US3557795A - Suture provided with wound healing coating - Google Patents

Abstract

Sutures coated with a wound-healing, nontoxic metal, such as aluminum or magnesium, are described as are methods for coating sutures with such material.

Description

United States Patent Inventor Winfred Hirsch Plainview, N.Y.

Appl No. 738,146

Filed June 19, 1968 Patented Jan. 26, 1971 Assignee Edward Week & Company, Inc.

Long Island City, N.Y.

a corporation of Delaware Continuation-impart of application Ser. No. 531,768, Mar. 4, 1966, now abandoned.

SUTURE PROVIDED WITH WOUND HEALINGCOATING 14 Claims, 7 Drawing Figs.

U.S.Cl 128/3355,

161/175: 117/130, 117/160 Int. Cl A611 17/00 Field ofSearch 128/3355;

OTHER REFERENCES Kraissl Surgery Gyne. & Obstet. May 1936 pp. 417- 423 1283355 Primary ExaminerDalton L. Truluck Attorney-Joseph Weingarten ABSTRACT: Sutures coated with a wound-healing, nontoxic metal, such as aluminum or magnesium, are described as are methods for coating sutures with such material.

SUTURE PROVIDED WITH WOUND HEALING COATING CROSS REFERENCES This is a continuation-in-part of application Ser. No. 531,768 filed Mar. 4, 1966, for SUTURES AND LIGA- TURES ADAPTED FOR THE ACCELERATION OF WOUND HEALING, and now abandoned.

BACKGROUND OF THE INVENTION This invention relates to absorbable and nonabsorbable sutures for closing wounds. In order for a material to be satisfactory as a suture, it must be nontoxic and noncarcinogenic, have tissue acceptance and be flexible yet strong enough to meet United States Pharmacopeia (USP) standards even when tied in a surgical knot. Naturally, it must also be sterilizable, be able to hold surgical knots without slipping and have only a limited stretchability so that under tension it does not exceed the stretch prescribed by USP standards. In addition, it is desirable to have the suture add something to the compendium of surgical materials already available for use as sutures. Finally, it is desirable to have the suture somehow contribute to the healing of the wound in which it is used.

These last characteristics are the ones to which this invention pertains. It has recently been discovered that pure aluminum (i.e., aluminum that is 99.9999 percent pure) accelerates wound healing by an electrochemical reaction between the metal and the surrounding tissues. The same effect is also achieved with pure magnesium, although magnesiums wound-healing ability is not as great. Monofilament sutures of either of these materials are not practical, however, because they are too brittle and cannot meet the knot-pull tensile strength requirements of the USP specifications for monofilament sutures. In the second place, since both aluminum and magnesium react with the surrounding tissues, they undergo a chemical transformation and dissipate during the wound-healing process and thus weaken the suture and lessen its ability to keep the wound closed.

SUMMARY OF THE INVENTION 1 have discovered that both these undesirable characteristics can be overcome by providing a suture which is coated with a wound-healing metal such as aluminum or mag nesium. The core os such a suture is preferably Dacron, nylon, polyester fiber or stainless steel, though any other suitable suture material such as cotton, silk, catgut (plain or chromicized), collagen (plain or chromicized) or any other organic, inorganic, metallic or synthetic material which lends itself to usage as a suture can also be used. The core can be a standard monofilament suture or it can be a twisted or braided suture made of any of these materials. Using aluminum as a coating not only helps heal the wound faster, it gives the advantage that the strength of the suture is not lessened as the aluminum dissipates in the wound. On an absorbable suture the aluminum or magnesium coating also acts as a temporary barrier between the tissue cells and the absorbable material, thus increasing the sutures useful life in the wound. The coating should be as pure as possible because its wound-healing ability diminishes with the number and amount of alloying materials in the metal as well as with the number and amount of contaminants it contains. Neither of these materials should comprise over 5 percent impurities. Aluminum that is 99.9999 percent pure is preferred, though if it contains 0.76 percent magnesium and less than 0.0009 percent of any other component, the coating is quite satisfactory. Oxidation of the coating also reduces its activity and its wound-healing ability. To give a suture the desired wound-healing characteristic, the coating should be of the appropriate thickness. A principal advantage of using either of these materials, and this is particularly true of aluminum, is that it enables the fibrotic reaction in wound healing to proceed at a controlled, faster-thamordinary rate. Thus, by controlling the thickness of the coating, it is possible to insure that when it is healed there will be no residual fibrotic reaction in the wound due to the presence of the coating material. I have found that a thickness from between about 6 to 40 microns is useful in achieving this result with the range of about ID to 20 microns being preferred in order that the reactive coating material be substantially completely dissipated from the suture core by the time the wound is healed.

