WO2005028722A1 - Composite twist core-spun yarn and method and device for its production - Google Patents
Composite twist core-spun yarn and method and device for its production Download PDFInfo
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- WO2005028722A1 WO2005028722A1 PCT/US2004/030253 US2004030253W WO2005028722A1 WO 2005028722 A1 WO2005028722 A1 WO 2005028722A1 US 2004030253 W US2004030253 W US 2004030253W WO 2005028722 A1 WO2005028722 A1 WO 2005028722A1
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- core
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- 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
- D02G3/00—Yarns or threads, e.g. fancy yarns; Processes or apparatus for the production thereof, not otherwise provided for
- D02G3/22—Yarns or threads characterised by constructional features, e.g. blending, filament/fibre
- D02G3/36—Cored or coated yarns or threads
-
- 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
- D02G3/00—Yarns or threads, e.g. fancy yarns; Processes or apparatus for the production thereof, not otherwise provided for
- D02G3/22—Yarns or threads characterised by constructional features, e.g. blending, filament/fibre
- D02G3/36—Cored or coated yarns or threads
- D02G3/367—Cored or coated yarns or threads using a drawing frame
Definitions
- This invention relates to a composite twist-spun yarn of the type having a central "hard" core covered with a dual-spun fiber covering, as well as to fabrics woven or knitted from the composite dual core-spun yarn, and to a method and a device for production of the yarn.
- Elongation at break of a yarn specimen is the increase in length produced by the breaking force, expressed as a percentage of the original nominal length. All values of elongation at break in the present disclosure are those established according to the methodology based ISO 2062, according to which a specimen of yarn is extended until rupture by a suitable mechanical device and elongation at break are recorded. A constant rate of specimen extension of 100% per minute (based on the specimen length) is used.
- Twist spun yarns with a central core covered with a dual-spun fiber covering are produced by bringing together two fiber slivers to form a spinning triangle, feeding the core in the spinning triangle between the two fiber slivers with the latter at an angle to the core, and spinning the brought-togefher fiber slivers around the core with an S or Z twist that is the same as or opposite to that of the core.
- This so-called Siro-core-spun process - which has the advantage of being a "one-step” spinning process - has been successful in particular for producing stretchable yarns that are widely used for manufacturing stretch fabrics.
- stretch yarns have elastane cores made for example of the polyurethane-elastane available from E. I. du Pont de Nemours and Company, Wilmington, Delaware, U.S.A., under the trademark LYCRA ® .
- Elastane cores typically have an elongation at break of 400%. or more.
- the elastane core is drafted between 250% and 350%, such that the elasticity of the core "takes up" the fiber covering, leading to the production of composite elastic yarns with consistent stretch and coverage by the fiber covering.
- substantially inelastic cores elongation at break less than 50%, usually well below 50%, and rarely exceeding 40%
- the torsion coefficient of the core (discussed further below) is equal to the value of the critical torsion coefficient of the yarn less the value of the total torsion coefficient of the composite yam multiplied by the proportion of the core yam in the composite yam.
- the process of EP 0 271 418 has the disadvantage that the produced core yam necessarily has a resulting torque.
- two of the covered yams must be assembled by twisting them together in opposite directions, as will be explained below in connection with Fig. 3. This implies a two step spinning process, which is less attractive.
- the invention provides a composite twist-spun yarn with substantially no torque (referred to herein as "substantially torqueless") and having a central hard core covered with a dual-spun fiber covering, wherein the central hard core has an elongation at break less than or equal to 50% and has a Z or S twist, and the fiber covering comprises dual-spun fibers twisted on the core with an S or Z twist opposite to that of the core, the opposite twists of the core and of the covering exerting opposite and substantially equal torques.
- the composite yam according to the invention is substantially torqueless by “cancellation" of the substantially equal and opposite torques of the core and the cover, as will be further discussed below with reference to Figs. 1 and 2.
- Another main aspect of the invention is a process for producing a substantially torqueless composite twist-spun yam having a central hard core covered with a dual- spun fiber covering, wherein the central hard core has an elongation at break less than 50%).
