US3167847A - Treatment of multi-filament yarn - Google Patents
Treatment of multi-filament yarn Download PDFInfo
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- US3167847A US3167847A US238506A US23850662A US3167847A US 3167847 A US3167847 A US 3167847A US 238506 A US238506 A US 238506A US 23850662 A US23850662 A US 23850662A US 3167847 A US3167847 A US 3167847A
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- D—TEXTILES; PAPER
- D02—YARNS; MECHANICAL FINISHING OF YARNS OR ROPES; WARPING OR BEAMING
- D02J—FINISHING OR DRESSING OF FILAMENTS, YARNS, THREADS, CORDS, ROPES OR THE LIKE
- D02J1/00—Modifying 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
- D02J1/08—Interlacing constituent filaments without breakage thereof, e.g. by use of turbulent air streams
Definitions
- the present invention relates to the treatment of yarn and more particularly to subjecting substantially untwisted thermoplastic synthetic high polymer multi-filament yarn to the action of a gas passing across or through the yarn in the form of a jet stream.
- the invention is also directed to an improved apparatus for carrying out the foregoing method.
- thermoplastic yarns having substantially no twist are difficult to handle in textile processes such as weaving and knitting because the parallel filaments are only loosely associated and therefore incur problems in the said handling operation.
- the twisting operation is time consuming and therefore a costly operation, and, from the standpoint of economy, it is highly desirable to eliminate the twisting step, if the filaments can be made to cohere by other methods.
- Still another method of treating filamentary yarn with ice gases is disclosed in US. Patent No. 2,985,995.
- the patentees preferably utilize several air jets of complicated construction in which the gas is directed onto the thread and impinged on a solid fiat surface.
- Such a system is conducive to interlacing to a lesser extent and the method causes adverse optical effects in the yarn which is objectionable in a woven fabric.
- the patent describes in detail the various factors necessary to produce interlaced yarn, but there is no systematic method in which the optimum interlacing action is determined and effected, nor is there any disclosure to correlate the air pressure and the tension in the yarn in order to effect optimum results.
- the intensity of the sound which is measured in decibels is a critical factor to effect optimum intertwining of the filaments.
- the air pressure is chosen which gives the highest number of decibels that can be borne by the human ear for an optimum degree of intertwining.
- the degree of intertwining varies inversely with the tension for any given air pressure. Therefore, at very low tension, for example, below 0.05 gram per denier, loops will form around the surface of the yarn and make the Taslan type of yarn.
- tensions cannot be permitted above 0.3 gram per denier because, then in attempting to obtain a sufficient intertwining of the filaments, the air pressure must be increased to a point where the yarn will be damaged.
- thermoplastic yarn composed of a multiplicity of filaments which have been treated with a gas to provide the optimum degree of intertwining or coherency effect.
- Another object of the present invention is to provide a simple yarn intertwining assembly which may be easily adjusted for varying yarn conditions and the efliciency of which is directly proportional to the loudness of sound produced.
- a still further object of this invention is to provide a resonance or cushioning chamber for receiving a stream of gas after passage of the same through a bundle of filaments and for absorbing the initial surge of said gas to prevent disorderly secondary gas currents from interfering with yarn entanglement by the gas jets.
- FIGURE 1 represents in perspective a preferred embodiment of the apparatus: of this invention with the vided for supporting and maintaining in proper position a jet assembly 11 and a cylindrical plug 12.
- the jet assembly 11, including gas supply tube 13, is removable and adjustably clamped within housing 10 by any suitable means such as set screw 14.
- cylindrical plug 12 is also adjustably positioned by set screw 15.
- housing 10 is provided with a hollow opening 16 to provide an area or zone for receiving the discharge end of jet assembly 11 and the free end of cylindrical plug 12.
- Thread guides 17, 17 are secured to housing 10 by any suitable means and extend diametrically across hollow opening 16. Although these thread guides may be of conventional V-slot construction, it is important that the slots in each be sufficiently small to prevent lateral vibration of yarn 18 passing therethrough. Moreover, as willbe seen from FIG- URE 2, thread guides 17, 17 should be adjusted to provide precise alignment between yarn 18 and jet orifice or nozzle 20 formed in the terminal end of the jet assembly.
- a resonance or cushioning chamber '21 is formed in thejfree end of cylindrical plug 12.
- a reduced entrance passageway 22 provides access between chamber 21 and the atmosphere within the area defined by hollow opening 16.
- chamber 21 is shown as being cylindrical although other shapes could be utilized if with its corresponding thread guides 17, 17 as shown in FIGURE 2 to position yarn 18 precisely within the thread guide slots in order to'insure alignment with jet orifice 20 without imparting excesstension.
- Thread guides 17, 17 and dampening members 24, 24 additionally define, within hollow opening 16, the operating portion of yarn The'intertwining effect produced by gas discharging under pressure from'orifice 20 will occur only in that unsupported portion of yarn extending between cooperating thread guides and dampening mernbers.
- Coverplate 23 also serves to support sound insulating or absorbing material 25. As shown in FIGURE 1, a blanket of material 25 overlies the entire exposed surface of housing 10 and also surrounds the operating zone defined within hollow opening 16. As will be seen presently, the
- the sound insulating or inhibiting material 25' which may be formed from foam rubber, felt, or porous plastics an indispensable element for preferred operation of this invention.
- the diameter b of entrance passageway 22 should lie in the range between 1.0 and 1.8 times the exit diameter a of jet orifice 20. With a jet orifice diameter a of unity measured in millimeters, therefore, the entrance b should lie between 1.0 and 1.8 millimeters in diameter.
- the spacing 0 between the exit or orifice 20 and the beginning or entrance 22 does not depend entirely upon the size of either of these elements, it has been found that the same should lie between 1 and 3 mm. for optimum results.
