US20010052660A1 - Method for reducing dilation balloon cone stiffness - Google Patents

Method for reducing dilation balloon cone stiffness Download PDF

Info

Publication number
US20010052660A1
US20010052660A1 US09/907,989 US90798901A US2001052660A1 US 20010052660 A1 US20010052660 A1 US 20010052660A1 US 90798901 A US90798901 A US 90798901A US 2001052660 A1 US2001052660 A1 US 2001052660A1
Authority
US
United States
Prior art keywords
mold
balloon
parison
stretch
polymeric composition
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
US09/907,989
Other versions
US6458313B2 (en
Inventor
R. Hudgins
Robert Farnan
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boston Scientific Scimed Inc
Original Assignee
Boston Scientific Scimed Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Boston Scientific Scimed Inc filed Critical Boston Scientific Scimed Inc
Priority to US09/907,989 priority Critical patent/US6458313B2/en
Publication of US20010052660A1 publication Critical patent/US20010052660A1/en
Application granted granted Critical
Publication of US6458313B2 publication Critical patent/US6458313B2/en
Assigned to BOSTON SCIENTIFIC SCIMED, INC. reassignment BOSTON SCIENTIFIC SCIMED, INC. CHANGE OF NAME (SEE DOCUMENT FOR DETAILS). Assignors: SCHNEIDER (USA) INC.
Assigned to SCIMED LIFE SYSTEMS, INC. reassignment SCIMED LIFE SYSTEMS, INC. MERGER (SEE DOCUMENT FOR DETAILS). Assignors: BOSTON SCIENTIFIC SCIMED, INC.
Assigned to BOSTON SCIENTIFIC SCIMED, INC. reassignment BOSTON SCIENTIFIC SCIMED, INC. CHANGE OF NAME (SEE DOCUMENT FOR DETAILS). Assignors: SCIMED LIFE SYSTEMS, INC.
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61MDEVICES FOR INTRODUCING MEDIA INTO, OR ONTO, THE BODY; DEVICES FOR TRANSDUCING BODY MEDIA OR FOR TAKING MEDIA FROM THE BODY; DEVICES FOR PRODUCING OR ENDING SLEEP OR STUPOR
    • A61M25/00Catheters; Hollow probes
    • A61M25/10Balloon catheters
    • A61M25/1027Making of balloon catheters
    • A61M25/1029Production methods of the balloon members, e.g. blow-moulding, extruding, deposition or by wrapping a plurality of layers of balloon material around a mandril
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C49/00Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61MDEVICES FOR INTRODUCING MEDIA INTO, OR ONTO, THE BODY; DEVICES FOR TRANSDUCING BODY MEDIA OR FOR TAKING MEDIA FROM THE BODY; DEVICES FOR PRODUCING OR ENDING SLEEP OR STUPOR
    • A61M25/00Catheters; Hollow probes
    • A61M25/10Balloon catheters
    • A61M2025/1043Balloon catheters with special features or adapted for special applications
    • A61M2025/1084Balloon catheters with special features or adapted for special applications having features for increasing the shape stability, the reproducibility or for limiting expansion, e.g. containments, wrapped around fibres, yarns or strands
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/07Preforms or parisons characterised by their configuration
    • B29C2949/079Auxiliary parts or inserts
    • B29C2949/08Preforms made of several individual parts, e.g. by welding or gluing parts together
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/25Solid
    • B29K2105/253Preform
    • B29K2105/258Tubular
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/753Medical equipment; Accessories therefor
    • B29L2031/7542Catheters
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S264/00Plastic and nonmetallic article shaping or treating: processes
    • Y10S264/90Direct application of fluid pressure differential to shape, reshape, i.e. distort, or sustain an article or preform and heat-setting, i.e. crystallizing of stretched or molecularly oriented portion thereof