- the process according to the invention comprises the following steps: bringing together two fiber slivers to form a spinning triangle; feeding the substantially inextensible central hard core in the spinning triangle between the two fiber slivers with the latter at an angle to the central core, the fed core being guided in the spinning triangle and having a Z or S twist that is overtwisted relative to the twist of the finished composite yam; controlling the speed of feeding the core in the spinning triangle to compensate for the angle between the slivers and the core and for detwisting elongation of the core; and spinning the brought-together fiber slivers around the core with an S or Z twist opposite to that of the core and corresponding to about 30% to about 70% of the twist of the fed overtwisted core to obtain said substantially torqueless composite core-spun yarn.
- a further main aspect of the invention is a device for producing a substantially torqueless composite twist-spun yam having a central hard core covered with a dual- spun fiber covering, wherein the central hard core has an elongation at break less than 50%, the core has an Z or S winding and the fiber covering has an S or Z winding opposite to that of the core.
- the device comprises: means for bringing together two fiber slivers in a spinning triangle; means for feeding the substantially-inextensible central hard core in the spinning triangle between the two fiber slivers whereby the core is guided in the spinning triangle with the two fiber slivers at an angle to the central core, the core having a Z or S winding that is overtwisted relative to the twist of the finished composite yam; means for controlling the speed of feeding the core in the spinning triangle to compensate for the angle between the slivers and the core and for detwisting elongation of the core; and means for spinning the brought-together fiber slivers around the core with an S or Z winding opposite to that of the core and corresponding to about 30% to about 70% of the twist of the fed overtwisted central hard core to obtain said substantially torqueless composite core-spun yarn.
- the invention also covers a fabric woven or knitted from the essentially torqueless composite twist-spun yam having a substantially inextensible hard core and a dual-spun fiber covering as set
- Fig. 1 is a schematic representation of a substantially torqueless composite twist-spun yam according to the invention
- Figs. 2A and 2B are diagrams illustrating the calculation of the moment of inertia for a twist-spun yarn according to the invention
- Fig. 3 is a schematic representation of a dual yam made by assembling two yams produced by the method of EP 0271 418
- Fig. 4A is a schematic representation of a spinning device according to the invention
- Fig. 4B is a diagram of the spinning triangle of the device shown in Fig. 4A
- Fig. 1 is a schematic representation of a substantially torqueless composite twist-spun yam according to the invention
- Figs. 2A and 2B are diagrams illustrating the calculation of the moment of inertia for a twist-spun yarn according to the invention
- Fig. 3 is a schematic representation of a dual yam made by assembling two yams produced by the method of EP 0271 418
- FIG. 5 is a diagram showing an arrangement of rollers for feeding the core and the slivers to the spinning triangle;
- Fig. 6 is a diagrammatic cross-section along line VI- VI of Fig. 5 illustrating the means for guiding the core, the latter not being shown;
- Fig. 7 A is a photograph of an example of a composite core-spun yam produced according to the invention;
- Fig. 7B is a corresponding photograph of a comparative yam;
- Fig. 8 A is a photograph of another example of a composite core-spun yam produced according to the invention; and
- Fig 8B is a corresponding photograph of another comparative yam.
- a substantially inextensible and torqueless composite yam 10 is twist spun with an essentially inextensible central hard core 20 having a covering 30.
- the core 20 has an elongation at break less than 50%.
- Cores/yams that are substantially inelastic typically have elongation at break well below 50%, usually below 40%.
- a core/yam is extensible its elongation at break is usually well above 50%, typically several hundred%.
- the core 20 is conveniently chosen from monofilaments, multiple filaments, spun yams and composites thereof.
- the core 20 can be made of materials chosen from glass, metal, synthetic fibers and filaments, carbon multifilaments and fibers, artificial fibers, natural fibers, antistatic fibers and composites thereof, according to the desired characteristics and the intended application of the final twist-spun composite yam 10.
- a core 20 made of aramid fibers is advantageous.
- Commercially available meta-aramid fibers for example those available under the trademark NOMEX ® from E. I.
- du Pont de Nemours and Company Wilmington, Delaware, U.S.A.
- Commercially available para-aramid fibers (for example those available under the trademark KEVLAR ® from E. I. du Pont de Nemours and Company, Wilmington, Delaware, U.S.A.) have an elongation at break in the range 0-5%.
- Other core materials can be used, depending on the application.
- a core made of glass fibers typically has an elongation at break from 0-5%>, whereas those made of polyester and cotton typically have an elongation at break from 5-30%.
