Example 1
Succinic acid-1,4-butanediol-malic acid copolyester (Tepha lot 180333) with weight average molecular weight of 184 kDa, Tm=115° C., (melt flow rate (MFR) at 190° C./2.16 kgf of 5 g/10 min) was dried under vacuum overnight to less than 0.01% (w/w) water. Dried pellets of the polymer were fed into an extruder barrel of an AJA (Alex James Associates, Greer, South Carolina) ¾ single screw extruder (24:1 L:D, 3:1 compression) equipped with a Zenith type metering pump (0.16 cc/rev) and a die with a single hole spinneret (0.026″, 2:1 L:D) under a blanket of nitrogen. The 4 heating zones of the extruder were set at 75° C., 165° C., 180° C. and 180° C. The extruder was fitted with a quench bath filled with water at 35° C. and set up with an air gap of 10 mm between the bottom of the spinneret and the surface of the water. Two 2-roll godets were positioned after the quench bath, followed by two sets of longitudinal hot convection chamber/2-roll godet combination. The temperatures of the hot convection chambers were set between 60° to 80° C., followed by 2-roll godets then a horizontal winder. Pellets of the copolyester were allowed to enter the heated extruder barrel, molten polymer passed through the barrel, entered a heated block followed by a metering pump then a single hole spinneret. The block, metering pump and the spinneret die were maintained at a constant temperature, preferably 180° C. Pump discharge pressure was kept below 1500 psi by controlling the temperatures and the speed of the metering pump. The resulting spun extrudate filament was free from all melt irregularities. The extrudate was quenched in a water bath, drawn through longitudinal ovens and wound on a horizontal tension controlled Sahm winder. The results of 3 trials with in-line orientation and shown in Table 1, together with the result of a fourth trial where the fiber was not oriented in-line, but rather off-line and 10 days after it had been extruded. From inspection of Table 1, it will be evident that the conditions used to prepare the monofilament fiber resulted in fiber with a tensile strength in the range of 434-518 MPa.
Example 2
Succinic acid-1,4-butanediol-malic acid copolyester (Tepha lot 180333) with weight average molecular weight of 184 kDa, PD=2.83, Tm=115° C., (MFR 190° C., 2.16 kg, 5 g/10 min) was dried under vacuum overnight to less than 0.01% (w/w) water. Dried pellets of the polymer were fed under a blanket of nitrogen into the extruder barrel of a 2½″ American Kuhne single screw extruder (30:1 L:D, 3:1 compression) equipped with a Zenith type metering pump model HPB917, a die with 0.5 mm-8 hole spinneret and 8 heat zones. The 8 heating zones of the extruder were set between 40° C. and 200° C. The extruder was fitted with a quench bath filled with water at 35°-70° C. and set up with an air gap of 10 mm between the bottom of the spinneret and the surface of the water. Two 5-roll godets were positioned after the quench bath, followed by three sets of hot conduction chambers fed by godets in order to orient the fiber in multiple stages. The temperatures of the hot chambers were set up between 50° to 90° C. temperature. Another godet was positioned after the last chamber, and then a multi-position Sahm winder. The results from three trials are shown in Table 2. In comparison to the results shown in Table 1, the use of multi-stage incremental orientation of the fiber and conductive chambers instead of standard conventional non-liquid chambers resulted in monofilament fiber with substantially higher tensile strengths of 779-883 MPa.
Example 3
Succinic acid-1,4-butanediol-malic acid copolyester (Tepha lot 180333) with weight average molecular weight of 184 kDa, PD=2.83, Tm=115° C., (melt flow rate (MFR) at 190° C./2.16 kgf of 5 g/10 min), was dried under vacuum overnight to less than 0.01% (w/w) water. Dried pellets of the polymer were fed into an extruder barrel of an AJA (Alex James Associates, Greer, South Carolina) ¾″ single screw extruder (24:1 L:D). The extrusion barrel contained 4 heating zones, a metering pump and a spin pack assembly. The pellets were gravity fed into a chilled feeder section and introduced into the extruder with temperature profile set as follows: Chimney 40° C.-100° C., Spinneret 170° C.±30° C., Pump 170° C.±30° C., Block 170° C.±30° C., Zone 4 160° C.±40° C., Zone 3 150° C.±40° C., Zone 2 120° C.±50° C., Zone 1 30° C.-40° C., Feed Zone: Ambient temperature. The heated and homogenized melted resin from the extruder was fed into a heated metering pump (melt pump), and from the melt pump the extruded resin was fed into the heated block and the spinneret assembly. The spinneret had 30 holes with a capillary diameter of 0.200 millimeters and a L/D ratio of 2:1. (The spinneret may also be configured in other alternative manners. For example, the spinneret can be configured with capillary diameters from 0.150 to 0.300 millimeters (6 mil to 12 mil) and 15, 120 and 240 holes, as well as higher and lower diameters and numbers of holes.) Processing temperature profile ranges from 35° C. to 250° C. were used with pressures ranging from 200 to 5,000 psi in the barrel and 200 to 5,000 psi in the spin pack. As the molten filaments exited the spin pack they passed through a heated chimney collar that was 6-12 inches long and ranged in temperature from 40° C. to 100° C., and then through an air quench box. The spin pack was suspended vertically above a yarn take-up roll at a distance sufficient to allow crystallization of the molten filaments and application of spin finish lubricant. A spin finish solution of 25% polyethylene 25 glycol 400 (PEG400) in water was used to hold the filaments together to form a yarn bundle. The speed of the yarn take-up rolls (typically 3-18 meters per minute) was set in proportion to the flow rate of the molten filament to control the denier of the as spun yarn bundle. The as spun yarn bundle was then conveyed to a Lessona winder for offline later orientation or conveyed to a take-up roll for inline orientation on a series of cold and heated godet pairs and separator rolls. The spin finish can be reactivated by rewetting the yarn bundle with pure water, and the yarn drawn at ratios from 5 to 14× and temperatures ranging from 50° C. to 90° C. The tenacity and denier of the multifilament yarn produced is shown in Table 3.