Definitions

  • the present invention relates to dilatation balloon catheters of the type employed in percutaneous transluminal angioplasty procedures, and more particularly to a method of molding such balloons to reduce their cone stiffness and thereby improve the maneuverability in smaller and more tortious passages of the vascular system.
  • Dilatation balloon catheters are well known for their utility in treating the build-up of plaque and other occlusions in blood vessels.
  • a catheter is used to carry a dilatation balloon to a treatment site, where fluid under pressure is supplied to the balloon, to expand the balloon against a stenotic lesion.
  • the dilatation balloon is affixed to an elongated flexible tubular catheter proximate its distal end region.
  • its working length i.e., its medial section
  • the proximal and distal shafts or stems of the balloon have diameters substantially equal to the diameter of the catheter body.
  • Proximal and distal tapered sections referred to herein as “cones”, join the medial section to the proximal and distal shafts, respectively. Each cone diverges in the direction toward the medial section.
  • Fusion bonds between the proximal and distal balloon shafts and the catheter form a fluid-tight seal to facilitate dilation of the balloon when a fluid under pressure is introduced into it, via an inflation port formed through the wall of the catheter and in fluid communication with the inflation lumen of the catheter.
  • dilatation balloons are their strength and pliability.
  • a higher hoop strength or burst pressure reduces the risk of accidental rupture of the balloon during dilation.
  • Pliability refers to formability into different shapes, rather than elasticity.
  • the dilatation balloon is evacuated, flattened and generally wrapped circumferentially about the catheter in its distal region.
  • Thin, pliable dilatation balloon walls facilitate a tighter wrap that minimizes the combined diameter of the catheter and the balloon during delivery.
  • pliable balloon walls enhance the catheter “trackability” in the distal region, i.e., the ability of the catheter to bend in conforming to the curvature in vascular passages through which it must be routed in reaching a particular treatment site.
  • PET polyethylene terrathalate
  • a tubular parison of PET is heated at least to its second order transition temperature, then drawn to at least triple its original length to axially orient the tubing.
  • the axially expanded tubing is then radially expanded within a heated mold to a diameter about triple the original diameter of the tubing.
  • the form of the mold defines the aforementioned medial section, shafts and cones, and the resulting balloon has a burst pressure greater than 200 psi.
  • Such balloons generally have a gradient in wall thickness along the cones.
  • larger dilatation balloons e.g., 3.0-4.0 mm diameter (expanded) tend to have a wall thickness in the working length in the range of from 0.010 to 0.020 mm.
  • the cones Near the transition of the cones with the working length or medial section, the cones have approximately the same wall thickness.
  • the wall thickness diverges in the direction away from the working length, until the wall thickness near the proximal and distal shafts is in the range of 0.025 to 0.040 mm near the associated shaft or stem.
  • the increased wall thickness near the stems does not contribute to balloon hoop strength, which is determined by the wall thickness along the balloon medial region. Thicker walls near the stems are found to reduce maneuverability of the balloon and catheter through a tortious path. Moreover, the dilatation balloon cannot be as tightly wrapped about the catheter shaft, meaning its delivery profile is larger and limiting the capacity of the catheter and balloon for treating occlusions in smaller blood vessels.
  • U.S. Pat. No. 4,963,133 discloses an alternative approach to forming a PET dilation balloon, in which a length of PET tubing comprising the parison is heated locally at opposite ends and subjected to axial drawing to form two “necked-down” portions, which eventually become the opposite ends of the completed balloon. The necked-down tubing is then simultaneously axially drawn and radially expanded with a gas. The degree to which the tubing ends had been necked-down is said to provide control over the ultimate wall thickness along the walls defining the cones.
  • the use of the Noddin method results in balloons exhibiting a comparatively low burst pressure.
  • a method of making dilatation balloons with reduced cone stiffness comprises the steps of first providing a mold having a cavity including a cylindrical center segment defining a working length of a dilatation balloon body where the center segment is of a predetermined diameter.
  • the mold cavity also includes two opposed end segments, each having an arcuate cone shape tapering from the predetermined diameter of the center segment to a smaller desired balloon shaft diameter.
  • the side edges of the mold are dimensioned to be within about 0.05 in. of the termination point of the arcuate cone at the smaller desired balloon shaft diameter.
  • a tubular polymeric parison of a predetermined diameter and wall thickness is placed with a mold and the parison has the opposed ends thereof extending beyond the side edges of the mold, the opposed ends being clamped in a tensioning fixture.
  • the mold is heated to bring the temperature of the parison near or above the glass transition temperature of the polymeric material comprising the parison.
  • the tensioning fixture is then longitudinally displaced relative to the mold to initially longitudinally stretch the parison by a predetermined amount to introduce a degree of longitudinal orientation and to neck down the tubular parison to a lesser diameter.
  • a second longitudinal stretching operation is initiated and as the tensioning fixture is being moved to achieve a second stretch, a gas is injected into the tubular parison to radially expand the parison to a limit defined by the mold cavity.
  • the wall thickness in the working length of the balloon and in its cones is a function of the degree of longitudinal and radial stretching as well as the gas pressure applied to effect the radial expansion.
  • a third longitudinal stretch is performed by further displacing the tensioning fixtures relative to the mold. It is the third stretch within the above-described mold that is found to remove material from the cone area as the tubing is drawn down to a desired size for a catheter shaft. Removal of material from the cone area renders them more pliable than balloons prepared in the same way but not subjected to longitudinal stretching following the radial expansion of the balloon within the mold. The third stretch also creates an increased number of nucleation sites for crystallization to occur.
  • the temperature of the mold is increased such that the biaxially oriented balloon reaches its crystallizing temperature for effectively locking the molecular structure in place.
  • the mold is cooled below the glass transition temperature of the polymer so that the crystallization structure of the balloon is not lost. Once the mold has sufficiently cooled, it can be opened and the balloon removed.
  • FIG. 1 is a top elevational schematic view of the equipment used in carrying out the method of the present invention
  • FIG. 2 is an enlarged view of one of the jaws of the mold showing the desired profile of the mold cavity used in preparing dilatation balloons having reduced cone stiffness;
  • FIG. 3 is a drawing helpful in understanding the manner in which the mold cavity shape is arrived at.
  • FIG. 4 is a flow chart of the steps employed in preparing dilatation balloons exhibiting reduced cone stiffness.
  • FIG. 1 there is illustrated schematically the apparatus for stretch blow molding dilatation balloons for later assembly on to catheter body stock in the fabrication of dilatation balloon catheters.
  • the mold itself is indicated generally by numeral 10 and comprises first and second mold halves 12 and 14 which when abutting one another at a parting line 16 define an internal mold cavity 18 .
  • the mold halves or jaws can be open or spread apart to allow placement of a tubular parison therein.
  • the opposed ends of the parison 22 and 24 are clamped in a tensioning fixture including clamping jaws 26 which are mounted on rails 28 and 30 for longitudinal movement therealong.