- the covering 30 can be made of synthetic, artificial or natural fibers chosen according to the desired yam characteristics and function.
- the fiber covering 30 can be a functional covering providing at least one of: high visibility (e.g., tinted viscose), low friction (e.g., PTFE), reinforcement (e.g., para-aramids), light-fastness (e.g., pigmented fibres), aesthetic appearance (e.g., meta-aramids or viscose), UN-protection (e.g., UN protective fibres), protection of the core (e.g., polyester, polyamide, viscose, PVA, or polyvinyl alcohol), abrasion resistance (e.g., meta- or para-aramids), protection against heat and thermal performance (e.g., meta-aramids, PBI, polybutylimide, PBO, polybenzoxazole, POD, or poly-p phenyline oxadiazole), fire- resistance (e.g., meta-aramids, PBI, or PBO), cut resistance (e.g., para-aramids or HPPE, high-
- the covering 30 can conveniently be made of viscose fibers.
- the central hard core 20 of the substantially inextensible and substantially torqueless yarn 10 can be covered to any suitable degree as required by the intended application.
- the % covering of the core 20 can be estimated by visual inspection of the composite fibers, especially when the cores and coverings are of contrasting colors. This estimation can be made directly or using photographs or video images, as in the Examples below.
- the core 20 typically constitutes 10-30 wt% of the total weight of the composite yam 10.
- the core mass is defined by the linear density of the core 20 (mass per unit length) measured by the skein method as described by the norm ISO 2060.
- the covering fiber mass is defined as the difference of the final yam linear density reduced by the core linear density.
- the linear mass of the composite yam is typically from 20-120 tex, and that of the covering is typically from 15-100 tex.
- Yam Torque As schematically illustrated in Fig. 1, the composite yam 10 according to the invention is substantially torqueless by "cancellation" of the substantially equal and opposite torques Ti of the core 20 and T 2 of the cover 30, as indicated by the arrows.
- the composite yam of the invention being substantially torqueless, has no tendency to twist. Moreover, when two substantially torqueless yams 10 (or yam sections) come to touch, they have no tendency to wrinkle. The presence or absence of torque in a yam can be checked by a simple test, as follows.
- a length of yarn is held approximately horizontally with outstetched arms, i.e., with the horizontal yam occupying 100% of its length. Then the two hands are slowly brought together, allowing the yam to droop. As the hands come together, if the yam has an inherent torque, the yam winds into a spiral as it comes together. When the hands meet, the wound yam is tangled and it is difficult to pull it apart again. On the other hand, if the yam has no or substantially no torque, as the hands come together the yam remains untangled or at most has only a few winds, so that when the hands meet they can easily be moved apart to bring the yam back to its initial horizontal position.
- the coefficient of torsion is a factor ⁇ giving the relation of the twist level of a yam with the square root of its linear density expressed in "Cotton metric count" (also called “Number Metric” Nm).
- FIG. 2 diagrammatically illustrates a composite torqueless yarn according to the invention whose core 20 has a diameter d core and whose covering 30 has a diameter d tota i-
- G Modulus 0 f inerti of the aterial
- This factor k for compensating the detwisting elongation of the core 20 is measured empirically for each core having regard to its dimensions and physical properties, either by testing on the spinning machine used in the process, or using a laboratory twist measurement machine.
- the twist coefficient in the composite core can be the same as the twist coefficient of the cover. However, the twist in rums per meter will be different.
- Fig. 3 schematically shows a composite twist-spun yam 10' produced by the process of European Patent 0 271 418.
- the yam 10 'produced by this process comprises a core 20', in particular an aramid core, with a covering 30'.
- Each yam is spun with the torsion coefficient of core 20' appreciably less than its critical torsion coefficient.
- the covering fibers 30' are spun on the core 20' such that the total torsion coefficient of the yarn 10' is less than its critical torsion coefficient. This leads to a twist-spun yam having a core 20' with a twist t 1 surrounded by a covering 30' twisted in the same direction with a twist t . Because each individual yam 10' is twisted, to produce a composite yarn with neutral torque two of the covered yams 10' must be assembled after spinning by twisting them together in opposite directions with an applied twist T ⁇ opposite to t l5 t 2 , as illustrated in Fig. 3.
- the slivers 30A,30B are fed to the spinning triangle 40 at a speed V, and the core 20 is fed to the spinning triangle 40 at a speed close to kN.cos ⁇ , where k is the above-mentioned factor compensating for the detwisting elongation of the core 20.