The coating process includes cleaning the suture core by any known chemical or other process. When Dacron, nylon, silk or certain other suture materials are used, it is also necessary to render them dimensionally stable by thermosetting them in a known manner at a temperature which is at least 10 F. higher than any temperature at which they are likely to be subjected later. Then all suture materials are bombarded over their entire surface with negatively charged particles under high vacuum with the result that they become negatively charged. This should be done in a thin atmosphere of pure nitrogen or one of the inert gases to prevent oxidation. By then vaporizing the aluminum, the vapor is attracted to and condensed on the suture material with a strong bond. Vaporization of the aluminum can be accomplished by any convenient known technique, such as by heating tungsten filaments over which strips of aluminum are twisted or hung, or by using a laser beam or by induction heating. If the filament method is used, the vaporization should take place at as low a temperature as possible to avoid vaporizing tungsten particles which would also be deposited on the suture material and which are toxic to the tissues. When sufficient aluminum has been vaporized and deposited on the core material, the vacuum is broken and the coating process is over. I have also discovered that (whether the core material is bombarded before deposition or not) all the aluminum or magnesium must be deposited on the core in a single session without breaking the vacuum. Once the vacuum is broken, even if more wound-healing metal is later deposited on the suture using a second vacuum, for some reason the first or undercoating material appears to have lost most of its wound-healing or reactive ability. Thus, the sutures wound-healing ability will depend almost entirely on the thickness of its second or last coating. To improve the adherence of the wound-healing coating on metallic sutures, it is useful to minutely etch the surface of the suture before subjecting it to the bombardment treatment.

Further, other and additional aspects of the invention will appear from the following description, the novel features of which will be particularly pointed out in the appended claims.

BRIEF DESCRIPTION OF THE DRAWING VIEWS FIG. 1 is a schematic perspective view of a vacuum chamber which can be used to coat a suture in accordance with the in vention.

FIG. 2 is a vertical elevation in cross section of the chamber of FIG. 1.

FIG. 3 is a perspective view of a portion of the tungsten heating element frame shown in FIG. 2.

FIG. 4 is a perspective view of a portion of the rotatable suture rack frame shown in FIG. 2.

FIG. 5 is a vertical elevation view in cross section of another kind of vacuum chamber usable in coating the suture core.

FIG. 6 is a plan view of the vacuum chamber of FIG. 5.

FIG. 7 is a cross section view of a coated Dacron suture according to the invention.

DETAILED DESCRIPTION Referring now more particularly to the drawings, the process of coating Dacron core material with aluminum is begun by thermosetting or dimensionally stabilizing the material in a known manner by bringing it up to a temperature of between 300--360 F. under a tension which can vary from 5-25 percent of its breaking tension depending on the residual stretch to be left in the material. Certain other materials, such as nylon or silk, must also be thermally set in this manner using other known temperatures and tensions.

Then the suture must be cleaned to remove all reactive constituents or substances from its surface. This can be done using standard ultrasonic cleaning techniques for sutures or by subjecting it to multiple washings in neutral nonreactive clean (USP) water. Stainless steel sutures are usually cleaned in toluene. When the material is clean, it is placed in avacuum chamber 10 having oneopen line 12 connected to a source of vacuum (not shown) and another open line M connected to a source of nitrogen (not shown). In operation the chamber is preferably drawn down to a high vacuum of about 4 X lO microns and is then filled with nitrogen after which the vacuum is again drawn down to about 4 X l microns. Lower vacuums down to 3X 10" microns can also be used, but the higher the vacuum the better the deposition and the lower the vaporizing temperature will be. By refilling the chamber this way, it is purged of air and all its contaminants and contaminating influences and is filled with a thin atmosphere which inhibits oxidation so the deposition process can be carried out effectively and easily. When a stainless steel suture is being coated, it is helpful if it can be heated while the deposition is taking place because I have found that such heating improves the bond between the coating and the suture.

