CA2162927C - Non-oxidizing polymeric medical implant - Google Patents

Non-oxidizing polymeric medical implant Download PDF

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Publication number
CA2162927C
CA2162927C CA002162927A CA2162927A CA2162927C CA 2162927 C CA2162927 C CA 2162927C CA 002162927 A CA002162927 A CA 002162927A CA 2162927 A CA2162927 A CA 2162927A CA 2162927 C CA2162927 C CA 2162927C
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Prior art keywords
oxygen
atmosphere
implant
set forth
free radicals
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French (fr)
Inventor
Deh-Chuan Sun
Casper F. Stark
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Howmedica Osteonics Corp
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Stryker Technologies Corp
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    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61LMETHODS OR APPARATUS FOR STERILISING MATERIALS OR OBJECTS IN GENERAL; DISINFECTION, STERILISATION OR DEODORISATION OF AIR; CHEMICAL ASPECTS OF BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES; MATERIALS FOR BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES
    • A61L2/00Methods or apparatus for disinfecting or sterilising materials or objects other than foodstuffs or contact lenses; Accessories therefor
    • A61L2/02Methods or apparatus for disinfecting or sterilising materials or objects other than foodstuffs or contact lenses; Accessories therefor using physical phenomena
    • A61L2/08Radiation
    • A61L2/081Gamma radiation
    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61LMETHODS OR APPARATUS FOR STERILISING MATERIALS OR OBJECTS IN GENERAL; DISINFECTION, STERILISATION OR DEODORISATION OF AIR; CHEMICAL ASPECTS OF BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES; MATERIALS FOR BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES
    • A61L15/00Chemical aspects of, or use of materials for, bandages, dressings or absorbent pads
    • A61L15/16Bandages, dressings or absorbent pads for physiological fluids such as urine or blood, e.g. sanitary towels, tampons
    • A61L15/42Use of materials characterised by their function or physical properties
    • A61L15/60Liquid-swellable gel-forming materials, e.g. super-absorbents
    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61LMETHODS OR APPARATUS FOR STERILISING MATERIALS OR OBJECTS IN GENERAL; DISINFECTION, STERILISATION OR DEODORISATION OF AIR; CHEMICAL ASPECTS OF BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES; MATERIALS FOR BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES
    • A61L2/00Methods or apparatus for disinfecting or sterilising materials or objects other than foodstuffs or contact lenses; Accessories therefor
    • A61L2/02Methods or apparatus for disinfecting or sterilising materials or objects other than foodstuffs or contact lenses; Accessories therefor using physical phenomena
    • A61L2/08Radiation
    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61LMETHODS OR APPARATUS FOR STERILISING MATERIALS OR OBJECTS IN GENERAL; DISINFECTION, STERILISATION OR DEODORISATION OF AIR; CHEMICAL ASPECTS OF BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES; MATERIALS FOR BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES
    • A61L2/00Methods or apparatus for disinfecting or sterilising materials or objects other than foodstuffs or contact lenses; Accessories therefor
    • A61L2/02Methods or apparatus for disinfecting or sterilising materials or objects other than foodstuffs or contact lenses; Accessories therefor using physical phenomena
    • A61L2/08Radiation
    • A61L2/082X-rays
    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61LMETHODS OR APPARATUS FOR STERILISING MATERIALS OR OBJECTS IN GENERAL; DISINFECTION, STERILISATION OR DEODORISATION OF AIR; CHEMICAL ASPECTS OF BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES; MATERIALS FOR BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES
    • A61L2/00Methods or apparatus for disinfecting or sterilising materials or objects other than foodstuffs or contact lenses; Accessories therefor
    • A61L2/02Methods or apparatus for disinfecting or sterilising materials or objects other than foodstuffs or contact lenses; Accessories therefor using physical phenomena
    • A61L2/08Radiation
    • A61L2/087Particle radiation, e.g. electron-beam, alpha or beta radiation
    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61LMETHODS OR APPARATUS FOR STERILISING MATERIALS OR OBJECTS IN GENERAL; DISINFECTION, STERILISATION OR DEODORISATION OF AIR; CHEMICAL ASPECTS OF BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES; MATERIALS FOR BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES
    • A61L27/00Materials for grafts or prostheses or for coating grafts or prostheses
    • A61L27/14Macromolecular materials
    • A61L27/16Macromolecular materials obtained by reactions only involving carbon-to-carbon unsaturated bonds
    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61LMETHODS OR APPARATUS FOR STERILISING MATERIALS OR OBJECTS IN GENERAL; DISINFECTION, STERILISATION OR DEODORISATION OF AIR; CHEMICAL ASPECTS OF BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES; MATERIALS FOR BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES
    • A61L29/00Materials for catheters, medical tubing, cannulae, or endoscopes or for coating catheters
    • A61L29/04Macromolecular materials
