described with the Example.
- 18. A method of making a highly resilient polypropylene fiber substantially as herein described with the Example.
- 19. A carpet made with fibers according to any one of the preceding claims. 3 0 DATED: 21 NOVEMBER, 1990 PHILLIPS ORMONDE FITZPATRICK Attorneys For: PHILLIPS PETROLEUM COMPANY 2778Z
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US16023288A | 1988-02-25 | 1988-02-25 | |
US160232 | 1993-11-30 |
Publications (2)
Publication Number | Publication Date |
---|---|
AU3078189A AU3078189A (en) | 1989-08-31 |
AU607311B2 true AU607311B2 (en) | 1991-02-28 |
Family
ID=22576062
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AU30781/89A Ceased AU607311B2 (en) | 1988-02-25 | 1989-02-27 | Resilient polypropylene fibers and preparation thereof |
Country Status (12)
Country | Link |
---|---|
EP (1) | EP0330212A3 (en) |
JP (1) | JPH01298231A (en) |
KR (1) | KR890013232A (en) |
CN (1) | CN1036052A (en) |
AU (1) | AU607311B2 (en) |
BR (1) | BR8900872A (en) |
DK (1) | DK89589A (en) |
FI (1) | FI890896A (en) |
NO (1) | NO890769L (en) |
PT (1) | PT89787A (en) |
YU (2) | YU40289A (en) |
ZA (1) | ZA891115B (en) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6716511B2 (en) | 1996-09-16 | 2004-04-06 | Bp Corporation North America Inc. | Propylene polymer fibers and yarns |
US5945215A (en) * | 1996-09-16 | 1999-08-31 | Bp Amoco Corporation | Propylene polymer fibers and yarns |
JP5497987B2 (en) * | 2007-06-22 | 2014-05-21 | ユニ・チャーム株式会社 | Nonwoven fabric and method for producing the same |
WO2015192007A1 (en) * | 2014-06-13 | 2015-12-17 | Invista North America S.A.R.L. | Mechanically crimped fiber tow having increased bulk and crimp take-up |
WO2016073713A1 (en) | 2014-11-06 | 2016-05-12 | The Procter & Gamble Company | Crimped fiber spunbond nonwoven webs / laminates |
EP3215095A1 (en) | 2014-11-06 | 2017-09-13 | The Procter and Gamble Company | Zonal patterned apertured webs, laminates, and methods for making the same |
EP4335420A3 (en) | 2017-02-16 | 2024-05-29 | The Procter & Gamble Company | Absorbent articles with substrates having repeating patterns of apertures comprising a plurality of repeat units |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3152380A (en) * | 1961-05-05 | 1964-10-13 | Du Pont | Process for treating polypropylene fibers |
US3461521A (en) * | 1967-11-24 | 1969-08-19 | American Enka Corp | Process for manufacture of yarns |
US3587145A (en) * | 1969-06-19 | 1971-06-28 | Bancroft & Sons Co J | Crimping apparatus with heating and cooling cage |
US4221838A (en) * | 1972-12-29 | 1980-09-09 | Phillips Petroleum Company | Crimped thermoplastic fibers |
-
1989
- 1989-02-13 ZA ZA891115A patent/ZA891115B/en unknown
- 1989-02-22 PT PT89787A patent/PT89787A/en unknown
- 1989-02-23 JP JP1044999A patent/JPH01298231A/en active Pending
- 1989-02-23 YU YU00402/89A patent/YU40289A/en unknown
- 1989-02-23 EP EP19890103218 patent/EP0330212A3/en not_active Withdrawn
- 1989-02-23 NO NO89890769A patent/NO890769L/en unknown
- 1989-02-23 KR KR1019890002307A patent/KR890013232A/en not_active Application Discontinuation
- 1989-02-24 FI FI890896A patent/FI890896A/en not_active Application Discontinuation
- 1989-02-24 BR BR898900872A patent/BR8900872A/en unknown
- 1989-02-24 DK DK089589A patent/DK89589A/en not_active Application Discontinuation
- 1989-02-25 CN CN89101153A patent/CN1036052A/en active Pending
- 1989-02-27 AU AU30781/89A patent/AU607311B2/en not_active Ceased
-
1990
- 1990-05-07 YU YU88790A patent/YU88790A/en unknown
Also Published As
Publication number | Publication date |
---|---|
YU40289A (en) | 1990-10-31 |
EP0330212A3 (en) | 1990-09-19 |
ZA891115B (en) | 1989-10-25 |
AU3078189A (en) | 1989-08-31 |
YU88790A (en) | 1994-01-20 |
PT89787A (en) | 1989-10-04 |
NO890769D0 (en) | 1989-02-23 |
BR8900872A (en) | 1989-10-17 |
NO890769L (en) | 1989-08-28 |
DK89589A (en) | 1989-08-26 |
JPH01298231A (en) | 1989-12-01 |
DK89589D0 (en) | 1989-02-24 |
FI890896A0 (en) | 1989-02-24 |
FI890896A (en) | 1989-08-26 |
CN1036052A (en) | 1989-10-04 |
KR890013232A (en) | 1989-09-22 |
EP0330212A2 (en) | 1989-08-30 |
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