- the distance d between thread guides 17, 17 should lie in the range between 20 and 55 mm., depending on denier, filament count, and pressure, to be discussed infra.
- the surface area of the jet orifice exit is adapted to the denier of yarn tobe treated. Larger denier yarns of as possible to conserve on'the consumption of gas. It has been found that jet orifices having surface areas lying between 0.2 mm. and 5.0 mm?v operate very effectively.
- the orifice 20 may be cylindrical or tapered in either direction, provided the exit area lies within the range speci-' fied, and the attitude of the jet orifice relative to the yarn axis may be oblique or normal, although'the normal is preferred.
- the yarns supplied must be thermoplastic and therefore of a synthetic high polymer type such as polyamides, polyesters, polyalkylenes, polyacrylonitriles, polyurethanes, etc.
- the cross section of the filaments may be circular, multi-lobal, triangular, etc.
- this system operates satisfactorily on yarns ranging in denier from to 2000 or above, and satisfactory results have been found to obtain at yarn speeds from 150 meters to 500 meters per minute.
- gas mediums such as carbon dioxide, nitrogen, unsaturated or saturated steam, and air. For purposes of economy, air is preferred.
- the needle should be inserted centrally of the filament 2 cm. per second.
- Toobtain the coherency factor index a yarn or thread at least 60 centimeters in length is clamped and suspended alongside a vertical'scale graduated in centimetersj
- a steel needle meas- sage of this gas through the traveling yarn bundle.
- the hook drop determination mentioned above should be repeated at least 10 times with additional yarn samples, after which an average hook drop distance x is calculated.
- the coherency factorused herein may be defined as It has been found that a coherency factor of at least 1.5, preferably higher, is required for use of multi-filament untwisted yarn on textilemachines, for example, weav-.
- the resonance chamber described herein and considered to be a critical feature of the present invention collects gas emerging throughfthejet orifice after pas- Inexits, the same operates asa cushion and also provides a back pressure vibrating at a resonant frequency. to assist in intermingling of filaments within the yarn bundle.
- a method of intertwining a substantially untwisted thermoplastic synthetic high polymer multi-filament yarn which comprises drawing said yarn under a low tension along a rectilinear path in which the yarn at the points of entering and leaving the path is held against substantial lateral vibration, directing a jet of gas across the yarn path and into a confined resonance zone under a pressure of 3 to 5 atmospheres to create a loudness which could not normally be borne by the human ear and inhibiting the noise in the resonance zone to thereby permit such pressure, and correlating the pressure with the tension on the yarn.
- a method of intertwining a substantially untwisted thermoplastic synthetic high polymer multi-filarnent yarn which comprises drawing said yarn under a low tension along a rectilinear path in which the yarn at the points of entering and leaving the path is held against substantial lateral vibration, directing a jet of gas across the yarn path and into a confined resonance zone under sufficient pressure to create a maximum loudness which could not normally be borne by the human ear and inhibiting the noise in the resonance zone to thereby permit 10 such pressure, and correlating the pressure with the ten sion on the yarn to obtain a yarn coherency factor of at least 1.5.
- An apparatus for intertwining a substantially untwisted thermoplastic synthetic high polymer multifilament yarn which comprises a nozzle having a fine orifice for supplying gas under pressure, a cylindrical resonance chamber having an opening disposed opposite the nozzle orifice at a distance from 1 to 3 mm., said opening having a diameter between 1.0 and 1.8 times the exit diameter of said orifice sound damping means surrounding said chamber, yarn guides located above and below the nozzle and chamber to position the yarn between the nozzle and the opening to the chamber, said guides embodying means to dampen the vibration of the yarn passing therebetween and to localize the nodes at those points, said guides being spaced from 20-55 mm. apart.
Description
Feb. 2, 1965 c.-.|. GONSA LVES 3, 7,
v TREATMENT OF MULTI-FILAMENT YARN Filed Nov. 19, 1962 2 Sheets-Sheet l INVENTOR. CONRAD JOSEPH GONSALVES BY a; aw
ATTORNEY Feb. 2, 1965 c. J. GONSALVES 3,167,847
TREATMENT OF MULTI-FILAMENT YARN Filed NOV. 19, 1962 2 Sheets-Sheet? VENTOR. CONRAD J08 GONSALVES ATTORNEY United States Patent 3,167,847 TREATMENT OF MULTI-FILAMENT YARN Conrad J. Gonsalves, Arnhem, Netherlands, assignor to American Erika Corporation, Enlca, N.C., a corporation of Delaware Filed Nov. 19, 1962, Ser. No. 238,506 Claims priority, application Netherlands, Nov. 28, 1961, 271,935 4 Claims. (Cl. 28-1) The present invention relates to the treatment of yarn and more particularly to subjecting substantially untwisted thermoplastic synthetic high polymer multi-filament yarn to the action of a gas passing across or through the yarn in the form of a jet stream. The invention is also directed to an improved apparatus for carrying out the foregoing method.
In the textile trade, it is a well known fact that thermoplastic yarns having substantially no twist are difficult to handle in textile processes such as weaving and knitting because the parallel filaments are only loosely associated and therefore incur problems in the said handling operation. In order to overcome this problem, it is normally necessary to provide a twisting step and, if required, the twisted threads are also given a sizing operation which imparts better coherence between the filaments of the yarn. However, the twisting operation is time consuming and therefore a costly operation, and, from the standpoint of economy, it is highly desirable to eliminate the twisting step, if the filaments can be made to cohere by other methods.
In recent years in the textile field, various methods and apparatus have been developed for modifying the characteristics of yarns consisting of a multiplicity of filaments by passing the yarn through a zone in which gas such as air and the like is introduced under pressure to effect a turbulence in the zone and thereby cause the individual filaments to form loops, convolutions, and the like and, upon withdrawing the yarn from the turbulent zone under a reduced tension, collect the same either with or without twisting depending upon whether the yarn was twisted prior to entry into the zone. Such yarn is characterized by a multiplicity of crunodal loops particularly along the outer surface of the yarn bundle and is known in the trade as Taslan. The basic patent covering this type of yarn is US. Patent No. 2,783,609.