    • A61L29/041Macromolecular materials obtained by reactions only involving carbon-to-carbon unsaturated bonds
    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61LMETHODS OR APPARATUS FOR STERILISING MATERIALS OR OBJECTS IN GENERAL; DISINFECTION, STERILISATION OR DEODORISATION OF AIR; CHEMICAL ASPECTS OF BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES; MATERIALS FOR BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES
    • A61L31/00Materials for other surgical articles, e.g. stents, stent-grafts, shunts, surgical drapes, guide wires, materials for adhesion prevention, occluding devices, surgical gloves, tissue fixation devices
    • A61L31/04Macromolecular materials
    • A61L31/048Macromolecular materials obtained by reactions only involving carbon-to-carbon unsaturated bonds
    • 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
    • B29C35/00Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
    • B29C35/02Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
    • B29C35/08Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation
    • B29C35/0805Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation using electromagnetic radiation
    • B29C2035/085Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation using electromagnetic radiation using gamma-ray
    • 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
    • B29C35/00Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
    • B29C35/02Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
    • B29C35/08Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation
    • B29C35/0805Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation using electromagnetic radiation
    • 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
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • 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
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/02Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
    • B29C43/16Forging
    • 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
    • B29K2023/00Use of polyalkenes or derivatives thereof as moulding material
    • B29K2023/04Polymers of ethylene
    • B29K2023/06PE, i.e. polyethylene
    • B29K2023/0658PE, i.e. polyethylene characterised by its molecular weight
    • B29K2023/0683UHMWPE, i.e. ultra high molecular weight polyethylene
    • 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
    • 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
    • B29K2995/00Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
    • B29K2995/0037Other properties
    • B29K2995/0087Wear resistance
    • 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
    • B29K2995/00Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
    • B29K2995/0037Other properties
    • B29K2995/0089Impact strength or toughness
    • 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
    • B29L2031/7532Artificial members, protheses
    • 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
    • Y10S522/00Synthetic resins or natural rubbers -- part of the class 520 series
    • Y10S522/915Synthetic resins or natural rubbers -- part of the class 520 series involving inert gas, steam, nitrogen gas, or carbon dioxide
    • 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
    • Y10S525/00Synthetic resins or natural rubbers -- part of the class 520 series
    • Y10S525/937Utility as body contact e.g. implant, contact lens or I.U.D.
    • 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
    • Y10S623/00Prosthesis, i.e. artificial body members, parts thereof, or aids and accessories therefor
    • Y10S623/901Method of manufacturing prosthetic device

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  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Veterinary Medicine (AREA)
  • Public Health (AREA)
  • Epidemiology (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Animal Behavior & Ethology (AREA)
  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Vascular Medicine (AREA)
  • Dispersion Chemistry (AREA)
  • Heart & Thoracic Surgery (AREA)
  • Dermatology (AREA)
  • Medicinal Chemistry (AREA)
  • Oral & Maxillofacial Surgery (AREA)
  • Transplantation (AREA)
  • Surgery (AREA)
  • Hematology (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Materials For Medical Uses (AREA)
  • Treatments Of Macromolecular Shaped Articles (AREA)
  • Polyesters Or Polycarbonates (AREA)

Abstract

A medical implant made of polymeric material having an increased oxidation resistance is formed by a method including the steps of placing a resin powder in a sealed container. A substantial portion of the oxygen is removed from the sealed container by either a vacuum, an oxygen absorbent or by flushing with inert gas. The container is then repressurized with a gas such as nitrogen, argon, helium or neon so that long term storage may be possible. On use, the resin is transferred to a forming device which both melts and forms the resin in an oxygen reduced atmosphere to produce a polymeric raw material such as a rod or bar stock. The medical implant is then formed from this raw material annealed and sealed in an airtight package in an oxygen reduced atmosphere. The implant is then radiation sterilized and thereafter annealed in the package for a predetermined time and temperature sufficient to form cross-links between any free radicals in neighboring polymeric chains.