- This speed control combined with the below-described accurate guiding of the core 20, ensures that the slivers 30A,30B and the core 20 meet at the convergence point 41 of the spinning triangle 40 under optimal spinning conditions avoiding problems related in particular with the inextensibility of the core 20 and its overtwisting.
- the two inclined slivers 30A,30B are obtained typically by feeding from two parallel rovings 30C,30D, which can be achieved using known equipment that is adapted so the substantially inextensible and over-twisted hard core 20 is guided and driven into the spinning triangle 40 at a controlled speed, as explained above.
- This controlled speed of core 20 is set by a positive drive on the core 20 or by braking an overfed core 20.
- Positive drive can be provided by inserting a gear mechanism in the kinematic chain of the spinning frame, or by using an individual motor with a special control.
- Braking of the core 20 can be achieved by means of a braking roller, or other convenient means.
- the two fiber slivers 30C,30D are brought together in the spinning triangle 40 by passing over a feed roller 50 having lateral smooth guide surfaces 51 for the slivers 30C,30D, this feed roller 50 cooperating with a facing roller 60, see Fig. 5.
- the core 20 is guided in the spinning triangle 40 by passing through a guide groove 52 centrally located on the feed roller 50.
- the core is fed over a centering roller 55 cooperating with the feed roller 50.
- the centering roller 55 has a central V-shaped pre-guide groove 56.
- Guide groove 52 is advantageously of substantially U-shaped cross section, the width and depth of groove 52 being sufficient to receive the hard core 20.
- a groove 52 of another shape can be used provided it guides well the hard core 20 and prevents it from jumping over the cylindrical surface 51 of the feed roller 50.
- the width of groove 52 is chosen as function of the size of the feed roller 50, and is sufficiently small to avoid that the "freely slipping" slivers 30A,30B risk moving over the smooth surface of feed roller 50 and entering the groove 52.
- the groove 52 must be sufficiently large that it can receive the core 20 and allow movement of the core 20 in the groove 52 independent from movement of the roller 50.
- A. referred shape for groove 52 is a U-shape with flat facing sides and chamfered edges. Typically the groove 52 is 1-3 mm wide and 1-20 mm deep.
- the depth of the groove is limited by the need to reduce rubbing of the core 20 against the sides of groove 52, so in principle the wider the groove 52 the deeper it can be.
- the V-shaped pre-guide groove 56 in the centering roller 55 can be wider than the groove 52.
- the dimensions of pre-guide groove 56 are not critical: what counts is that the apex of pre-guide groove 56 is centered exactly over the center of guide groove 52, so as to feed the core 20 accurately and centrally into the middle of groove 52, avoiding contact of the core 20 with the groove 52's edges.
- the pre-guide groove 56 can be similar to the known V-shaped grooves used to feed an elastomeric core onto a non-grooved feed cylinder in the conventional Siro-core-spun process.
- the V-shaped groove 56 is used for a new purpose, to ensure perfect positioning of the core 20 in the central guide groove 52.
- the fed core 20 tends to jump as a result of tensions created due to the low elasticity of the core 20 and varying forces acting at the point of convergence 41.
- the fed core 20 is initially twisted in the S or Z direction with a twist that is overtwisted relative to the twist of the finished composite yarn direction.
- the brought-together slivers 30A,30B are spun around the core 20 with a twist opposite to that of the core 20 and corresponding to about 30% to 70% of the twist, of the overfed core 20.
- the core 20 will be obliged to twist in the opposite direction of its original twist. This process is called detwisting.
- the core 20 will naturally elongate as the orientation of the individual fibres are closer to parallel to the yam axis.. For this reason, the speed of feeding of the core 20 is adjusted to compensate for this elongation, as described above.
- Example 1 This example was performed on a laboratory spinning machine, spinntester SKF 82 equipped with PK 600 type arms designed for long staple processing also called worsted spinning.
- the core yarn (20) was a black KEVLAR ® para-aramid spun yam with 100 dtex (Nm 100/1).
- This core yam was spun from stretch-broken KEVLAR ® fibers having a length of approximately 100 rrirn, spun in the Z direction with 800 turns/meter. The yam was previously steamed.