Another air jet treatment of regenerated cellulose yarn is covered in Canadian Patent No. 554,150 and the object of that process is to produce a tousled yarn. It is stated therein that the thread undergoes an increase in denier and decrease in length during the treatment which in effect is making a more voluminous yarn by the said treatment. The patentee describes a treatment in which the rate of withdrawing yarn from the treatment zone is from 4% to less than the rate of feed. In the case of regenerated cellulose yarn, it has been determined that it is impossible to provide that degree of overfeed because slack will occur in the yarn which will cause it to wrap around the feed roller. This is due to the inelasticity of regenerated cellulose yarn. There would be an absence of tension on the yarn and the only way to induce tension would be to maintain the withdrawal speed at least equal to the input speed. This, however, is not contemplated by the patent.
Still another method of treating filamentary yarn with ice gases is disclosed in US. Patent No. 2,985,995. However, in this case, the patentees preferably utilize several air jets of complicated construction in which the gas is directed onto the thread and impinged on a solid fiat surface. Such a system is conducive to interlacing to a lesser extent and the method causes adverse optical effects in the yarn which is objectionable in a woven fabric. The patent describes in detail the various factors necessary to produce interlaced yarn, but there is no systematic method in which the optimum interlacing action is determined and effected, nor is there any disclosure to correlate the air pressure and the tension in the yarn in order to effect optimum results.
It has now been unexpectedly determined that in addition to the two basic controling factors, which are yarn tension and air pressure, in order to obtain the desired degree of intertwining of filaments, the intensity of the sound which is measured in decibels is a critical factor to effect optimum intertwining of the filaments. In other words, for a given tension, the air pressure is chosen which gives the highest number of decibels that can be borne by the human ear for an optimum degree of intertwining. The degree of intertwining varies inversely with the tension for any given air pressure. Therefore, at very low tension, for example, below 0.05 gram per denier, loops will form around the surface of the yarn and make the Taslan type of yarn. On the other hand, tensions cannot be permitted above 0.3 gram per denier because, then in attempting to obtain a sufficient intertwining of the filaments, the air pressure must be increased to a point where the yarn will be damaged.
It is therefore an object of the present invention to provide a thermoplastic yarn composed of a multiplicity of filaments which have been treated with a gas to provide the optimum degree of intertwining or coherency effect.
It is a further object of this invention to utilize a method in which tension on the yarn and the air pressure are correlated to effect a maximum degree of sound or loudness as measured in decibels.
Another object of the present invention is to provide a simple yarn intertwining assembly which may be easily adjusted for varying yarn conditions and the efliciency of which is directly proportional to the loudness of sound produced.
A still further object of this invention is to provide a resonance or cushioning chamber for receiving a stream of gas after passage of the same through a bundle of filaments and for absorbing the initial surge of said gas to prevent disorderly secondary gas currents from interfering with yarn entanglement by the gas jets.
These objects may be accomplished, in accordance with the present invention, by providing an intertwining method based upon an air pressure system using a resonance chamber constructed in different dimensions from which one dimension specifically will give the optimum intertwining effect while, with the change of the dimensions of the resonance chamber in cooperation with a range of air pressure, overfeed and tension will cover a broad spectrum of intertwining effects sufficient for a filament cohesion ranging from twist imitating draw twist up to a twist avoiding twist slashing.
The foregoing, as well as other objects and advantages of the present invention, will become apparent to those skilled in this art upon study of the following description taken in conjunction with the accompanying drawings, wherein undergoing treatment.
FIGURE 1 represents in perspective a preferred embodiment of the apparatus: of this invention with the vided for supporting and maintaining in proper position a jet assembly 11 and a cylindrical plug 12. The jet assembly 11, including gas supply tube 13, is removable and adjustably clamped within housing 10 by any suitable means such as set screw 14. Likewise, cylindrical plug 12 is also adjustably positioned by set screw 15.
As will be seen from the drawing, housing 10 is provided with a hollow opening 16 to provide an area or zone for receiving the discharge end of jet assembly 11 and the free end of cylindrical plug 12. Thread guides 17, 17 are secured to housing 10 by any suitable means and extend diametrically across hollow opening 16. Although these thread guides may be of conventional V-slot construction, it is important that the slots in each be sufficiently small to prevent lateral vibration of yarn 18 passing therethrough. Moreover, as willbe seen from FIG- URE 2, thread guides 17, 17 should be adjusted to provide precise alignment between yarn 18 and jet orifice or nozzle 20 formed in the terminal end of the jet assembly.
In order to produce the desired effect on yarn processed by the present invention, a resonance or cushioning chamber '21 is formed in thejfree end of cylindrical plug 12.
A reduced entrance passageway 22 provides access between chamber 21 and the atmosphere within the area defined by hollow opening 16. Although the exact shape of .resonance chamber 21 is not critical, the capacity or volume of the same is very important as will be discussed infra. Accordingly, chamber 21 is shown as being cylindrical although other shapes could be utilized if with its corresponding thread guides 17, 17 as shown in FIGURE 2 to position yarn 18 precisely within the thread guide slots in order to'insure alignment with jet orifice 20 without imparting excesstension. Thread guides 17, 17 and dampening members 24, 24 additionally define, within hollow opening 16, the operating portion of yarn The'intertwining effect produced by gas discharging under pressure from'orifice 20 will occur only in that unsupported portion of yarn extending between cooperating thread guides and dampening mernbers.
operating elficiency or effectiveness of the present inven- 7 tion increases directly in proportion to noise produced byv gas discharging through orifice '20 and resonating within" such as relatively stiff polyurethane foam, is considered Accord, ingly, the sound insulating or inhibiting material 25', which may be formed from foam rubber, felt, or porous plastics an indispensable element for preferred operation of this invention.