Description

WO 94/27651 ~ PCT/IB94/00083 _1_ NON-OXIDIZING POLYMERIC MEDICAL IMPLANT
BACKGROUND OF THE INVENTION
Field of the Invention This invention relates to medical implants formed of a polymeric material such as ultra-high molecular weight polyethylene, with superior oxidation resistance upon irradiation and a method for making the same.
Description of the Prior Art Various polymer systems have been used for the preparation of artificial prostheses for biomedical use, particularly orthopedic applications. Among them, ultra-high molecular weight polyethylene is widely used for articulation surfaces in artificial knee and hip replacements. Ultra-high molecular weight polyethylene (UHMWPE) has been defined as those linear polyethylenes which have a relative viscosity of 2.3 or greater at a solution concentration of 0.05°~ at 135°C in decahydronaphthalene. The nominal weight - average molecular weight is at least 400,000 and up to 10,000,000 and usually from three to six million. The manu-facturing process begins with the polymer being supplied as fine powder which is consolidated into various forms, such as rods and slabs, using ram extrusion or compression molding. Afterwards, the consolidated rods or slabs are machined into the final shape of the orthopedic implant components. Alternatively, the component can be produced by compression molding of the UHMWPE resin powder.
All components must then go through a sterilization procedure prior to use, but usually after being packaged. There exists several sterilization methods which can be utilized for medical applications, such as the use of ethylene oxide, heat, or radiation. However, applying heat to a packaged polymeric medical product can destroy either the integrity of the packaging material (particularly the seal, which prevents bacteria from going into the package after the sterilization step) or the product itself.
Because ethylene oxide may adversely impact environmental and employee safety, gamma ray, x-ray or electron beam radiation has been utilized as a preferred means of sterilization. These types of radiation use a high energy beam to kill WO 94/27651 Z ? PCT/IB94/00083 bacteria, viruses, or other microbial species contained in the packaged medical products, achieving the goal of product sterility.
However, it has been recognized that regardless of the radiation type, the high energy beam causes generation of free radicals in polymers during radiation. It has also been recognized that the amount of free radicals generated is dependent upon the radiation dose received by the polymers and that the distribution of free radicals in the polymeric implant depends upon the geometry of the component, the type of polymer, the dose rate, and the type of radiation beam. The generation of free radicals can be described by the following reaction (which uses polyolefin and gamma ray irradiation for illustration):
gamma rays Polyolefin ------------~ r~ where r~ are primary free radicals * (1) *(through C-C chain scission or C-H scission) Depending whether or not oxygen is present, primary free radicals r~ will react with oxygen and the polymer according to the following reactions as described in "Radiation Effects on Polymers", edited by Roger L. Clough and Shalaby W.
Shalaby, published by American Chemical Society, Washington, D.C., 1991.
In the presence of oxygen r~ -----> r02~ (2) r02~ + polyolefin --------~ rOOH + P~ (3) P ~ + 02 __-. P02 ~ (4) OZ
POZ~ + polyolefin -----------~ POOH + P~ -> P02~ (5) r02 ~, P02 ~ -------~ Some chain scission products (6) room temperature rOOH, POOH - --~ free radicals, rOH, POH (7) P~ + POz~ - -~ POOP (ester cross-links) (8) 2 P~ ~ P-P (C-C cross-links) WO 94/27651 ~ ~ ~ ~ ~ PCT/IB94/00083 In radiation in air, primary free radicals r~ will react with oxygen to form peroxyl free radicals rOZ~, which then react with polyolefin (such as UHMWPE) to start the oxidative chain scission reactions (reactions 2 through 6). Through these reactions, material properties of the plastic, such as molecular weight, tensile, and wear properties, are degraded.
Recently, it was found that the hydroperoxides (rOOH and POOH) formed in reactions 3 and 5 will slowly break down as shown in reaction 7 to initiate post-radiation degradation. Reactions 8 and 9 represent termination steps of free radicals to form ester or carbon-carbon cross-links. Depending on the type of polymer, the extent of reaction 8 and 9 in relation to reactions 2 through 7 may vary. For irradiated UHMWPE, a value of 0.3 for the ratio of chain scission to cross-linking has been obtained, indicating that even though cross-linking is a dominant mechanism, a significant amount of chain scission occurs in irradiated polyethylene.