  • the mold 10 incorporates heating elements (not shown) and appropriately positioned temperature sensors for monitoring the mold temperature and sending temperature information back to a microprocessor-based controller for maintaining precise closed-loop control of the temperature of the mold and of the parison contained in it.
  • a suitable linear encoder (not shown) is operatively coupled to the translatable clamping fixtures 26 to provide positional information to the microprocessor-based controller whereby the degree of longitudinal stretch imparted to the parison 20 can be precisely controlled.
  • the equipment for stretch blow molding shown in FIG. 1 also includes a means for introducing a gas 32 , under pressure, into the lumen of the tubular parison 20 and for monitoring and controlling that pressure again, using closed-loop control.
  • the equipment used in carrying out the method of the present invention is altogether conventional.
  • the mold cavity employed is unique, as is the operation whereby the cone segments of the balloons to be formed in it are made to contain less material than in conventional designs.
  • FIG. 2 is a view looking at the interior of one of the jaws 12 or 14 and showing the preferred profile of the mold cavity 18 .
  • the portion of the balloon between the dashed construction lines A-A define the working length of a dilatation balloon formed therein and this portion of the balloon is generally cylindrical.
  • the portion of the mold between construction lines A and B form the cones and, as can be seen from FIG. 2, the cones do not have a linear taper. They are slightly arcuate in the zone between the construction lines A and B.
  • the portion of the mold between the construction lines B and C will ultimately comprise the shaft portion of the balloon formed in the mold cavity 18 .
  • the radiused balloon ends of the mold are designed using the following graphical construction technique:
  • Construction lines 34 above and below the horizontal center line 32 are established to define the desired balloon diameter.
  • Construction lines 36 above and below the center line establish the desired balloon shaft diameters for both the proximal and distal ends.
  • Lines 40 and 40 ′ define the desired working length of the balloon body on either side of the vertical center line 38 .
  • Construction lines 42 are created at the points of intersections of lines 36 and 40 such that lines 42 form a desired angle with respect to line 36 . An angle of 12° is typical. Each of lines 42 should cross the horizontal center line 32 of the mold. Construction lines 42 determine the length of the end of the balloon.
  • Construction line 44 is created at the intersection of lines 36 and 42 . Construction line 44 indicates the boundary for the end of the balloon and the transition to the balloon shaft.
  • Arcs 46 are next constructed. Arc 46 is a three point arc, and it should pass through the intersection of lines 34 and 40 , and lines 42 and 44 . The end point of the arcs 46 should be chosen so that they are tangent to line 34 at the intersection of lines 34 and 40 .
  • Construction lines 42 can now be erased and the portion of the arcs 46 to the left (outside) of construction line 44 can also be erased.
  • Construction line 44 can now be erased and lines 34 trimmed to the left (outside) of line 40 of the left half of the mold.
  • dilatation balloons exhibiting a reduced cone thickness as compared to prior art stretch blow molding operations can be achieved.
  • FIG. 4 there is illustrated a flow chart of the steps used to prepare such improved dilatation balloons.
  • a precut length of a suitable tubular parison is placed in the mold so as to span the mold cavity in the longitudinal direction.
  • the opposed ends of the parison are clamped by the tensioning member 26 .
  • the mold is partially closed about the tubular parison 20 and a gas at a relatively low pressure is introduced into the lumen of the parison and a slight tension is applied to eliminate sagging of the parison when subsequently heated.
  • the mold 10 is heated up to a desired temperature which depends upon the thermoplastic material involved. Generally speaking, the mold is heated to a temperature which is above the glass transition temperature. For PET, the mold may typically be heated to 175°. Once this temperature is reached, the molding operation can be begin.
  • the parison is subjected to a first stretching operation to initiate longitudinal orientation in the plastic.
  • the degree of stretch varies with the tube size (wall thickness) and the tube material.
  • This first stretch which for a PET parison may be in the range of 1 ⁇ 4 in. to 1-1 ⁇ 2 in. at each end thereof, not only results in some longitudinal orientation, but it also necks down the original tubing comprising the parison to a smaller diameter.
  • the mold is completely closed and a second longitudinal stretch is initiated.
  • the balloon is fully inflated by injected an inert, dry gas, e.g., nitrogen, under relatively high pressure into the lumen of the parison to thereby radially expand the parison to fill the mold.
  • the gas pressure depends on tubing thickness and the desired wall thickness of the resulting balloon but will typically be in the range of from 50 psi to about 400 psi.
  • the wall thickness of the resulting balloon is a function of both the longitudinal stretch and the radial stretch employed. There is also an interaction between the pressure and the degree of longitudinal stretch on the thickness of the resulting balloon wall. Generally speaking, the higher the pressure, the less the wall is thinned by the longitudinal stretching.
  • the parison is longitudinally stretched a third time. Because of the arcuate shape of the mold in the zone thereof defining the end cones and because of the short dimension B-C (FIG. 2 and Table I), the third longitudinal stretch is effective to remove material from the cone area of the balloon and to simultaneously draw the tubing down to a desired size thereby providing a thinner shaft portion for later attachment to the catheter body.
  • the first stretch ratio may be in the range of from 1.005 to 2.0, that for the second stretch in the range of from 1.05 to 3.0 and for the third stretch in the range of from 1.1 to 4.0.
  • the temperature of the mold is increased to the crystallizing temperature of the polymer employed to effectively “freeze” the molecular structure resulting from the longitudinal and radial orientation in place.
  • the crystallizing step takes place with the balloon pressurized to the same inflation pressure earlier applied during the balloon inflation step. This helps to ensure that the balloon walls in the working area will remain at the same thickness after the third longitudinal stretch and subsequent crystallizing.
  • the mold can now be cooled down back below the glass transition temperature for the polymer and, following that, the mold can be opened and the clamps released. The portion of the parison outside of the mold is then trimmed off and the balloon is ready to be mounted on a catheter body.
  • the purpose of this test was to evaluate the forces required to push the catheter through the fixture and the ability of the catheter to pass through each of the stents without getting caught by the stent's structure.
  • the average force that was required to pass the conventional catheter through the test fixture was 695.9 grams. This is to be compared with 390.5 grams required to be applied to the catheters having balloons made in accordance with the present invention to traverse the same test fixture. This represents approximately a 44 percent reduction in tracking force.
  • Balloons made in accordance with the three stretch process of the present invention were able to be guided through the stent blocks.
  • the conventional balloons made using the two stretch process were not capable of being pushed through the stents, even with considerable effort.
  • the improved performance of dilatation balloons made in accordance with the present invention is believed to be due to the extraction of material from the cone areas of the balloon taking place during the third stretch.
  • the process of the present invention produces a high degree of molecular orientation, yielding balloons with high strength and simultaneously a reduced balloon wall thickness, balloon cone thickness and balloon shaft diameter. This eliminates the need for subsequent balloon processing following the balloon blowing operation.