Attention is now directed to FIGURE3 which indicates more clearly the relative size and disposition of parts found to be necessary for satisfactory operation of this invention. The diameter b of entrance passageway 22 should lie in the range between 1.0 and 1.8 times the exit diameter a of jet orifice 20. With a jet orifice diameter a of unity measured in millimeters, therefore, the entrance b should lie between 1.0 and 1.8 millimeters in diameter. Although the spacing 0 between the exit or orifice 20 and the beginning or entrance 22 does not depend entirely upon the size of either of these elements, it has been found that the same should lie between 1 and 3 mm. for optimum results. Moreover, the distance d between thread guides 17, 17 should lie in the range between 20 and 55 mm., depending on denier, filament count, and pressure, to be discussed infra.
As indicated earlier, it has unexpectedly been found that optimum results are obtained only when a definite relationship is establishedand maintained between the volume or capacity of resonance chamber '21 and the pressure of gas supplied through orifice 20. When using compressed air, for example, preferred results are obtained when the capacity of chamber 21 lies between (44p+229) mm. and (-78p+402) mm. where p is the gauge pressure of the compressed air in atmospheres.
Furthermore, the distance'between thread guides 17, 17
must be adapted to the, pressure of gas utilized. For example, it has been found thatwhen using compressed air at a gauge pressure of 4-atmospheres for treating polyamide yarn having a denier of 70 and consisting of 24 filaments, the yarn'tension should be maintained between 4 and 12 grams and the. distance between thread guides 17, 17 must be between 20 and 40 mm., preferably between 30 andmm., in order to obtain satisfactory intertwining. Should the gas pressure be increased to 5 atmospheres, then the distance between thread guides should also be increased to between 30 and 55 mm., preferably between and mm., within a tension range of 5 to 14 grams. 7 As previously mentioned, practiceof the present invention requires maintenance of yarn tension between about 0.05 grams per denier and about 0.3 grams per denier. At a lower tension, the filaments will be interlaced as be fore but crunodal loops will occur on the surface of the filament bundles. Use of tensions higher than 0.3 grams per denier would necessitate an increase in air pressure to such'extent that filaments will be completely disrupted in an uncontrollable manner and in some instances broken. The surface area of the jet orifice exitis adapted to the denier of yarn tobe treated. Larger denier yarns of as possible to conserve on'the consumption of gas. It has been found that jet orifices having surface areas lying between 0.2 mm. and 5.0 mm?v operate very effectively. The orifice 20 may be cylindrical or tapered in either direction, provided the exit area lies within the range speci-' fied, and the attitude of the jet orifice relative to the yarn axis may be oblique or normal, although'the normal is preferred.
Artificial multi-filament yarn to be treated by this invention should have little or no twist. If the yarn supplied to this tangling assembly contains a twist signifia cantly higher than about 40 turns per meter, it has been.
found that the filaments do not separate satisfactorily and consequently are, not intertwined. As indicated earlier, however, weaving yarns of the type primarily under consideration do not contain large. amounts of twist and therefore the problem of over-twisted yarn normally would not occur. 7
For effective intertwining, the yarns supplied must be thermoplastic and therefore of a synthetic high polymer type such as polyamides, polyesters, polyalkylenes, polyacrylonitriles, polyurethanes, etc. The cross section of the filaments may be circular, multi-lobal, triangular, etc. Moreover, it has been found that this system operates satisfactorily on yarns ranging in denier from to 2000 or above, and satisfactory results have been found to obtain at yarn speeds from 150 meters to 500 meters per minute. It is believed that the apparatus disclosed herein may be used equally effectively with various types of gas mediums such as carbon dioxide, nitrogen, unsaturated or saturated steam, and air. For purposes of economy, air is preferred. Generally speaking, however, use of steam necessitates less pressure than use of air. It should be pointed out in this connection that use of any gaseous medium which might impart shrinkage to the yarn treated, for example, steam or heated air, must be compensated for by a slight overfeed of yarn into the system. Only that amount of overfeed necessary to compensate for shrinkage should be provided, however, since any excess amount results in formation of surface loops explained earlier. Moreover, it is essential to satisfactory operation that the thread be maintained under a low tension during treatment whether or not overfeed occurs. Finally, any tendency toward development of electrostatic charges which arises may be obviated through use of conventional procedures such as by Wetting the thread with either water or a sizing agent or both.
The use of sound insulation or absorbing material 25 has been found to be an essential ingredient of the present invention, not because of the direct participation thereof in the intertwining of filaments, but because of the unbearable sound inherently produced at air pressures necessary for providing the desired results. Although precise sound measurements are difficult to achieve, and the maximum bearable loudness depends upon the opera- 1 operation and results obtained.
tor, experiments have shown, and this is believed to be unexpected, that optimum results cannot be obtained at low noise levels. Conversely, it has been found that best results are obtained by tuning the device, through use of any conventional air pressure adjustment, to provide maximum sound. The tangling assemblies are calibrated, so to speak, by relying upon the sound produced, and any system for alleviating the loud noise involved permits use of higher gas pressure and thereby improves the overall It has been found that a noise level of 124 decibels, for example, can be effectively reduced through use of sound insulation such as that shown herein to a level of 80 decibels without impairing eificiency of the entangling assembly. Conse- 15 quently, the assembly may be tuned, so to speak, for
maximum efiiciency at a more satisfactory sound level of operation.