By applying radiation in an inert atmosphere, since there is no oxidant present, the primary free radicals r~ or secondary free radicals P~ can only react with other neighboring free radicals to form carbon-carbon cross-links, according to reactions 10 through 12 below. If all the free radicals react through reactions 10 through 12, there will be no chain scission and there will be no molecular weight degradation. Furthermore, the extent of cross-linking is increased over the original polymer prior to irradiation. On the other hand, if not all the free radicals formed are combined through reactions 10, 11 and 12, then some free radicals will remain in the plastic component.
In an Inert Atmosphere r~ + polyolefin - -> P~ (10) 2 r~ ----~ r-r (C-C cross-linking) (11 ) 2 P~ - -~ P-P (C-C cross-linking) (12) It is recognized that the fewer the free radicals, the better the polymer retains its physical properties over time. The greater the number of free radicals, the greater the degree of molecular weight and polymer property degradation will occur.

WO 94/27651 ~ ~ ~ PCT/IB94/00083 Applicant has discovered that the extent of completion of free radical cross-linking reactions is dependent on the reaction rates and the time period given for reaction to occur.
Several prior art patents attempt to provide methods which enhance UHMWPE physical properties. European Patent Application 0 177 522 B1 discloses UHMWPE powders being heated and compressed into a homogeneously melted crystallized morphology with no grain memory of the UHMWPE powder particles and with enhanced modulus and strength. U.S. Patent 5,037,928 discloses a prescribed heating and cooling process for preparing a UHMWPE exhibiting a combination of properties including a creep resistance of less than 1 °~6 (under exposure to a temperature of 23°C and a relative humidity of 50°~ for 24 hours under a com-pression of 1000 psi) without sacrificing tensile and flexural properties.
U.K. Patent Application GB 2 180 815 A discloses a packaging method where a medical device which is sealed in a sterile bag, after radiation/sterilization, is hermetically sealed in a wrapping member of oxygen-impermeable material together with a deoxidizing agent for prevention of post-irradiation oxidation.
U.S. Patent 5,153,039 relates to a high density polyethylene article with oxygen barrier properties. U.S. Patent 5,160,464 relates to a vacuum polymer irradiation process.
SUMMARY OF THE INVENTION
The present invention relates to a method for providing a polymeric material, such as UHMWPE, with superior oxidation resistance upon irradiation. For the purpose of illustration, UHMWPE will be used as an example to describe the invention. However, all the theories and processes described hereafter should also apply to other polymeric materials such as polypropylene, high density polyethylene, polyester, nylon, polyurethane and poly(methylmethacrylate) unless otherwise stated.
As stated above, while UHMWPE polymer is very stable and has very good resistance to aggressive media except for strong oxidizing acids. Upon sterilization radiation, free radicals are formed which cause UHMWPE to become activated for chemical reactions and physical changes. Possible chemical reactions include reacting with oxygen, water, body fluids, and other chemical compounds while physical changes include density, crystallin'tty, color, and other physical properties.
In the present invention a new sterilization radiation process greatly reduces the adverse effects caused by a conventional radiation process:
Furthermore, this new sterilization process does not employ stabilizers, antioxidants, or any other chemical compounds which may have potential adverse effects in biomedical or orthopedic applications.
In the sterilization process of the present invention, a polymeric orthopedic implant component to be sterilized by radiation does not contain oxidants, such as oxygen or water (or moisture), or free radicals. This may be accomplished by obtaining a raw material for the implant manufactured under a special process as described herein and forming a part of the invention.
The finished polymeric orthopedic component is then sealed in an oxidant-free atmosphere. This oxidant-free atmosphere is maintained during radiation. The radiated polymeric component is then subjected to a heat treatment to cross-link all the free radicals within themselves. During this treatment, the condition of oxidant-free atmosphere is maintained. The irradiated, heat treated plastic component is now ready to use. Exposure to oxygen or moisture will not cause oxidation. The oxidation resistance to any oxidizing agent is similar to that of the unirradiated virgin polymer.
It is therefore an object of the invention to provide a polymeric orthopedic implant having superior oxidation resistance after irradiation.
It is still another object of the invention to provide a method for manufacturing such an implant from the resin powder thereof through the final sterilization step so that the implant may thereafter be exposed to air without degradation due to oxidation.
Thus, a first aspect of the invention provides a medical implant made of an olefinic material, which has been irradiated in an atmosphere with no more than 1% oxygen v/v to form free radicals in the material and then heated to form cross-links between the free radicals in neighboring polymeric chains in an atmosphere having no more than 1% oxygen v/v at a temperature of between 25°C and the melting point of the material, and for a sufficient time to inactivate any residual free radicals.