Abstract

A method for stretch blow molding dilatation balloons for angioplasty catheters having a significantly reduced cone thickness without sacrifice in burst strength is achieved by utilizing a mold whose cavity includes arcuate walls defining the balloon's end cones and a predetermined minimal distance from the side edges of the mold to the points where the arcuate walls intersect with a smaller diameter balloon stem portion. Utilizing this mold and providing for three longitudinal stretching sequences, one prior to, one during and one following radial expansion of the heated plastic parison, results in an improved balloon exhibiting reduced cone stiffness.

Description

    BACKGROUND OF THE INVENTION
  • I. Field of the Invention [0001]
  • The present invention relates to dilatation balloon catheters of the type employed in percutaneous transluminal angioplasty procedures, and more particularly to a method of molding such balloons to reduce their cone stiffness and thereby improve the maneuverability in smaller and more tortious passages of the vascular system. [0002]
  • II. Discussion of the Prior Art [0003]
  • Dilatation balloon catheters are well known for their utility in treating the build-up of plaque and other occlusions in blood vessels. Typically, a catheter is used to carry a dilatation balloon to a treatment site, where fluid under pressure is supplied to the balloon, to expand the balloon against a stenotic lesion. [0004]
  • The dilatation balloon is affixed to an elongated flexible tubular catheter proximate its distal end region. When the balloon is expanded, its working length, i.e., its medial section, exhibits a diameter substantially larger than that of the catheter body on which it is mounted. The proximal and distal shafts or stems of the balloon have diameters substantially equal to the diameter of the catheter body. Proximal and distal tapered sections, referred to herein as “cones”, join the medial section to the proximal and distal shafts, respectively. Each cone diverges in the direction toward the medial section. Fusion bonds between the proximal and distal balloon shafts and the catheter form a fluid-tight seal to facilitate dilation of the balloon when a fluid under pressure is introduced into it, via an inflation port formed through the wall of the catheter and in fluid communication with the inflation lumen of the catheter. [0005]
  • Along with body tissue compatibility, primary attributes considered in the design and fabrication of dilation balloons are their strength and pliability. A higher hoop strength or burst pressure reduces the risk of accidental rupture of the balloon during dilation. Pliability refers to formability into different shapes, rather than elasticity. In particular, when delivered by the catheter, the dilatation balloon is evacuated, flattened and generally wrapped circumferentially about the catheter in its distal region. Thin, pliable dilatation balloon walls facilitate a tighter wrap that minimizes the combined diameter of the catheter and the balloon during delivery. Furthermore, pliable balloon walls enhance the catheter “trackability” in the distal region, i.e., the ability of the catheter to bend in conforming to the curvature in vascular passages through which it must be routed in reaching a particular treatment site. [0006]
  • One method of forming strong, pliable dilatation balloons of polyethylene terrathalate (PET) is disclosed in U.S. Pat. No. RE. 33,561 (Levy). A tubular parison of PET is heated at least to its second order transition temperature, then drawn to at least triple its original length to axially orient the tubing. The axially expanded tubing is then radially expanded within a heated mold to a diameter about triple the original diameter of the tubing. The form of the mold defines the aforementioned medial section, shafts and cones, and the resulting balloon has a burst pressure greater than 200 psi. [0007]
  • Such balloons generally have a gradient in wall thickness along the cones. In particular, larger dilatation balloons, e.g., 3.0-4.0 mm diameter (expanded) tend to have a wall thickness in the working length in the range of from 0.010 to 0.020 mm. Near the transition of the cones with the working length or medial section, the cones have approximately the same wall thickness. However, the wall thickness diverges in the direction away from the working length, until the wall thickness near the proximal and distal shafts is in the range of 0.025 to 0.040 mm near the associated shaft or stem. [0008]
  • The increased wall thickness near the stems does not contribute to balloon hoop strength, which is determined by the wall thickness along the balloon medial region. Thicker walls near the stems are found to reduce maneuverability of the balloon and catheter through a tortious path. Moreover, the dilatation balloon cannot be as tightly wrapped about the catheter shaft, meaning its delivery profile is larger and limiting the capacity of the catheter and balloon for treating occlusions in smaller blood vessels. [0009]
  • U.S. Pat. No. 4,963,133 (Noddin) discloses an alternative approach to forming a PET dilation balloon, in which a length of PET tubing comprising the parison is heated locally at opposite ends and subjected to axial drawing to form two “necked-down” portions, which eventually become the opposite ends of the completed balloon. The necked-down tubing is then simultaneously axially drawn and radially expanded with a gas. The degree to which the tubing ends had been necked-down is said to provide control over the ultimate wall thickness along the walls defining the cones. However, it is believed that the use of the Noddin method results in balloons exhibiting a comparatively low burst pressure. [0010]
  • Copending application Ser. No. 08/582,371, filed Jan. 11, 1996, describes a method for reducing cone stiffness by using a laser to ablate and remove polymeric material from the cone areas after the balloon is blown. It is preferable that the desired result be obtained during the balloon molding operations obviating the need for additional post molding operations. [0011]
  • Therefore, it is an object of the present invention to provide a method for stretch blow molding dilatation balloon having a high burst pressure and hoop strength, but with reduced material mass in the balloon cones, thus reducing cone stiffness and improving the trackability, crossing profile, stenosis recross and balloon retrieval, via a guiding catheter. [0012]
  • SUMMARY OF THE INVENTION
  • To achieve these and other objects of the invention, there is provided a method of making dilatation balloons with reduced cone stiffness. The method comprises the steps of first providing a mold having a cavity including a cylindrical center segment defining a working length of a dilatation balloon body where the center segment is of a predetermined diameter. The mold cavity also includes two opposed end segments, each having an arcuate cone shape tapering from the predetermined diameter of the center segment to a smaller desired balloon shaft diameter. The side edges of the mold are dimensioned to be within about 0.05 in. of the termination point of the arcuate cone at the smaller desired balloon shaft diameter. [0013]
  • Next, a tubular polymeric parison of a predetermined diameter and wall thickness is placed with a mold and the parison has the opposed ends thereof extending beyond the side edges of the mold, the opposed ends being clamped in a tensioning fixture. The mold is heated to bring the temperature of the parison near or above the glass transition temperature of the polymeric material comprising the parison. The tensioning fixture is then longitudinally displaced relative to the mold to initially longitudinally stretch the parison by a predetermined amount to introduce a degree of longitudinal orientation and to neck down the tubular parison to a lesser diameter. [0014]
  • Following this initial longitudinal stretch, a second longitudinal stretching operation is initiated and as the tensioning fixture is being moved to achieve a second stretch, a gas is injected into the tubular parison to radially expand the parison to a limit defined by the mold cavity. At this point, the wall thickness in the working length of the balloon and in its cones is a function of the degree of longitudinal and radial stretching as well as the gas pressure applied to effect the radial expansion. [0015]
  • Following inflation of the balloon within the mold, a third longitudinal stretch is performed by further displacing the tensioning fixtures relative to the mold. It is the third stretch within the above-described mold that is found to remove material from the cone area as the tubing is drawn down to a desired size for a catheter shaft. Removal of material from the cone area renders them more pliable than balloons prepared in the same way but not subjected to longitudinal stretching following the radial expansion of the balloon within the mold. The third stretch also creates an increased number of nucleation sites for crystallization to occur. [0016]
  • After the third stretch operation is terminated, the temperature of the mold is increased such that the biaxially oriented balloon reaches its crystallizing temperature for effectively locking the molecular structure in place. [0017]
  • Following crystallization, the mold is cooled below the glass transition temperature of the polymer so that the crystallization structure of the balloon is not lost. Once the mold has sufficiently cooled, it can be opened and the balloon removed.[0018]
  • DESCRIPTION OF THE DRAWINGS
  • FIG. 1 is a top elevational schematic view of the equipment used in carrying out the method of the present invention; [0019]
  • FIG. 2 is an enlarged view of one of the jaws of the mold showing the desired profile of the mold cavity used in preparing dilatation balloons having reduced cone stiffness; [0020]
  • FIG. 3 is a drawing helpful in understanding the manner in which the mold cavity shape is arrived at; and [0021]
  • FIG. 4 is a flow chart of the steps employed in preparing dilatation balloons exhibiting reduced cone stiffness.[0022]
  • DESCRIPTION OF THE PREFERRED EMBODIMENT
  • Referring to FIG. 1, there is illustrated schematically the apparatus for stretch blow molding dilatation balloons for later assembly on to catheter body stock in the fabrication of dilatation balloon catheters. The mold itself is indicated generally by [0023] numeral 10 and comprises first and second mold halves 12 and 14 which when abutting one another at a parting line 16 define an internal mold cavity 18. The mold halves or jaws can be open or spread apart to allow placement of a tubular parison therein. The opposed ends of the parison 22 and 24 are clamped in a tensioning fixture including clamping jaws 26 which are mounted on rails 28 and 30 for longitudinal movement therealong.
  • As those skilled in the art appreciate, the [0024] mold 10 incorporates heating elements (not shown) and appropriately positioned temperature sensors for monitoring the mold temperature and sending temperature information back to a microprocessor-based controller for maintaining precise closed-loop control of the temperature of the mold and of the parison contained in it. Likewise, a suitable linear encoder (not shown) is operatively coupled to the translatable clamping fixtures 26 to provide positional information to the microprocessor-based controller whereby the degree of longitudinal stretch imparted to the parison 20 can be precisely controlled.