EXAMPLE A number of experiments were conducted with an apparatus substantially similar to that shown and described herein. A nylon 6 type yarn having a denier of 70 and filament count of 24 was fed through the assembly and treated with compressed air while maintaining a tension of about 6 grams. The feed rate and draW-oif rate were maintained at about 150 meters perminute (no overfeed), although the rate could have been adjusted up to about 500 meters per minute or higher. During these experiments, the results of which appear hereinbelow in table form, the distance 0 between the nozzle exit and varied. These variations appear in the table and are recorded under various runs.
Distance Distance Nylon 6 Dia. exit nozzle between Dia. inlet Capacity Dia. Depth Gauge Tension Run thread 70 nozzle exit to inlet thread resonance resonance resonance resonance pressure of in the coherency den/24 fil. in mm. (a) resonance guides in chamber chamber chamber chamber air in atm. thread factor chamber mm. (d) in mm. (b) in mm. in mm. in mm. in grams in mm. (c)
1 Nylon 6 1. 2 0.5 32 1. 4 50 8 1 4 6 1. 2
thread 70 den./ 24 ill. 2 do 12 1 32 1.4 50 8 1 4 6 7.3 1. 2 2 32 1. 4 50 8 1 4 6 74. 5 1. 2 3 32 1. 4 50 8 1 4 6 6. 6 l. 2 4 32 1. 4 50 8 1 4 6 1. 1 1. 2 2 10 1. 4 50 8 1 4 6 1. 1 1. 2 2 20 1. 4 50 8 1 4 G 17.1 1. 2 2 30 1. 4 50 8 1 4 6 73. 2 1. 2 2 35 1. 4 50 8 1 4 6 76. 8 1. 2 2 1. 4 8 1 4 6 40. 1 1. 2 2 50 1. 4 50 8 1 4 6 1. 4 1. 2 2 2O 1. 4 10 8 O. 2 5 6 1. 2 1. 2 2 30 1. 4 1O 8 0.2 5 6 20. 2 1. 2 2 40 1. 4 10 8 0. 2 5 6 75. 8 1.2 2 1.4 10 8 0.2 5 6 81.3 1. 2 2 1. 4 10 8 0.2 5 6 1. 5 1. 2 2 30 1. 1 50 8 1 4 6 1. 2 1. 2 2 30 1. 2 50 8 1 4 6 50. 4 1. 2 2 30 2.0 50 8 l 4 6 60.3 1. 2 2 30 3.0 50 8 1 4 6 1.0 1. 2 2 30 1. 4 30 8 0.6 4 6 0.9 1. 2 2 3O 1. 4 53 8 1 4 6 72. 8 1. 2 2 30 1. 4 8 1. 5 4 6 81. 4 1.2 2 30 1.4 8 1.8 4 6 73.2 1. 2 2 3O 1. 4 8 2.0 4 6 1. 4 1.2 2 30 1.4 65 8 1.3 4 6 76.4 1. 2 2 30 1. 4 65 5 2. 3 4 6 69. 5 1. 2 2 30 1.4 65 2 20. 7 4 6 56. 5 1. 2 2 32 1. 4 82 8 1.6 3. 33 6 24. 2 1. 2 2 32 1. 4 143 8 2. 9 3.33 6 26. 3 1. 2 2 32 1. 4 68 8 1. 4 3. 66 6 61. 4 1. 2 2 32 1.4 117 8 3. 3 3. 66 6 64. 2 1. 2 2 32 1. 4 53 8 1.1 4 6 76. 4 1.2 2 32 1.4 90 8 1.8 4 6 75.8 1. 2 2 32 1.4 39 8 0.8 4. 33 6 81. 6 1.2 2 32 1.4 64 8 1.3 4.33 6 80.4 1. 2 2 32 1. 4 29 8 0.6 4. 66 6 93. 7 1. 2 2 3 1. 4 39 8 0.8 4. 66 6 94. 8 1. 2 2 32 1. 4 50 8 1 4 3. 5 75.4 1. 2 2 32 1. 4 50 8 1 4 6 73. 2 1. 2 2 32 1. 4 50 8 1 4 9 62. 8 1. 2 2 32 1. 4 50 8 1 4 12 41. 4 1. 2 2 32 1. 4 50 8 1 4 14 20.8
. mospheres pressure.
sive, were made at a constant gauge. pressure of 4 atmospheres, and runs 12 to 16, inclusive, were made at 5 atwas maintained at 6 grams. As the table will indicate, variation in thread guide spacing d above 40 mm. or below mm. at 4 atmospheres pressure produces unfavorable results, with the most desired characteristics being obtained at the to mm. spacings of runs 8 and 9. Likewise,.most favorable results were obtained during the 5 atmosphere runs at a higher spacing at of 30 to 55 mm., and particularly about or mm. Runs 17 to 20 were made while maintaining constant allfeatures of the assembly except diameter b of the entrance passageway 22 leading into resonance chamber 21. Very poor results were obtained in run 17 with diameter 12 smaller than the dimensions of a of the jet orifice exit. Similarly, with diameter b at about 2.5 times the dimension a, the results are poor. Preferred results shown at runs 18 and 19 occur when the opening or entrancepassageway 22 is only slightly larger or equal to the dimens1on a.
The depth of resonance chamber 21 and likewise the volume or capacity thereof was changed in varying degree during runs 21 to 25. It will be seen that satisfactory, results were obtained only at capacities ranging in the neighborhood of from 53 to 90 cubic millimeters at uring 0.4 in thickness and bent through an angle of 120 into hookshape is inserted into the bundle of file-- ments at a point immediately below the suspension clamp.
The needle should be inserted centrally of the filament 2 cm. per second.
' tualiy a point will be reached where the filaments are In each of these runs, the tension the 4 atmospheres gauge pressure and 6 grams tension shown. In runs 26 to 28 the: capacity of chamber 21 was maintained constant at cubic miilimeters while varychamber were varied. It will be seen that better entangle.
ment results from increase in gauge pressure throughout the range used. It also appears that capacity of the resonance chambercan be varied satisfactorily onlywithin relatively narrow limits. For example, at capacities of 82 to 143 cubic millimeters, the entanglement dropped ofi considerably below the desired level obtained at lower chamber capacities.