A second aspect of the invention provides a method for producing a polymeric medical implant. The method may include the steps of placing the polymeric resin in a sealed container and removing a substantial portion of the oxygen from the container. After a predetermined time, the container is repressurized with an inert gas such as nitrogen, argon, helium or neon. The resin is thereafter transferred to a forming device which normally melts and forms the resin in an oxygen reduced atmosphere to produce a polymeric raw material.
The polymeric raw material such as UHMwPE is then machined to an implant such as a tibial tray or a linear for an acetabular cup. The finished part is then sealed into a package in an oxygen reduced atmosphere. The package is of an air-tight nature to prevent oxygen or moisture from entering after the package is sealed. The then packaged implant is radiation sterilized and then heat treated for the predetermined time and temperature sufficient to form cross-links between free - 6a -radicals of the neighboring polymeric chains. This prevents further oxidation once the implant is removed from the package.
In general, the implant is heated for at least 48 hours at a temperature of about 37°C to about 70°C and preferably for 144 hours at 50°C.
It should be understood that the expressions "oxidant-free atmosphere" and "oxygen reduced atmosphere"
share the same meaning and may be employed interchangeably in this specification.
DESCRIPTION OF THE PREFERRED EMBODIMENT
In the preferred method, a raw polymeric material such as UHMWPE is obtained by, for example, ram extrusion, compression molding, or other forming processes. These methods use virgin polymer powder as a starting material.
However, virgin polymeric resin powder may contain air or moisture, which may exist in the resin micro-structure or simply deposited on the resin surfaces. If air or moisture is not removed from resin powder prior to the forming process, it can be trapped in the plastic matrix after forming and can not escape. This is true even with the use of vacuum or gas flushing techniques. During the sterilization radiation process, the trapped air or moisture or both will react with free radicals generated in the plastic to cause oxidation.
The trapped moisture can also absorb radiation energy and dissociate into oxygen and hydroxyl free radicals which will also react with the plastic to cause oxidation. Therefore, by removing air and moisture prior to the forming process, - 6b -oxidation during sterilization radiation can be avoided.
The preferred method of eliminating air and moisture is to apply a vacuum of less than 3° of mercury (76 torr) to the polymer resin for a prescribed time to reduce the levels of air and moisture to a minimal or acceptable value. The level for oxygen is preferably 0.5% (volume by volume and no more than 1%). The moisture level is preferably 10% of relative humidity (and no more than 20% relative humidity).
Then sufficient amounts of deoxidizing agents, such as oxygen absorbents and moisture desiccants, are placed together with the polymer resin in a sealed container to reduce the levels of air and moisture to the minimal or acceptable value. An example of an oxygen absorbent is AGELESS° which is an iron oxide compound and commercially available from Cryovac Division, W.R. Grace & Co., Duncan, S.C. An example of moisture desiccant is silica gel which is commercially available. These materials are placed with the resin in the sealed container for approximately 10 hours. Alternately, or in combination, an inert gas, such as nitrogen, argon, helium or neon is used to flush the container, holding the polymer resin powder, _7_ until the levels of air and moisture are reduced to the accepted value. Of course, any combination of the above methods can also be used.
In order to ensure a raw material for an orthopedic implant with no oxygen, not only must the UHMWPE resin powder be free of air and moisture, but the entire forming operation of, for example, ram extrusion, compression molding, or other forming process should be carried out in an inert or low oxygen atmosphere as well.
During the forming process, due to high temperature and high pressure applied in the process, UHMWPE polymer chains may be broken to generate free radicals and cross-links. While cross-links generated in the forming process have no adverse effects on material properties, the free radicals produced, as described above, can react with air or other oxidants. Therefore, it is important to maintain the inert atmosphere during the forming process to minimize oxidation.