  • The equipment for stretch blow molding shown in FIG. 1 also includes a means for introducing a [0025] gas 32, under pressure, into the lumen of the tubular parison 20 and for monitoring and controlling that pressure again, using closed-loop control.
  • Except for the [0026] mold cavity 18 formed in the mold halves 12 and 14, the equipment used in carrying out the method of the present invention is altogether conventional. The mold cavity employed is unique, as is the operation whereby the cone segments of the balloons to be formed in it are made to contain less material than in conventional designs.
  • FIG. 2 is a view looking at the interior of one of the [0027] jaws 12 or 14 and showing the preferred profile of the mold cavity 18.
  • The portion of the balloon between the dashed construction lines A-A define the working length of a dilatation balloon formed therein and this portion of the balloon is generally cylindrical. The portion of the mold between construction lines A and B form the cones and, as can be seen from FIG. 2, the cones do not have a linear taper. They are slightly arcuate in the zone between the construction lines A and B. The portion of the mold between the construction lines B and C will ultimately comprise the shaft portion of the balloon formed in the [0028] mold cavity 18.
  • The following table sets out typical mold dimensions in stretch blow-molding a dilatation balloon having a working length of 20 mm and an expanded diameter of 4.0 mm. These dimensions are illustrative only because the various dimensions change depending upon the size of the balloon to be formed. [0029]
    TABLE I
    Dimension Magnitude (Inches)
    A-A .763
    B-B 1.532
    C-C 1.557
    B-C .025
    A-B .372
    R1 .832
    R2 1.010
  • With reference to FIG. 3, for any size balloon diameter, the radiused balloon ends of the mold are designed using the following graphical construction technique: [0030]
  • 1. The [0031] horizontal centerline 32 for the mold is first established.
  • 2. [0032] Construction lines 34 above and below the horizontal center line 32 are established to define the desired balloon diameter.
  • 3. [0033] Construction lines 36 above and below the center line establish the desired balloon shaft diameters for both the proximal and distal ends.
  • 4. The [0034] vertical center line 38 for the mold is set.
  • 5. [0035] Lines 40 and 40′ define the desired working length of the balloon body on either side of the vertical center line 38.
  • 6. [0036] Construction lines 42 are created at the points of intersections of lines 36 and 40 such that lines 42 form a desired angle with respect to line 36. An angle of 12° is typical. Each of lines 42 should cross the horizontal center line 32 of the mold. Construction lines 42 determine the length of the end of the balloon.
  • 7. [0037] Construction line 44 is created at the intersection of lines 36 and 42. Construction line 44 indicates the boundary for the end of the balloon and the transition to the balloon shaft.
  • 8. [0038] Arcs 46 are next constructed. Arc 46 is a three point arc, and it should pass through the intersection of lines 34 and 40, and lines 42 and 44. The end point of the arcs 46 should be chosen so that they are tangent to line 34 at the intersection of lines 34 and 40.
  • 9. [0039] Construction lines 42 can now be erased and the portion of the arcs 46 to the left (outside) of construction line 44 can also be erased.
  • 10. Displace [0040] construction line 44 to the left by 0.025 in. to 0.25 in. establish the left end of the mold which is depicted in FIG. 13 by construction line 48.
  • 11. The [0041] lines 36 to the right (inside) of construction line 44 and to the left (outside) of construction line 48 are trimmed to form the short land of the mold.
  • 12. [0042] Construction line 44 can now be erased and lines 34 trimmed to the left (outside) of line 40 of the left half of the mold.
  • 13. The foregoing construction steps are then repeated for the right side of the mold to form the other balloon end. [0043]
  • As will be explained in further detail hereinbelow, by providing the arcuate cone segments and the short cylindrical shaft segments (dimension B-C in Table I), it is possible to remove polymeric material from the cone portions of the mold by providing a third stretch to the parison following inflation of the parison to achieve radial orientation. [0044]
  • Using the mold created using the techniques outlined above in the apparatus of FIG. 1, dilatation balloons exhibiting a reduced cone thickness as compared to prior art stretch blow molding operations can be achieved. Referring to FIG. 4, there is illustrated a flow chart of the steps used to prepare such improved dilatation balloons. In carrying out the method, a precut length of a suitable tubular parison is placed in the mold so as to span the mold cavity in the longitudinal direction. The opposed ends of the parison are clamped by the tensioning [0045] member 26. The mold is partially closed about the tubular parison 20 and a gas at a relatively low pressure is introduced into the lumen of the parison and a slight tension is applied to eliminate sagging of the parison when subsequently heated.
  • Following this initial setup and pretensioning, the [0046] mold 10 is heated up to a desired temperature which depends upon the thermoplastic material involved. Generally speaking, the mold is heated to a temperature which is above the glass transition temperature. For PET, the mold may typically be heated to 175°. Once this temperature is reached, the molding operation can be begin.
  • The parison is subjected to a first stretching operation to initiate longitudinal orientation in the plastic. The degree of stretch varies with the tube size (wall thickness) and the tube material. This first stretch which for a PET parison may be in the range of ¼ in. to 1-½ in. at each end thereof, not only results in some longitudinal orientation, but it also necks down the original tubing comprising the parison to a smaller diameter. [0047]
  • After the prestretch (first stretch), the mold is completely closed and a second longitudinal stretch is initiated. During the time that the second stretch is occurring, the balloon is fully inflated by injected an inert, dry gas, e.g., nitrogen, under relatively high pressure into the lumen of the parison to thereby radially expand the parison to fill the mold. The gas pressure depends on tubing thickness and the desired wall thickness of the resulting balloon but will typically be in the range of from 50 psi to about 400 psi. The wall thickness of the resulting balloon is a function of both the longitudinal stretch and the radial stretch employed. There is also an interaction between the pressure and the degree of longitudinal stretch on the thickness of the resulting balloon wall. Generally speaking, the higher the pressure, the less the wall is thinned by the longitudinal stretching. [0048]
  • With continued reference to the flow chart of FIG. 4, following inflation of the balloon and while the balloon is still subjected to the pressure of the inflation gas, the parison is longitudinally stretched a third time. Because of the arcuate shape of the mold in the zone thereof defining the end cones and because of the short dimension B-C (FIG. 2 and Table I), the third longitudinal stretch is effective to remove material from the cone area of the balloon and to simultaneously draw the tubing down to a desired size thereby providing a thinner shaft portion for later attachment to the catheter body. [0049]
  • Defining the stretch ratio as the ratio of the length after the stretch divided by the length prior to the stretch, for a PET polymer the first stretch ratio may be in the range of from 1.005 to 2.0, that for the second stretch in the range of from 1.05 to 3.0 and for the third stretch in the range of from 1.1 to 4.0. [0050]
  • Following the third stretch operation, the temperature of the mold is increased to the crystallizing temperature of the polymer employed to effectively “freeze” the molecular structure resulting from the longitudinal and radial orientation in place. The crystallizing step takes place with the balloon pressurized to the same inflation pressure earlier applied during the balloon inflation step. This helps to ensure that the balloon walls in the working area will remain at the same thickness after the third longitudinal stretch and subsequent crystallizing. [0051]
  • The mold can now be cooled down back below the glass transition temperature for the polymer and, following that, the mold can be opened and the clamps released. The portion of the parison outside of the mold is then trimmed off and the balloon is ready to be mounted on a catheter body. [0052]
  • Comparative tests were run on balloons prepared in accordance with the method of FIG. 4 when using a mold having a profile like that of FIG. 2 with balloons fabricated using a prior art “two stretch” molding process having all of the steps of FIG. 4 except the third stretch following balloon inflation and in a mold that had linear (rather than arcuate) cone profiles. These specific parameters that were compared were derived by advancing a plurality of dilatation catheters having balloons manufactured in accordance with the method of the present invention and balloons manufactured in accordance with the described prior art through a test fixture. The test fixture had a tortuous path and located at differing spots within the tortuous path were a Palmez-Schatz stent and a Wallstent® Endoprosthesis. The purpose of this test was to evaluate the forces required to push the catheter through the fixture and the ability of the catheter to pass through each of the stents without getting caught by the stent's structure. The average force that was required to pass the conventional catheter through the test fixture was 695.9 grams. This is to be compared with 390.5 grams required to be applied to the catheters having balloons made in accordance with the present invention to traverse the same test fixture. This represents approximately a 44 percent reduction in tracking force. [0053]
  • A further test was conducted to assess the force required to re-cross a stenosis following balloon inflation. Balloons made in accordance with the method of the present invention in the mold cavity made as described herein showed an approximate decrease of 18 percent in the stenosis recross force when compared to balloons molded in the conventional “two stretch” process. [0054]
  • Testing further revealed that the balloons molded with the “three stretch” process of the present invention required the lowest force to withdraw the balloon catheter through a guiding catheter. The force to withdraw the balloons prepared in the three stretch process was about 28% less than the force necessary to withdraw balloons made using the prior art two stretch process. [0055]
  • Balloons made in accordance with the three stretch process of the present invention were able to be guided through the stent blocks. The conventional balloons made using the two stretch process were not capable of being pushed through the stents, even with considerable effort. [0056]
  • The improved performance of dilatation balloons made in accordance with the present invention is believed to be due to the extraction of material from the cone areas of the balloon taking place during the third stretch. The process of the present invention produces a high degree of molecular orientation, yielding balloons with high strength and simultaneously a reduced balloon wall thickness, balloon cone thickness and balloon shaft diameter. This eliminates the need for subsequent balloon processing following the balloon blowing operation.[0057]