In the remaining runs 39 through 43, all critical features of this invention were maintained constant except yarn tension, which was varied from 3.5 to 14 grams. It willbe eminently obvious that the desired entanglement varied inversely withtension. In other words, increased yarn tension produces a lower entanglement evidenced by a reduced coherency factor.-
To permit duplication of the experiments recorded herein by those skilled in this art, it is deemed advisable to. explain in some detail the manner in which the filament intertwining, referred to in the table as coherency A factor, was determined. The method to be described admittedly represents an arbitrary standard or index, but
'one which clearly records improvements of one run rela-:
tive to other runs.
Toobtain the coherency factor index, a yarn or thread at least 60 centimeters in length is clamped and suspended alongside a vertical'scale graduated in centimetersj A clip having a weight numerically equal to 0.2 times: the yarn denier, but not greater than 100 grams for yarn above SOD-denier, isattached to the free lower end of yarn suspended from the clamp. A steel needle meas- ,sage of this gas through the traveling yarn bundle.
asmuch as the chamber has been provided with nogas heavily intertwined or entangled. Needle lowering should be interrupted at a point where further movement obviously would result in filament breakage. Hook drop distances are read at this point with all distances of more than 50 cm. beingrecorded as cm. To compensate for inaccurate needle insertion, it has been found that 0.5 cm. should be subtracted from the distance recorded.
The hook drop determination mentioned above should be repeated at least 10 times with additional yarn samples, after which an average hook drop distance x is calculated. The coherency factorused herein may be defined as It has been found that a coherency factor of at least 1.5, preferably higher, is required for use of multi-filament untwisted yarn on textilemachines, for example, weav-.
. apparatus operating at yarn speeds within the capabilities of available airpressure, it being understood that a high traveling speed of yarn enabling insufiicient exposure to the gas jet assembly would not produce the desired results.
The resonance chamber described herein and considered to be a critical feature of the present invention collects gas emerging throughfthejet orifice after pas- Inexits, the same operates asa cushion and also provides a back pressure vibrating at a resonant frequency. to assist in intermingling of filaments within the yarn bundle.
This chamber, therefore, is believed to operate as. a hexible battle and the same produces considerably improved results over the rigid bafiies heretofore used or unbafiled thrusts of air. I
As indicated earlier, it"is important that yarn traveling through the intertwining assembly be substantially restrained fromall but longitudinal movement. With such an arrangement, any vibration produced by the jet blast will be limited to wave length-or nodes defined by the spacingd between the thread guides Accordinglygrjnore. orderly entanglement and less air bulking of yarn occurs.
tween 0.05 grn./den. and 0.3 gm./den. along a rectilinear path in which the yarn at the points of entering and leaving the path is held against substantial lateral vibration, directing a jet of gas across "the yarn path and into a confined resonance zone under sufiicient pressure to create a greater loudness in that area than can normally be borne by the human ear, and correlating the pressure with the tension on the yarn.
2. A method of intertwining a substantially untwisted thermoplastic synthetic high polymer multi-filament yarn which comprises drawing said yarn under a low tension along a rectilinear path in which the yarn at the points of entering and leaving the path is held against substantial lateral vibration, directing a jet of gas across the yarn path and into a confined resonance zone under a pressure of 3 to 5 atmospheres to create a loudness which could not normally be borne by the human ear and inhibiting the noise in the resonance zone to thereby permit such pressure, and correlating the pressure with the tension on the yarn.
3. A method of intertwining a substantially untwisted thermoplastic synthetic high polymer multi-filarnent yarn which comprises drawing said yarn under a low tension along a rectilinear path in which the yarn at the points of entering and leaving the path is held against substantial lateral vibration, directing a jet of gas across the yarn path and into a confined resonance zone under sufficient pressure to create a maximum loudness which could not normally be borne by the human ear and inhibiting the noise in the resonance zone to thereby permit 10 such pressure, and correlating the pressure with the ten sion on the yarn to obtain a yarn coherency factor of at least 1.5.
4. An apparatus for intertwining a substantially untwisted thermoplastic synthetic high polymer multifilament yarn which comprises a nozzle having a fine orifice for supplying gas under pressure, a cylindrical resonance chamber having an opening disposed opposite the nozzle orifice at a distance from 1 to 3 mm., said opening having a diameter between 1.0 and 1.8 times the exit diameter of said orifice sound damping means surrounding said chamber, yarn guides located above and below the nozzle and chamber to position the yarn between the nozzle and the opening to the chamber, said guides embodying means to dampen the vibration of the yarn passing therebetween and to localize the nodes at those points, said guides being spaced from 20-55 mm. apart.