In carrying out the process, with all suture materials it is important that to the extent possible the entire surface of the material be exposed not only to the conditioning step in which the surface is treated to insure adequate bonding of the coating but also that it face directly and be exposed on all sides to the source of the metal being deposited on it. This can be accomplished by rotating thematerial in'the chamber 10. As seen in FIGS. 14,chamber 10 includes a fixedcylinder 16 separated from thecylindrical wall 18 of the chamber by a plurality ofmounts 20. Insidecylinder 16 is a cage 17 which can be rotated by agear 22 rigidly connected to it about its central axis by means of a collar 24. A spider bearing26 rotatably supports the collar along the axis of the cylinder. Cage 17 includes anidler gear 19 at one end and a drivengear 21 at its opposite end and the two gears are connected to each other by a plurality ofrods 23.Gear 21 is releasably fixed to collar 24. Apinion gear 28 powered byshaft 30 driven by amotor 32 drives gear 22 to rotate collar 24 and thusgear 21.Motor 32 is shown schematically outside the chamber in FIG. 1.

Surrounding cage 17 there is aframe assembly 34 for carrying and rotating the Dacron or other material to be coated. Inside the cage is anonrotating framework 36 for carrying and vaporizing the aluminum to be deposited on the material.

Assembly 34 preferably includes four rack units each of which includes twoframes 38 separated from each other but rigidly mounted coaxially on arotatable shaft 40. Each frame has a plurality offingers 41 protruding from its edges to enable the Dacron 42 to be strung back and forth between opposing fingers on the other frame on the shaft. The racks are independent but lie parallel and 90 apart from each other in a pair of rims 4 1 in which each shaft is rotatabiy mounted (see FIG. 2). Mounted on opposite ends of each shaft 4!) beyondrims 44 is agear 46 which meshes either withidler gear 19 or drivengear 21 so that when the cage rotates eachrack unit 35 rotates about itsshaft 40 in the same direction. At the same time thewhole assembly 34 rotates about the central axis of the cylinder. Thus, when the cage rotates, each of theracks 35 moves around the cylinder in addition to rotating about the axis of itsshaft 40.

The aluminum is supplied to the Dacron or other material on these racks by aheater framework 36 mounted inside cage 17 between acup 48 at one end and a mounting block 50 at the other.Framework 36 includes fourheater racks 52 each of which includes four or more tungsten filaments on which are placed or twisted the strips ofaluminum 62 whichare to be vaporized. These racks are mounted parallel each other and 90 part on a pair offrames 54 at opposite ends of each rack and frames 54 are rigidly mounted coaxially on ashaft 56. One end of the shaft is mounted incup 48 and the other end extends throughgears 21 and 22 and collar 24 to mounting block 50in the rear ofthe chamber. The end ol'thc shaft in the mounting block has arectangular cross section 58 to prevent the shaft and the framework from rotating.Cup 48 is mounted coaxial with assembly 341 on one side ofgear 19 which has one end ofastub shaft 64 fixedly mounted on its opposite side. The other end ofstub shaft 64 is journaled in aspider 68, the radial tips of which are releasably attached to the forward end ofcylinder 16. In operation, cage 17 rotates at one speed, suture racks 35rotate around theirshafts 40 drivingassembly 34 around the cylinder in the same direction but at a slower speed than the cage. Heater racks 52,framework 36 andspider 68 remain stationary. In this way all the surfaces of the Dacron or other material are brought close to the source of the aluminum vapor.