Claims (11)

What is claimed is:
1. A method of making dilatation balloons with reduced cone stiffness, comprising the steps of:
(a) providing a mold having a cavity therein including a center section of a predetermined diameter defining a working length for a balloon to be formed therein and opposed end cone segments, each defined by an arcuate wall tangent to a wall defining the generally cylindrical center section and terminating in a cylindrical end segment corresponding to a desired shaft size for the balloon to be formed therein, the mold having opposed side edges spaced less than 0.25 inch from a point of intersection of the arcuate wall and the cylindrical end segment;
(b) placing a tubular parison of a predetermined polymeric composition across the mold cavity, the tubular parison having opposed ends extending outwardly from the opposed side edges of the mold;
(c) clamping the opposed ends of the tubular parison in longitudinally displaceable tensioning fixtures;
(d) heating the mold to a temperature above the glass transition temperature of the polymeric composition of the parison;
(e) longitudinally displacing the tensioning fixture relative to the mold a first time to effect a first predetermined stretch ratio;
(f) subsequently longitudinally displacing the tensioning fixture relative to the mold a second time to effect a second predetermined stretch ratio while simultaneously injecting a gas, under pressure, into the tubular parison to radially expand the parison against the walls defining the mold cavity;
(g) further longitudinally displacing the tensioning fixture relative to the mold a third time to effect removing a third stretch ratio and polymeric material from the end segments of the mold;
(h) heating the mold to the crystallizing temperature of the polymeric composition;
(i) cooling the mold to a temperature below the glass transition temperature of the polymeric composition; and
(j) removing the resulting balloon from the mold.
2. The method as in
claim 1
and further including a step of pretensioning the tubular parison prior to step (d).
3. The method as in
claim 1
wherein the polymeric composition comprises PET.
4. The method as in
claim 3
wherein the first predetermined stretch ratio is in a range of from 1.005 to 2.0.
5. The method as in
claim 3
wherein the second predetermined stretch ratio is in a range of from 1.05 to 3.0.
6. The method as in
claim 3
wherein the third stretch ratio is in a range of from 1.1 to 4.0.
7. The method as in
claim 1
wherein the tubular parison is a co-extrusion of Nylon 12 over PET.
8. The method as in
claim 1
wherein the gas injected is at a pressure in a range of from 50 psi to 400 psi.
9. A method of fabricating a dilatation balloon in a stretch blow molding operation comprising the steps of:
(a) providing a mold having a cavity formed therein defining a desired shape configuration of a dilatation balloon to be formed therein, the balloon including a cylindrical central section and opposed generally spherical end sections tapering to a reduced diameter balloon shaft segment;
(b) placing a tubular parison of a polymeric composition having a predetermined diameter and wall thickness across the mold with opposed ends of the parison extending outward beyond the side edges of the mold;
(c) clamping the opposed ends of the parison in a tensioning fixture;
(d) heating the mold to a temperature above the glass transition temperature of the polymeric composition;
(e) simultaneously inflating and longitudinally displacing the tensioning fixture relative to the mold to thereby stretch the parison to form a balloon within the mold cavity;
(f) subjecting the balloon of step (d) to a further longitudinal stretch within the heated mold to draw polymeric material from the generally conical end sections without appreciable thinning of the central section thereof;
(g) heating the mold to a crystallizing temperature of the polymeric composition;
(h) cooling the mold back down below the glass transition temperature of the polymeric composition; and
(i) removing the balloon from the mold.
10. The method as in
claim 9
wherein the mold cavity includes arcuate boundaries defining the opposed conical end sections.
11. The method as in
claim 10
wherein the arcuate boundaries are tangent at one end to a segment defining the central section of the balloon and intersect the segment defining the balloon shaft at another end.
US09/907,989 1998-07-09 2001-07-18 Method for reducing dilation balloon cone stiffness Expired - Lifetime US6458313B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US09/907,989 US6458313B2 (en) 1998-07-09 2001-07-18 Method for reducing dilation balloon cone stiffness

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/112,532 US6287506B1 (en) 1998-07-09 1998-07-09 Method for reducing dilation balloon cone stiffness
US09/907,989 US6458313B2 (en) 1998-07-09 2001-07-18 Method for reducing dilation balloon cone stiffness

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
US09/112,532 Continuation US6287506B1 (en) 1998-07-09 1998-07-09 Method for reducing dilation balloon cone stiffness

Publications (2)

Publication Number Publication Date
US20010052660A1 true US20010052660A1 (en) 2001-12-20
US6458313B2 US6458313B2 (en) 2002-10-01

Family

ID=22344403

Family Applications (2)

Application Number Title Priority Date Filing Date
US09/112,532 Expired - Lifetime US6287506B1 (en) 1998-07-09 1998-07-09 Method for reducing dilation balloon cone stiffness
US09/907,989 Expired - Lifetime US6458313B2 (en) 1998-07-09 2001-07-18 Method for reducing dilation balloon cone stiffness

Family Applications Before (1)

Application Number Title Priority Date Filing Date
US09/112,532 Expired - Lifetime US6287506B1 (en) 1998-07-09 1998-07-09 Method for reducing dilation balloon cone stiffness

Country Status (6)

Country Link
US (2) US6287506B1 (en)
EP (1) EP1100573B1 (en)
JP (1) JP4201983B2 (en)
CA (1) CA2336741C (en)
DE (1) DE69920474T2 (en)
WO (1) WO2000002613A1 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090133817A1 (en) * 2006-06-19 2009-05-28 Patrick Sabaria Stent manufacturing methods
US7654264B2 (en) 2006-07-18 2010-02-02 Nellcor Puritan Bennett Llc Medical tube including an inflatable cuff having a notched collar
DE10305799B4 (en) * 2003-02-12 2012-12-27 Henkel Ag & Co. Kgaa Process for the preparation of a blow-molded detergent body
US20210291428A1 (en) * 2020-03-23 2021-09-23 Steer Medical Inc. Method and system for stretching a tubular material over a mandrel
WO2024015125A1 (en) * 2021-08-07 2024-01-18 Blockwise Engineering Llc Parison former