Example 4
Oriented yarn produced according to Example 3 and with properties shown in Table 3 was braided using 8 and 16 carrier Steeger braiding equipment to form the braid constructions shown in Table 4. The mechanical properties of the high strength braided sutures, determined according to USP 24, are also shown in Table 4. The examples include a braid formed as a tape (shown as the last example in Table 4.
Example 5
Monofilament fiber (USP suture size 5/0) prepared according to the method of Example 2 was processed into knitted mesh according to the following procedure. Monofilament fibers from 49 spools were mounted on a creel, aligned side by side and pulled under uniform tension to the upper surface of a “kiss” 10″ roller. The “kiss” roller was spun while semi-immersed in a bath filled with a 10% solution of TWEEN® 20 lubricant. The TWEEN® 20 lubricant was deposited on the surface of the sheet of monofilament fibers. Following the application of TWEEN® 20, the sheet of fiber was passed into a comb guide and then wound on a warp beam. A warp is a large wide cylinder onto which individual fibers are wound in parallel to provide a sheet of fibers. Next, warp beams were converted into a finished mesh fabric by means of interlocking knit loops. Eight warp beams were mounted in parallel onto tricot machine let-offs and fed into the knitting elements at a constant rate determined by the ‘runner length’. Each individual monofilament fiber from each beam was fed through a series of 20 dynamic tension elements down into the knitting ‘guides’. Each fiber was passed through a single guide, which was fixed to a guide bar. The guide bar directed the fibers around the needles forming the mesh fabric structure. The mesh fabric was then pulled off the needles by the take down rollers at a constant rate of speed determined by the fabric ‘quality’. The mesh fabric was then taken up and wound onto a roll and scored ultrasonically with water, heat set in hot water, and then washed with a 70% aqueous ethanol solution. The knitted mesh produced with monofilament fiber from Example 2 had the following properties (as shown in Table 11 at time 0): burst strength of 22.668 kgf, thickness of 0.683 mm, and Taber Stiffness of 0.116.
Example 6
Spools of multifilament fiber prepared according to the method of Example 3 were processed into knitted multifilament mesh using the method described in Example 5.
Example 12
The in vitro degradation rate of an implantable mesh prepared from oriented monofilament fibers of succinic acid-1,4-butanediol-malic acid copolyester (prepared as described in Example 5) was studied by incubation of the mesh in phosphate buffered saline. The buffer solution contained 137 mM NaCl, 2.7 mM KCl, 9.8 mM phosphate and 0.05 wt % sodium azide and had pH 7.4 at 25° C. The prepared buffer solution was filtered through a 0.45 um filter (VWR Product # 10040-470) prior to use. Mesh samples were sterilized by exposure to ethylene oxide gas. Samples (2×2 in.) were placed in sterile containers covered in buffer solution and incubated in a shaker incubator at 50 rpm and at a temperature of 37° C. Buffer media was monitored monthly and changed if the pH was outside of the targeted value 7.4±0.2. At prescribed time points, the samples were removed from the buffer and rinsed with deionized water to remove buffer salts. The samples were then tested for mechanical properties and weight average molecular weight retention of the polymer by gel permeation chromatography (as further described in Example 15). The in vitro degradation data is shown in Table 5.
Example 13
The degradation rate of an implantable suture prepared from oriented monofilament fibers of succinic acid-1,4-butanediol-malic acid copolyester in vitro was studied by incubation of the suture in phosphate buffered saline. The initial properties of the suture are shown in Table 6, line 1 (t=0). The buffer solution contained 137 mM NaCl, 2.7 mM KCl, 9.8 mM phosphate and 0.05 wt % sodium azide and had pH 7.4 at 25° C. The prepared buffer solution was filtered through a 0.45 um filter (VWR Product # 10040-470) prior to use. Suture samples were sterilized by exposure to ethylene oxide gas. Samples (12 in. length) were placed in sterile containers covered in buffer solution and incubated in a shaker incubator at 50 rpm and at a temperature of 37° C. Buffer media was monitored monthly and changed if the pH was outside of the targeted value 7.4±0.2. At prescribed time points, the samples were removed from the buffer and rinsed with deionized water to remove buffer salts. The samples were then tested for mechanical properties and weight average molecular weight (Mw) retention of the polymer by gel permeation chromatography (as further described in Example 15). The in vitro degradation data is shown in Table 6.