Adoor 72 is provided to close the open front end of the chamber and is equipped with conventional means for sealing the chamber against air leaks when a vacuum is drawn. A conventional spark gap unit 74 is also provided in the chamber to detect the presence of substantial amounts of free metal in the chamber during deposition of the metal. The chamber also includes a knowndevice 76 for bombarding the material mounted onv racks 35 with negatively charged particles such as electrons. The device is shown schematically in FIG. 2 and is connected to a control (not shown) outside the chamber bywires 70. Preferably the device produces a stream of electrons accelerated through a potential of 25,000-30,000 volts for at least 5 minutes, while theracks 35 are rotating to insure that all the surfaces of the Dacron have been bombarded and become negatively charged.

After the Dacron has undergone this conditioning treatment, the aluminum deposition begins. In the device shown in FIGS. 1-4 in the drawings, this is accomplished by energizing one of the tungsten filaments on eachrack 52 at a time. Under a vacuum, aluminum vaporizes into positively charged particles at temperatures ranging from 800 to 1500 F. The precise temperature depends on the purity of the aluminum and the extent of the vacuum. Electrical controls (not shown) are provided outside the chamber to insure that the temperature of the filaments doesnt get too hot. As soon as all the aluminum that will vaporize from these filaments at the desired temperature has beengiven off, the filaments are turned off. The existence of this condition is detected by observing the spark gap unit to see when the residual amount of free aluminum in the atmosphere within the chamber is not sufficiently concentrated to conduct electricity across the gap of the unit..When this occurs, the condition has been reached, and after the first set has been turned off, another set of filaments is energized to vaporize additional aluminum. This sequence is followed again and again until all the filaments in the chamber have been energized and no more aluminum can be vaporized at the desired temperature. The aluminum particles are initially attracted to the suture because of the potential difference between them; and while the deposition process is going on, the cage, racks, gears, frames andassemblies are rotating to expose as much of thesurface of the suture materi al as possible and to get it as close as possible to the vaporized aluminum source.Wiring 78, shown schematically in FIGS. 1 and 2, connects the filaments with the controls (not shown) and permits them to be selectively energized.

When the deposition is finished, the vacuum is released and the coated suture is removed from the chamber by removingcylinder 16 along guide tracks 80 (see FIG. I).

As seen in FIGS. 5 and 6, the Dacron or other suitable suture core material need not be wound between fingers on spaced apartframes, as in FIGS. 2 and 4, but can be stored on spools IEO which can be stacked one on top of the other and fixed to arotating shaft 112 driven by a motor H4 in the base E02 of a different kind of vacuum chamber. This type of chamber comprises a metal bell jar me which is releasably scalable to the base which has a vacuum line I04 and a nitrogen-purgingline 106 opening within the jar. The chamber also includes a known electron bombardment device 1M3 shown schematically, a known spark gap unit 121 and a supply of aluminum for vaporization as in the first type chamber. Though the aluminum supply shown in FlGS. 5 and 6 comprisesstrips 122 of aluminum placed or twisted ontungsten filaments 124, it should be realized that the supply could comprise an aluminum bar which is vaporizable by a laser beam or by induction heating. The essential difference between this type chamber and that shown in FIGS. 1-4 is that here there has to be at least one takeup spool and one feed spool in the chamber. As shown in FIG. 6, there are two stacks of each type,reference character 110a referring to the feed spools and 1 10b to the takeup spools. Thesuture material 116 is threaded fromspools 110a over and through a set of three idler rollers 118 to spools 11Gb in such a way that all surfaces of the material can be directly exposed to the source of vaporized aluminum by rotating the spools so as to transfer the material from one spool to another. Then, by rotating the spools, all the suture material may be bombarded and coated with aluminum. The finished product has a cross section like that shown in FIG. 7 in which 126 is the suture core and 128 the coating.

If desired, a nonabsorbable coated suture according to this invention can be left in the body as a supporting element even after the coating has been dissipated. lt is still useful in strengthening the tissues around the location of the healed wound even after the coating is gone.

it will be understood that various changes in the details, materials, steps and arrangements of parts, which have been herein described and illustrated in order to explain the nature of the invention, may be made by those skilled in the art within the principle and scope of the invention, as expressed in the claims.