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6048338A (en) 1997-10-15 2000-04-11 Scimed Life Systems, Inc. Catheter with spiral cut transition member
US6193738B1 (en) * 1998-05-11 2001-02-27 Scimed Life Systems, Inc. Balloon cones and waists thinning methodology
US6287506B1 (en) 1998-07-09 2001-09-11 Schneider (Usa) Inc. Method for reducing dilation balloon cone stiffness
US6863861B1 (en) * 2000-09-28 2005-03-08 Boston Scientific Scimed, Inc. Process for forming a medical device balloon
US6835189B2 (en) * 2002-10-15 2004-12-28 Scimed Life Systems, Inc. Controlled deployment balloon
US7306616B2 (en) * 2003-05-05 2007-12-11 Boston Scientific Scimed, Inc. Balloon catheter and method of making same
US7727442B2 (en) * 2003-07-10 2010-06-01 Boston Scientific Scimed, Inc. Medical device tubing with discrete orientation regions
US20050137619A1 (en) * 2003-12-19 2005-06-23 Scott Schewe Molds and related methods and articles
US7264458B2 (en) * 2004-01-07 2007-09-04 Boston Scientific Scimed, Inc. Process and apparatus for forming medical device balloons
IL161554A0 (en) 2004-04-22 2004-09-27 Gali Tech Ltd Catheter
US7947207B2 (en) 2005-04-12 2011-05-24 Abbott Cardiovascular Systems Inc. Method for retaining a vascular stent on a catheter
WO2006138741A1 (en) 2005-06-17 2006-12-28 Abbott Laboratories Method of reducing rigidity of angioplasty balloon sections
US9439662B2 (en) 2005-07-05 2016-09-13 Angioslide Ltd. Balloon catheter
EP1904139B1 (en) * 2005-07-05 2010-09-08 Angioslide Ltd. Balloon catheter
US8556851B2 (en) 2005-07-05 2013-10-15 Angioslide Ltd. Balloon catheter
AU2006287610A1 (en) * 2005-09-06 2007-03-15 Nantero, Inc. Nanotube fabric-based sensor systems and methods of making same
JP4920247B2 (en) * 2005-11-18 2012-04-18 株式会社カネカ Manufacturing method of stent delivery system
US20070205539A1 (en) * 2006-03-03 2007-09-06 Boston Scientific Scimed, Inc. Balloon mold design
JP5023802B2 (en) * 2007-05-15 2012-09-12 株式会社カネカ Medical balloon and stent delivery system and method for manufacturing the same
US8313687B2 (en) * 2007-09-20 2012-11-20 Kimberly-Clark Worldwide, Inc. Method of making an improved balloon cuff tracheostomy tube
US20110125158A1 (en) 2008-05-01 2011-05-26 Ashish Dhar Diwan Systems, methods and apparatuses for formation and insertion of tissue prostheses
US8827951B2 (en) 2008-07-02 2014-09-09 Doron Besser Balloon catheter system and methods of use thereof
DE102008040914A1 (en) * 2008-08-01 2010-02-04 Biotronik Vi Patent Ag Balloon catheter and process for its preparation
US9675780B2 (en) 2010-01-19 2017-06-13 Angioslide Ltd. Balloon catheter system and methods of making and use thereof
JP2016503330A (en) 2012-12-04 2016-02-04 アンジオスライド リミテッド Balloon catheter and method of using the same
CN103231530B (en) * 2013-04-12 2016-01-27 张向阳 A kind of full-automatic balloon heat pressing forming machines
EP3142738B1 (en) * 2014-05-16 2020-11-04 Boston Scientific Scimed Inc. High pressure low cost multilayer balloon catheter
US9539692B2 (en) 2014-08-15 2017-01-10 Covidien Lp Material removal from balloon cone
CN112848246B (en) * 2021-01-25 2023-02-03 宜宾天亿新材料科技有限公司 Forming method of biaxial orientation plastic pipe
CN114407383A (en) * 2022-01-28 2022-04-29 海南一剂堂生物科技有限公司 Balloon preparation method of balloon dilatation catheter