Example 15
The properties of a monofilament knitted mesh prepared from a copolymer of 1,4-butanediol and succinic acid units (the “PBS” mesh), as described in Example 5, were compared to a commercial mesh, the “GalaFLEX mesh (Galatea Surgical, Lexington, Massachussets)” prepared from knitting of poly-4-hydroxybutyrate monofilament in an in vivo implantation study in rabbits. The weight average molecular weight of the PBS mesh fibers prior to implantation was 173 kDa. The PBS and GalaFLEX meshes were implanted in the dorsal, subcutaneous tissue of New Zealand White rabbits to evaluate the local tissue reaction, the degree of tissue in-growth and the changes in mechanical properties of the meshes over time in vivo. Six (6) female New Zealand White (NZW) rabbits were implanted with 6 mechanical (4×4 cm), 1 histological (2×2 cm), and 1 scanning electron microscopy (SEM) (2×2 cm) test articles per animal.
Prior to implantation, the rabbits (weighing at least 3.5 kg at implantation) were anesthetized by an intramuscular injection, followed by maintenance under isoflurane. Following anesthesia, the animals were injected subcutaneously with an analgesic. The surgical sites were prepared for implantation. An incision was made through the skin and the skin was resected laterally by blunt dissection to create a pocket. Three individual mechanical samples (4×4 cm) and 1 histo/SEM sample (2×2 cm) were implanted on each side of each animal, for a total of 8 specimens per animal. The specimens were implanted by placing the mesh flat along the back of the animal without folding or rolling and fixated with a Prolene suture at each corner. The skin was closed and a bandage was applied. The animals were returned to their respective cages, monitored for recovery from the anesthetic, and then monitored daily for general health.
At 4 and 12 weeks, three rabbits were euthanized from each group. The skin was reflected, the subcutaneous tissues were examined and the area around each implant was dissected free. The implanted meshes were recovered by dissection from the surrounding tissue. The explants were processed for histological, biomechanical and polymer testing. At each time point, half of the 4×4 cm implanted meshes (n=9) were tested for mechanical properties including the in-grown tissue. The other samples (n=9), were designated for mesh-only analyses and were tested following collagenase digestion to remove ingrown tissue and evaluate the residual strength of the residual polymeric scaffold. In this way, the mechanical properties of the mesh alone could be measured and compared to that of the combination of mesh and tissue in the composite.
For the mesh-only samples, the in-grown tissue was removed from the explanted samples using enzymatic digestion with collagenase. Previous testing demonstrated no impact of the collagenase enzyme on the mesh mechanical properties or Mw properties. Individual explanted mesh specimens were placed in a 50 mL Falcon tube containing 25 mL collagenase (type I) solution (1.0 mg/mL) in TESCA buffer (50 mM TES, 2 mM calcium chloride, 10 mM NaN3, pH 7.4, sterile filtered). The tube was placed in a shaker (50 rpm) and incubated at 37° C. overnight (˜17 h) to digest and remove tissue attached to the mesh specimen. After the incubation was complete, the specimens were removed from the tubes, residual tissue was manually removed from the explant taking care not to damage the mesh, and the meshes were rinsed with distilled water followed by 70% ethanol. Mesh specimens were blotted dry using a lint-free wipe.
Samples were tested for dimensions, relative stiffness (Taber tester), burst strength and evaluated for surface morphology via SEM. Comparison was made to non-implanted (T0) articles (n=9/group). Polymer degradation was further evaluated by Gel Permeation Chromatography (GPC). The host tissue response and degree of tissue remodeling were evaluated histologically
Example 17
A mesh suture was prepared using triaxial braiding from high strength monofilament PBS fibers. Spooled monofilament fibers of succinic acid-1,4-butanediol-malic acid copolyester extruded and oriented as described in Example 2 were unspooled and wound on braider bobbins. The bobbins were then loaded onto Herzog 4, 8, 16 and 24 carrier braiders. Additional spooled monofilament fiber was used to provide axial fiber in the mesh suture. The monofilament fibers were unspooled and threaded through the hollow axles of the horn gears, and all bobbin and axial fiber ends were pulled through the braiding ring to form the fell point. The braiders' bobbins were allowed to move along the braiding track, and the braid helix angle was adjusted to 15 degrees at 1 to 2 Picks Per Inch (PPI). The constructions (number of carriers and axial fibers used to prepare the hollow braids) and properties of the triaxial braided mesh sutures prepared with 100 μm, 150 μm, and 200 μm P4HB monofilament fiber are shown in Tables 14, 15 and 16. The tables show the outside (OD) and inside (ID) diameters of the mesh suture hollow braids. The width and thickness of the hollow braided mesh sutures were measured after the hollow braids had been squashed flat.