- the core yarn was positively fed at a speed of 16 m/min using a yam-drive control system. For this, the core yam was passed between a set of rolls driven at the given speed, and a heavy rubber-coated metallic roll. The core yarn was deviated to the centering roller (55) and engaged in the fine guide groove (52) in the feed roller (50). This guide groove (52) was of approximately U-shaped cross-section, width 0.5 mm, depth 1 mm. The speed of the feed roller (50) was adjusted at 17.5 m/min.
- Fig. 7A is a photograph of the resulting composite core-spun yam (10) taken under a microscope using light from a Mercury short arc lamp. As can be seen the core is well covered, practically 100%. The resulting composite core-spun yam is also substantially neutral, i.e., with virtually zero torque.
- Table I summarizes the above-described conditions for Example 1, as well as the corresponding conditions for Example 2 (Comparative), Example 3 and Example 4 (Comparative). Table I
- Example 2 (Comparative) This Comparative Example duplicated the conditions of Example 1, except that the special grooved feed roller was replaced by a standard non-grooved feed roller and the core yam was not fed at a controlled speed using positive drive, but was fed over the feed roller (cylinder) in the normal way.
- Fig. 7B is a photograph like Fig. 7 A of the resulting comparative yarn. It can be seen from Fig. 7B that the black "core" of the resulting yam was spirally wound with the lighter-colored spirally wound "cover”. The spiral black “core” is clearly visible.
- the resulting yam unlike that according to the invention, does not have a central core covered by the covering, but the two are wound together forming a composite twisted yam. The core of this composite yam is practically not covered. We can say that the covering is practically 0%.
- Example 3 Example 3 repeats Example 1 except for the fact that the core was a yellow
- Example 4 This Comparative Example duplicated the conditions of Example 3, except that the special grooved feed roller was replaced by a standard non-grooved feed roller and the core yarn was not fed at a controlled speed using positive drive, but was fed over the feed roller (cylinder) in the nom al way.
- Fig. 8B is a photograph like Fig. 8 A of the resulting comparative yarn. It can be seen from Fig.
- Example 5 This Example was performed on a full-size commercial spinning machine specially adapted to operate according to this invention, to produce a high visibility composite yam having a core (20) of poly (metaphenylene isophthalimide) (MPD-I) staple fiber and a covering (30) of crimped flame-retardant viscose (FRV) which is a regenerated cellulosic fiber incorporating a flame-retardant chlorine-free phosphorous and sulfur-containing pigment, available under the trademark "Lenzing FR".
- the FRV fibers had a staple cut length of approximately 5 to 9 cm and an average measured staple length of 6.8 cm.
- the FRV fibers were separately stock died in a high visibility yellow color.
- These fibers were prepared according to the conventional long staple processing also called worsted spinning into two fine roving slivers of 6666 dtex (Nm 1.5) each.
- the core was spun from a crimped non-dyed (natural color) 100% poly (metaphenylene isophthalimide) (MPD-I) staple fiber, having a cut length in the range 8 to 12 cm and an average measured staple length of 10 cm.
- MPD-I poly (metaphenylene isophthalimide)
- the core yarn had a count of 10 tex and a twist of 800 tpm in the Z-direction.
- This staple core yam was treated with steam to stabilize partly the yarn, and the steamed yam was rewound on a special bobbin designed for cooperation with the devices on the spinning frame for fixing the core yam bobbin.
- the core yarn tension was regulated using a yarn braking device, in addition to a positive feeding device.
- the core yarn was fed into the spinning system using a suitable centering roll (55) on top of the central guide groove (52) in the feed roll (50). The feed roll was working with 20 m/min.
- the covering (30) was spun in the S-direction with a speed of 9000 turns per minute applying a twist of 450 tpm in the S-direction.
- the resulting composite yam (10) had a cotton count of 20/1 or an approximate linear density of 450 denier (55 dtex). It was essentially neutral, i.e., torqueless.
- the resulting composite yams were woven at high speed in combination with
- the composite twist-spun yams of the invention were on top.
- the resulting composite yarn was also knitted into a Jersey fabric with 194 grams per square meter.
- Both knitted and woven fabric passed the test for high visibility using the EN 471 method, as well as the "limited flame spread" test as defined in the EN532.