References Cited in the file of this patent UNITED STATES PATENTS 1,115,704 Manes Nov. 3, 1914 2,629,544 Ohmart Feb. 24, 1953 2,928,589 Davey Mar. 15, 1960 2,985,995 Bunting et a1. May 30, 1961 3,110,151 Bunting et al. Nov. 12, 1963 FOREIGN PATENTS 554,150 Canada Mar. 11, 1958
Claims (1)
- 4. AN APPARATUS FOR INTERWINING A SUBSTANTIALLY UNTWISTED THERMOPLASTIC SYNTHETIC HIGH POLYMER MULTIFILAMENT YARN WHICH COMPRISES A NOZZLE HAVING A FINE ORIFICE FOR SUPPLYING GAS UNDER PRESSURE, A CYLINDRICAL RESONANCE CHAMBER HAVING AN OPENING DISPOSED OPPOSITE THE NOZZLE ORIFICE AT A DISTANCE FROM 1 TO 3 MM., SAID OPENING HAVING A DIAMETER BETWEEN 1 TO 3 MM., SAID OPENING HAVING A DIAMETER BETWEEN 1.0 AND 1.8 TIMES THE EXIT DIAMETER OF SAID ORIFICE SOUND DAMPING MEANS SURROUNDING SAID CHAMBER, YARN GUIDES LOCATED ABOVE AND BELOW THE NOZZLE AND CHAMBER TO POSITION THE YARN BETWEEN THE NOZZLE AND THE OPENING TO THE CHAMBER, SAID GUIDES EMBODYING MEANS TO DAMPEN THE VIBRATION OF THE YARN PASSING THEREBETWEEN AND TO LOCALIZE THE NODES AT THOSE POINTS, SAID GUIDES BEING SPACED FROM 20-55 MM. APART.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NL271935 | 1961-11-28 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3167847A true US3167847A (en) | 1965-02-02 |
Family
ID=19753443
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US238506A Expired - Lifetime US3167847A (en) | 1961-11-28 | 1962-11-19 | Treatment of multi-filament yarn |
Country Status (4)
Country | Link |
---|---|
US (1) | US3167847A (en) |
CH (1) | CH402271A (en) |
ES (1) | ES282849A1 (en) |
GB (1) | GB990593A (en) |
Cited By (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3304593A (en) * | 1965-01-21 | 1967-02-21 | Burklund Lab Inc | Yarn bulking method and apparatus |
US3339362A (en) * | 1966-07-05 | 1967-09-05 | Du Pont | Method of joining strands |
US3363294A (en) * | 1964-12-18 | 1968-01-16 | American Enka Corp | Self-closing tangling jet apparatus |
US3385048A (en) * | 1963-02-08 | 1968-05-28 | Snia Viscosa | Multifilament yarn |
US3394440A (en) * | 1965-08-20 | 1968-07-30 | American Enka Corp | Continuous filament interlacing, bulking or tangling apparatus |
US3417445A (en) * | 1965-06-23 | 1968-12-24 | Ver Glanztoff Fabriken A G | Method and apparatus for producing a voluminous yarn with uniformly spaced bindings |
US3425108A (en) * | 1966-02-09 | 1969-02-04 | Bemberg Spa | Device and method for treating a running artificial multifilamentary thread with a gas jet |
US3425107A (en) * | 1965-10-11 | 1969-02-04 | Kanebo Ltd | Apparatus for developing crimps by heating composite filament |
US3474510A (en) * | 1966-11-17 | 1969-10-28 | Renato Torsellini | Process and a device for producing interlaced filament synthetic and artificial yarns |
US3484914A (en) * | 1966-06-13 | 1969-12-23 | Bemberg Spa | Method and means for treating with a gasiform stream a thread bundle made of a plurality of elementary threads |
US3488671A (en) * | 1967-08-30 | 1970-01-06 | Rhodiaceta Ag | Process and device for preparing a tangle fiber |
US3537248A (en) * | 1967-06-19 | 1970-11-03 | Glanzstoff Ag | Simultaneously twisting and interlacing a continuous multifilament yarn |
US3571868A (en) * | 1967-11-30 | 1971-03-23 | Rhodiaceta | Apparatus for interlacing continuous filaments |
US3701248A (en) * | 1969-02-24 | 1972-10-31 | Du Pont | Interlaced multifilament yarn |
US3823449A (en) * | 1971-12-27 | 1974-07-16 | Akzona Inc | Apparatus for interlacing yarns |
US3863435A (en) * | 1973-03-20 | 1975-02-04 | Du Pont | Method for restringing a threadline |
US3875625A (en) * | 1973-03-05 | 1975-04-08 | Rhone Poulenc Textile | Apparatus for interlacing filaments of multifilament yarns |
US3905075A (en) * | 1974-09-06 | 1975-09-16 | Allied Chem | Noise reduction and heat zone separation system |
US4030651A (en) * | 1976-09-21 | 1977-06-21 | Allied Chemical Corporation | Interfloor tube aspirator muffler |
US4035883A (en) * | 1975-03-14 | 1977-07-19 | Fiber Industries, Inc. | Multipurpose intermingling jet and process |
US4043008A (en) * | 1976-09-08 | 1977-08-23 | Allied Chemical Corporation | Noise reduction system |
DE2813368A1 (en) * | 1977-03-30 | 1978-10-05 | Toray Industries | METHOD AND DEVICE FOR BRAIDING A MULTI-THREAD YARN |
US4237187A (en) * | 1979-02-26 | 1980-12-02 | Allied Chemical Corporation | Highly oriented, partially drawn, untwisted, compact poly(ε-caproamide) yarn |
US4535516A (en) * | 1980-08-18 | 1985-08-20 | Maschinenfabrik Rieter Ag | Apparatus for the production of fixed point multifilament yarns |
US4563799A (en) * | 1982-10-08 | 1986-01-14 | Barmag Barmer Maschinenfabrik Ag | Air jet nozzle for treatment of yarns |
EP1600535A1 (en) * | 2004-05-29 | 2005-11-30 | Schärer Schweiter Mettler AG | Housing |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1492945A (en) * | 1966-05-16 | 1967-08-25 | Rhodiaceta | Method and device for the manufacture of a yarn with interlaced strands and products obtained |
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US1115704A (en) * | 1913-12-23 | 1914-11-03 | Edward Manes | Pneumatic-hammer muffler. |