I claim:

1. A surgical suture useful for accelerating the healing of wounds by beneficial fibrotic reaction with the tissues surrounding such wounds, said suture comprising:

an elongated core of surgical suture material; and

a coating on said core of a different material, said coating extending over a substantial portion of the surface of said core, said coating material being selected from the group consisting of substantially pure aluminum and substantially pure magnesium.

2. A suture material according to claim 1 wherein said coating has a thickness of between about 6 and 40 microns.

3. A suture material according to claim 2 wherein said coating comprises aluminum.

4. A suture material according to claim 2 wherein said coating comprises magnesium.

5. A suture component according to claim 3 wherein said suture component comprises a nonabsorbable suture.

6. A suture material according to claim 5 wherein said nonabsorbable suture component comprises Dacron and said aluminum coating has a thickness of between 10 to 20 microns.

7. A suture material according to claim 2 wherein said suture component comprises an absorbable suture and said coaring comprises aluminum.

8. A suture material according to claim 5 wherein said nonabsorbable suture component comprises stainless steel.

9. A surgical material for use in a patient as ligatures and as sutures for closing wounds, said surgical material comprising:

an elongated core of surgical suture material; and

a coating on said core of a different material, said coating extending over a substantial portion of the surface of said core, said coating material being selected from the group consisting of substantially pure aluminum and substantially pure magnesium; said coating being adapted to beneficially chemically react with the tissues in the vicinity of said surgical material, said coating being of such thickness as to increase the rate of fibrosis in said tissues at a controlled rate, said coating being dissipated by said chemical reaction and the residual fibrotic reaction due to said coating materials ceasing when said coating has been completely dissipated.

10. The combination according to claim 9 wherein said coating comprises pure aluminum.

11. The combination according to claim 10 wherein said suture component comprises a nonabsorbable material which can be left as a supporting element for the wound tissues after said coating has been completely dissipated.

12. The combination according to claim 11 wherein said aluminum coating has a thickness of between about 6 to 40 microns.

13. A suture component and coating according to claim 7 wherein said suture component is resorbable in the wound and said coating protects said component against resorption until said coating has been dissipated.

14. A suture component and coating according to claim 11 wherein said coating comprises pure aluminum between about l0 to 20 microns in thickness.

Claims (13)

1. 2. A suture material according to claim 1 wherein said coating has a thickness of between about 6 and 40 microns.
2. 3. A suture material according to claim 2 wherein said coating comprises aluminum.
3. 4. A suture material according to claim 2 wherein said coating comprises magnesium.
4. 5. A suture component according to claim 3 wherein said suture component comprises a nonabsorbable suture.
5. 6. A suture material according to claim 5 wherein said nonabsorbable suture component comprises Dacron and said aluminum coating has a thickness of between 10 to 20 microns.
6. 7. A suture material according to claim 2 wherein said suture component comprises an absorbable suture and said coating comprises aluminum.
7. 8. A suture material according to claim 5 wherein said nonabsorbable suture component comprises stainless steel.
8. 9. A surgical material for use in a patient as ligatures and as sutures for closing wounds, said surgical material comprising: an elongated core of surgical suture material; and a coating on said core of a different material, said coating extending over a substantial portion of the surface of said core, said coating material being selected from the group consisting of substantially pure aluminum and substantially pure magnesium; said coating being adapted to beneficially chemically react with the tissues in the vicinity of said surgical material, said coating being of such thickness as to increase the rate of fibrosis in said tissues at a controlled rate, said coating being dissipated by said chemical reaction and the residual fibrotic reaction due to said coating materials ceasing when said coating has been completely dissipated.
9. 10. The combination according to claim 9 wherein said coating comprises pure aluminum.
10. 11. The combination according to claim 10 wherein said suture component comprises a nonabsorbable material which can be left as a supporting element for the wound tissues after said coating has been completely dissipated.
11. 12. The combination according to claim 11 wherein said aluminum coating has a thickness of between about 6 to 40 microns.
12. 13. A suture component and coating according to claim 7 wherein said suture component is resorbable in the wound and said coating protects said component against resorption until said coating has been dissipated.
13. 14. A suture component and coating according to claim 11 wherein said coating comprises pure aluminum between about 10 to 20 microns in thickness.

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