Family Cites Families (58)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2273021B1 (en) 1974-05-31 1977-03-11 Ato Chimie
US4154244A (en) 1977-11-21 1979-05-15 Baxter Travenol Laboratories, Inc. Balloon-type catheter
US4254774A (en) 1979-02-14 1981-03-10 The United States Of America As Represented By The Department Of Health, Education And Welfare Balloon catheter and technique for the manufacture thereof
FR2466478B2 (en) 1979-10-02 1986-03-14 Ato Chimie PROCESS FOR THE PREPARATION OF ELASTOMERIC ALIPHATIC COPOLYETHERESTERAMIDES
US4675361A (en) 1980-02-29 1987-06-23 Thoratec Laboratories Corp. Polymer systems suitable for blood-contacting surfaces of a biomedical device, and methods for forming
US4385635A (en) 1980-04-25 1983-05-31 Ruiz Oscar F Angiographic catheter with soft tip end
US4413989A (en) 1980-09-08 1983-11-08 Angiomedics Corporation Expandable occlusion apparatus
WO1984001513A1 (en) 1982-10-08 1984-04-26 David Hardcastle Balloon catheter and process for the manufacture thereof
US4563181A (en) 1983-02-18 1986-01-07 Mallinckrodt, Inc. Fused flexible tip catheter
USRE33561E (en) 1983-07-05 1991-03-26 E. I. Du Pont De Nemours And Company Balloon and manufacture thereof
USRE32983E (en) 1983-07-05 1989-07-11 E. I. Du Pont De Nemours And Company Balloon and manufacture thereof
US4490421A (en) 1983-07-05 1984-12-25 E. I. Du Pont De Nemours And Company Balloon and manufacture thereof
US4786556A (en) 1986-03-24 1988-11-22 Becton, Dickinson And Company Polymeric articles having enhanced antithrombogenic activity
US4886506A (en) 1986-12-23 1989-12-12 Baxter Travenol Laboratories, Inc. Soft tip catheter
EP0274411A3 (en) 1987-01-09 1988-11-30 C.R. Bard, Inc. Thin wall high strength balloon and method of manufacture
US5250069A (en) 1987-02-27 1993-10-05 Terumo Kabushiki Kaisha Catheter equipped with expansible member and production method thereof
US4963133A (en) 1987-12-31 1990-10-16 Pharmacia Deltec, Inc. Catheter attachment system
US4917667A (en) 1988-02-11 1990-04-17 Retroperfusion Systems, Inc. Retroperfusion balloon catheter and method
US4952357A (en) 1988-08-08 1990-08-28 Scimed Life Systems, Inc. Method of making a polyimide balloon catheter
US4898591A (en) 1988-08-09 1990-02-06 Mallinckrodt, Inc. Nylon-PEBA copolymer catheter
US4950239A (en) 1988-08-09 1990-08-21 Worldwide Medical Plastics Inc. Angioplasty balloons and balloon catheters
US4950257A (en) 1988-09-15 1990-08-21 Mallinckrodt, Inc. Catheter introducer with flexible tip
US4906244A (en) 1988-10-04 1990-03-06 Cordis Corporation Balloons for medical devices and fabrication thereof
US4938676A (en) * 1988-10-04 1990-07-03 Cordis Corporation Apparatus for manufacturing balloons for medical devices
US5304197A (en) 1988-10-04 1994-04-19 Cordis Corporation Balloons for medical devices and fabrication thereof
US5335675A (en) 1988-11-15 1994-08-09 Family Health International Stress-softened elastomeric films, articles, and method and apparatus for making such films and articles
JP3560031B2 (en) * 1989-07-24 2004-09-02 コーディス・コーポレイション Balloon for medical device and molding thereof
FR2651681B1 (en) 1989-09-11 1991-12-13 Medicorp Research Lab CATHETER.
ES2043289T3 (en) 1989-09-25 1993-12-16 Schneider Usa Inc THE EXTRUSION OF MULTIPLE LAYERS AS A PROCEDURE FOR MAKING ANGIOPLASTY BALLS.
US5087394A (en) 1989-11-09 1992-02-11 Scimed Life Systems, Inc. Method for forming an inflatable balloon for use in a catheter
US5478320A (en) 1989-11-29 1995-12-26 Cordis Corporation Puncture resistant balloon catheter and method of manufacturing
US5290306A (en) 1989-11-29 1994-03-01 Cordis Corporation Puncture resistant balloon catheter
JP2528011B2 (en) 1989-12-20 1996-08-28 テルモ株式会社 Catheter
JP3339683B2 (en) 1990-11-09 2002-10-28 ボストン サイエンティフィック コーポレイション Medical catheter balloon
JP2555298B2 (en) 1990-11-10 1996-11-20 テルモ株式会社 CATHETER BALLOON, CATHETER BALLOON MANUFACTURING METHOD, AND BALLOON CATHETER
US5295978A (en) 1990-12-28 1994-03-22 Union Carbide Chemicals & Plastics Technology Corporation Biocompatible hydrophilic complexes and process for preparation and use
US5195969A (en) 1991-04-26 1993-03-23 Boston Scientific Corporation Co-extruded medical balloons and catheter using such balloons
EP0513459A1 (en) 1991-05-16 1992-11-19 Terumo Kabushiki Kaisha Indwelling catheter
EP0972535B1 (en) 1991-09-12 2005-12-28 Advanced Cardiovascular Systems, Inc. Inflatable member having elastic expansion with limited range
JP3053029B2 (en) 1991-10-08 2000-06-19 テルモ株式会社 Vascular dilatation catheter balloon
US5304134A (en) 1992-01-17 1994-04-19 Danforth Biomedical, Inc. Lubricious yet bondable catheter channel sleeve for over-the-wire catheters
US5344400A (en) 1992-04-06 1994-09-06 Terumo Kabushiki Kaisha Balloon catheters containing molded polyarylenesulfide material
DE69211678T2 (en) 1992-04-21 1996-11-07 Cordis Corp Polyether hose for medical devices
US5281677A (en) 1992-09-03 1994-01-25 Becton, Dickinson And Company Thermoplastic polyurethane blends
US5348538A (en) 1992-09-29 1994-09-20 Scimed Life Systems, Inc. Shrinking balloon catheter having nonlinear or hybrid compliance curve
US5500180A (en) 1992-09-30 1996-03-19 C. R. Bard, Inc. Method of making a distensible dilatation balloon using a block copolymer
US5512051A (en) 1993-02-16 1996-04-30 Boston Scientific Corporation Slip-layered catheter balloon
US5300048A (en) 1993-05-12 1994-04-05 Sabin Corporation Flexible, highly radiopaque plastic material catheter
WO1995022367A1 (en) * 1994-02-17 1995-08-24 Scimed Life Systems, Inc. Process improvements for preparing catheter balloons
US5556383A (en) 1994-03-02 1996-09-17 Scimed Lifesystems, Inc. Block copolymer elastomer catheter balloons
US5587125A (en) * 1994-08-15 1996-12-24 Schneider (Usa) Inc. Non-coextrusion method of making multi-layer angioplasty balloons
WO1996012516A1 (en) 1994-10-19 1996-05-02 Advanced Cardiovascular Systems, Inc. High strength dilatation balloons
EP0707942B1 (en) * 1994-10-20 2000-03-01 Interventional Technologies Inc Method for manufacturing a polymeric material with enhanced mechanical properties
NL9500468A (en) 1995-03-08 1996-10-01 Cordis Europ Balloon catheter and method of making it.
US5645789A (en) * 1995-07-20 1997-07-08 Navius Corporation Distensible pet balloon and method of manufacture
JP3742696B2 (en) * 1995-10-11 2006-02-08 テルモ株式会社 Catheter balloon and balloon catheter and vasodilator catheter
US5948345A (en) * 1998-01-05 1999-09-07 Medtronic, Inc. Method for making medical balloon catheter
US6287506B1 (en) 1998-07-09 2001-09-11 Schneider (Usa) Inc. Method for reducing dilation balloon cone stiffness

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10305799B4 (en) * 2003-02-12 2012-12-27 Henkel Ag & Co. Kgaa Process for the preparation of a blow-molded detergent body
US20090133817A1 (en) * 2006-06-19 2009-05-28 Patrick Sabaria Stent manufacturing methods
US7654264B2 (en) 2006-07-18 2010-02-02 Nellcor Puritan Bennett Llc Medical tube including an inflatable cuff having a notched collar
US8096299B2 (en) 2006-07-18 2012-01-17 Nellcor Puritan Bennett Llc Medical tube including an inflatable cuff having a notched collar
US20210291428A1 (en) * 2020-03-23 2021-09-23 Steer Medical Inc. Method and system for stretching a tubular material over a mandrel
US11724438B2 (en) * 2020-03-23 2023-08-15 Steer Medical Inc. Method and system for stretching a tubular material, over a mandrel
WO2024015125A1 (en) * 2021-08-07 2024-01-18 Blockwise Engineering Llc Parison former

Also Published As

Publication number Publication date
JP2002520099A (en) 2002-07-09
JP4201983B2 (en) 2008-12-24
EP1100573B1 (en) 2004-09-22
CA2336741C (en) 2008-01-08
WO2000002613A1 (en) 2000-01-20
US6458313B2 (en) 2002-10-01
US6287506B1 (en) 2001-09-11
DE69920474T2 (en) 2005-10-13
CA2336741A1 (en) 2000-01-20
DE69920474D1 (en) 2004-10-28
EP1100573A1 (en) 2001-05-23

Similar Documents

Publication Publication Date Title
US6287506B1 (en) Method for reducing dilation balloon cone stiffness
US5807520A (en) Method of balloon formation by cold drawing/necking
US10245352B2 (en) Catheter shaft having high strength and flexibility
US6328710B1 (en) Process improvements for preparing catheter balloons
US4963313A (en) Balloon catheter
US6863861B1 (en) Process for forming a medical device balloon
US6176698B1 (en) Thin cone balloons through a unique mold design
US6719774B1 (en) Method for forming low profile balloon and low profile balloon for use with a catheter
US20020171180A1 (en) Method of making a catheter balloon

Legal Events

Date Code Title Description
STCF Information on status: patent grant

Free format text: PATENTED CASE

FPAY Fee payment

Year of fee payment: 4

AS Assignment

Owner name: BOSTON SCIENTIFIC SCIMED, INC., MINNESOTA

Free format text: CHANGE OF NAME;ASSIGNOR:SCHNEIDER (USA) INC.;REEL/FRAME:018454/0858

Effective date: 19990427

Owner name: BOSTON SCIENTIFIC SCIMED, INC., MINNESOTA

Free format text: CHANGE OF NAME;ASSIGNOR:SCIMED LIFE SYSTEMS, INC.;REEL/FRAME:018454/0866

Effective date: 20050101

Owner name: SCIMED LIFE SYSTEMS, INC., MINNESOTA

Free format text: MERGER;ASSIGNOR:BOSTON SCIENTIFIC SCIMED, INC.;REEL/FRAME:018454/0834

Effective date: 20050101

FPAY Fee payment

Year of fee payment: 8

FPAY Fee payment

Year of fee payment: 12