US2629544A (en) * | 1947-12-17 | 1953-02-24 | Nash Kelvinator Corp | Refrigerating apparatus |
CA554150A (en) * | 1958-03-11 | A. Hartley Kenneth | Treatment of threads | |
US2928589A (en) * | 1958-10-31 | 1960-03-15 | Gen Electric | Hermetically-sealed, motor compressor unit including noise reducing means |
US2985995A (en) * | 1960-11-08 | 1961-05-30 | Du Pont | Compact interlaced yarn |
US3110151A (en) * | 1961-05-26 | 1963-11-12 | Du Pont | Process for producing compact interlaced yarn |
-
1962
- 1962-11-19 US US238506A patent/US3167847A/en not_active Expired - Lifetime
- 1962-11-22 CH CH1377962A patent/CH402271A/en unknown
- 1962-11-26 GB GB44566/62A patent/GB990593A/en not_active Expired
- 1962-11-27 ES ES282849A patent/ES282849A1/en not_active Expired
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA554150A (en) * | 1958-03-11 | A. Hartley Kenneth | Treatment of threads | |
US1115704A (en) * | 1913-12-23 | 1914-11-03 | Edward Manes | Pneumatic-hammer muffler. |
US2629544A (en) * | 1947-12-17 | 1953-02-24 | Nash Kelvinator Corp | Refrigerating apparatus |
US2928589A (en) * | 1958-10-31 | 1960-03-15 | Gen Electric | Hermetically-sealed, motor compressor unit including noise reducing means |
US2985995A (en) * | 1960-11-08 | 1961-05-30 | Du Pont | Compact interlaced yarn |
US3110151A (en) * | 1961-05-26 | 1963-11-12 | Du Pont | Process for producing compact interlaced yarn |
Cited By (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3385048A (en) * | 1963-02-08 | 1968-05-28 | Snia Viscosa | Multifilament yarn |
US3363294A (en) * | 1964-12-18 | 1968-01-16 | American Enka Corp | Self-closing tangling jet apparatus |
US3304593A (en) * | 1965-01-21 | 1967-02-21 | Burklund Lab Inc | Yarn bulking method and apparatus |
US3417445A (en) * | 1965-06-23 | 1968-12-24 | Ver Glanztoff Fabriken A G | Method and apparatus for producing a voluminous yarn with uniformly spaced bindings |
US3394440A (en) * | 1965-08-20 | 1968-07-30 | American Enka Corp | Continuous filament interlacing, bulking or tangling apparatus |
US3425107A (en) * | 1965-10-11 | 1969-02-04 | Kanebo Ltd | Apparatus for developing crimps by heating composite filament |
US3425108A (en) * | 1966-02-09 | 1969-02-04 | Bemberg Spa | Device and method for treating a running artificial multifilamentary thread with a gas jet |
US3484914A (en) * | 1966-06-13 | 1969-12-23 | Bemberg Spa | Method and means for treating with a gasiform stream a thread bundle made of a plurality of elementary threads |
US3339362A (en) * | 1966-07-05 | 1967-09-05 | Du Pont | Method of joining strands |
US3474510A (en) * | 1966-11-17 | 1969-10-28 | Renato Torsellini | Process and a device for producing interlaced filament synthetic and artificial yarns |
US3537248A (en) * | 1967-06-19 | 1970-11-03 | Glanzstoff Ag | Simultaneously twisting and interlacing a continuous multifilament yarn |
US3488671A (en) * | 1967-08-30 | 1970-01-06 | Rhodiaceta Ag | Process and device for preparing a tangle fiber |
US3571868A (en) * | 1967-11-30 | 1971-03-23 | Rhodiaceta | Apparatus for interlacing continuous filaments |
US3701248A (en) * | 1969-02-24 | 1972-10-31 | Du Pont | Interlaced multifilament yarn |
US3823449A (en) * | 1971-12-27 | 1974-07-16 | Akzona Inc | Apparatus for interlacing yarns |
US3875625A (en) * | 1973-03-05 | 1975-04-08 | Rhone Poulenc Textile | Apparatus for interlacing filaments of multifilament yarns |
US3863435A (en) * | 1973-03-20 | 1975-02-04 | Du Pont | Method for restringing a threadline |
US3905075A (en) * | 1974-09-06 | 1975-09-16 | Allied Chem | Noise reduction and heat zone separation system |
US4035883A (en) * | 1975-03-14 | 1977-07-19 | Fiber Industries, Inc. | Multipurpose intermingling jet and process |
US4043008A (en) * | 1976-09-08 | 1977-08-23 | Allied Chemical Corporation | Noise reduction system |
US4030651A (en) * | 1976-09-21 | 1977-06-21 | Allied Chemical Corporation | Interfloor tube aspirator muffler |
DE2813368A1 (en) * | 1977-03-30 | 1978-10-05 | Toray Industries | METHOD AND DEVICE FOR BRAIDING A MULTI-THREAD YARN |
US4417375A (en) * | 1977-03-30 | 1983-11-29 | Toray Industries, Inc. | Apparatus for interlacing multifilament yarn by fluid |
US4237187A (en) * | 1979-02-26 | 1980-12-02 | Allied Chemical Corporation | Highly oriented, partially drawn, untwisted, compact poly(ε-caproamide) yarn |
US4535516A (en) * | 1980-08-18 | 1985-08-20 | Maschinenfabrik Rieter Ag | Apparatus for the production of fixed point multifilament yarns |
US4563799A (en) * | 1982-10-08 | 1986-01-14 | Barmag Barmer Maschinenfabrik Ag | Air jet nozzle for treatment of yarns |
EP1600535A1 (en) * | 2004-05-29 | 2005-11-30 | Schärer Schweiter Mettler AG | Housing |
US20060010668A1 (en) * | 2004-05-29 | 2006-01-19 | Martin Meinhardt | Housing |
US7207094B2 (en) | 2004-05-29 | 2007-04-24 | SSM Schärer Schweiter Mettler AG | Housing |
Also Published As
Publication number | Publication date |
---|---|
ES282849A1 (en) | 1963-01-16 |
GB990593A (en) | 1965-04-28 |
CH402271A (en) | 1965-11-15 |
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