- This Example establishes that the method of the invention can be performed on a large scale under commercial high-speed spinning conditions leading to a perfectly satisfactory composite twist spun yam of neutral torque in a one-step spinning process, and that the resulting composite twist spun yam can be processed by large scale weaving processes to produce fabrics of desirable properties.
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- Mechanical Engineering (AREA)
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Abstract
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Priority Applications (8)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP04784199A EP1664407B1 (en) | 2003-09-15 | 2004-09-15 | Composite twist core-spun yarn and method and device for its production |
| BRPI0413942A BRPI0413942B8 (en) | 2003-09-15 | 2004-09-15 | PROCESS FOR THE PRODUCTION OF A DOUBLE SPINN CORE COMPOSITE YARN, DOUBLE SPINN CORE COMPOSITE YARN AND DEVICE FOR THE PRODUCTION OF A CORE DOUBLE SPINN COMPOSITE YARN |
| CA2538787A CA2538787C (en) | 2003-09-15 | 2004-09-15 | Composite twist core-spun yarn and method and device for its production |
| DE602004006634T DE602004006634T2 (en) | 2003-09-15 | 2004-09-15 | CABLE COVER AND METHOD AND DEVICE FOR ITS MANUFACTURE |
| KR1020067005129A KR101102655B1 (en) | 2003-09-15 | 2004-09-15 | Composite combustible core-spun yarn and method and apparatus for manufacturing same |
| MXPA06002670A MXPA06002670A (en) | 2003-09-15 | 2004-09-15 | Composite twist core-spun yarn and method and device for its production. |
| CN2004800266461A CN1853008B (en) | 2003-09-15 | 2004-09-15 | Composite twist core-spun yarn and method and device for its production |
| JP2006527008A JP4435166B2 (en) | 2003-09-15 | 2004-09-15 | Composite twisted core spun yarn and method and apparatus for manufacturing the same |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/663,546 | 2003-09-15 | ||
| US10/663,546 US7155891B2 (en) | 2003-09-15 | 2003-09-15 | Composite twist core-spun yarn and method and device for its production |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2005028722A1 true WO2005028722A1 (en) | 2005-03-31 |
Family
ID=34274404
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/US2004/030253 Ceased WO2005028722A1 (en) | 2003-09-15 | 2004-09-15 | Composite twist core-spun yarn and method and device for its production |
Country Status (10)
| Country | Link |
|---|---|
| US (2) | US7155891B2 (en) |
| EP (1) | EP1664407B1 (en) |
| JP (1) | JP4435166B2 (en) |
| KR (1) | KR101102655B1 (en) |
| CN (1) | CN1853008B (en) |
| BR (1) | BRPI0413942B8 (en) |
| CA (1) | CA2538787C (en) |
| DE (1) | DE602004006634T2 (en) |
| MX (1) | MXPA06002670A (en) |
| WO (1) | WO2005028722A1 (en) |
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- 2004-09-15 EP EP04784199A patent/EP1664407B1/en not_active Expired - Lifetime
- 2004-09-15 KR KR1020067005129A patent/KR101102655B1/en not_active Expired - Lifetime
- 2004-09-15 MX MXPA06002670A patent/MXPA06002670A/en active IP Right Grant
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Also Published As
| Publication number | Publication date |
|---|---|
| JP4435166B2 (en) | 2010-03-17 |
| KR20060076294A (en) | 2006-07-04 |
| BRPI0413942A (en) | 2006-10-24 |
| JP2007506006A (en) | 2007-03-15 |
| US20070062172A1 (en) | 2007-03-22 |
| EP1664407B1 (en) | 2007-05-23 |
| CN1853008A (en) | 2006-10-25 |
| US20050055997A1 (en) | 2005-03-17 |
| CA2538787C (en) | 2012-03-20 |
| CN1853008B (en) | 2012-07-18 |
| CA2538787A1 (en) | 2005-03-31 |
| BRPI0413942B8 (en) | 2023-01-31 |
| MXPA06002670A (en) | 2006-06-06 |
| US7493747B2 (en) | 2009-02-24 |
| DE602004006634D1 (en) | 2007-07-05 |
| US7155891B2 (en) | 2007-01-02 |
| DE602004006634T2 (en) | 2008-01-31 |
| EP1664407A1 (en) | 2006-06-07 |
| KR101102655B1 (en) | 2012-01-04 |
| BRPI0413942B1 (en) | 2014-12-16 |
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