Any free radicals generated should be eliminated as soon as the forming process is completed by annealing. If the formed UHMWPE contains free radicals and is exposed to air or other oxidants after the forming process, oxidation will occur. The polymer should be annealed at an elevated temperature in an inert atmosphere for a prescribed time. This is because the rate of free radical reactions (reactions 10 through 12) increase with increasing temperature, according to the following general expressions:
dt. k, [r'] and dP' = k2 [P~] (13) Compared to room temperature, an elevated temperature not only increases the reaction rate constants, k, and k2, but also helps free radicals r~ and P~
to migrate in the plastic matrix to meet other neighboring free radicals for cross-linking reactions. In general, the desired elevated temperature is between the room temperature and the melting point of the polymer. For UHMWPE, this temperature range is between about 25°C and about 140°C. However, the preferred annealing temperature range is from about 37°C to about 135°C. The preferred time and temperature is 130°C for 20 hours with the minimum annealing time being about 4 hours (requiring a temperature at the high end of the range). It is to be noted that the higher the temperature used, the shorter the time period needed to combine free radicals. Additionally, due to the high viscosity of an UHMWPE melt, the formed UHMWPE often contains residual (internal) stress caused by incomplete relaxation WO 94/27651 d~ '~ ~ ~ ~ PCTIIB94100083 _g_ during the cooling process, which is the last step of the forming process. The annealing process described herein will also help to eliminate or reduce the residual stress. A residual stress contained in a plastic matrix can cause dimensional instability and is in general undesirable.
In applications such as for orthopedic implants, the formed UHMWPE is further machined into desired shapes. In general, the machining is done at room temperature and no damage to the plastic will occur. However, certain machine tools, when operated at a high speed, may generate local heat and cause thermal breakdown of UHMWPE polymer chains. In this case, the above described annealing process may be employed to eliminate any newly formed free radicals prior to packaging.
After machining, the polymeric component is packaged in an air tight package in an oxidant-free atmosphere. Thus, all air and moisture must be removed from the package prior to the sealing step. Machines to accomplish this are commercially available, such as from Orics Industries Inc., College Point, New York, which flush the package with a chosen inert gas, vacuum the container, flush the container for the second time, and then heat seal the container with a lid. In general, less than 0.5°~ (volume by volume) oxygen concentration can be obtained consistently. An example of a suitable oxidant impermeable (air tight) packaging material is polyethylene terephthalate (PET). Other examples of oxidant imper-meable packaging material is polyethylene vinyl alcohol) and aluminum foil, whose oxygen and water vapor transmission rates are essentially zero. All these materials are commercially available. Several other suitable commercial packaging materials utilize a layer structure to form a composite material with superior oxygen and moisture barrier properties. An example of this type is a layered composite comprised of poly-propylene/poly(ethylene vinyl alcohol)/polypropylene.
In general, the sterilization radiation step for the packaged implant may take a few hours to complete. As described above, it is imperative that during this time period, the transmission of oxidants, such as oxygen and moisture, into the package be kept to a minimal or at an acceptable value to avoid oxidation.
Following sterilization radiation, a heat treatment step should be performed in an inert atmosphere and at an elevated temperature to cause free radicals to form cross-links without oxidation. If proper packaging materials and processes are used and oxidant transmission rates are minimal, then the oxidant-free atmosphere can be WO 94/27651 ' ' PCTIIB94/00083 _g_ maintained in the package and a regular oven with air circulation can be used for heat treatment after sterilization. To absolutely ensure that no oxidants leak into the package, the oven may be operated under a vacuum or purged with an inert gas.
In general, if a higher temperature is used, a shorter time period is required to ' 5 achieve a prescribed level of oxidation resistance and cross-linking. In many cases, the relationship between the reaction temperature and the reaction rate follows the well-known Arrhennius equation:
k, or k2 = A * exp (~Hm (14) where k, and k2 are reaction rate constants from reactions 13 and 14 A is a reaction dependent constant ~H is activation energy of reaction T is absolute temperature (l~
However, the temperature should not exceed the distortion temperature of either the packaging material or the plastic components. For UHMWPE, the temp-erature range is between about 25°C and about 140°C. However, considering the distortion of the packaging material, the preferred temperature is 37°C
to 70°C.
It is very important to ensure that the number of free radicals has been reduced to a minimal or an accepted level by the heat treatment. This is because the presence of an oxidant causes not only the oxidation of pre-existing free radicals, but also the formation of new free radicals via reactions 2 through 7. When the number of free radicals grows, the extent of oxidation and the oxidation rate will increase according to the following equations:
dt. k3 ~r~1I~21 and dP~ - k~ IP'1(~21 (15) Where free radicals r~ and P~ can grow in number in the presence of oxidants and in tum increase the oxidation rates. It is also to be noted that the oxidation reaction rate constants k3 and k, increase with increasing temperature, similar to k, and kz. Therefore, to determine if a certain level of residual free radicals is acceptable or not, it is required to evaluate specific material properties after the plastic sample is stored or aged at the application temperature for a time period which is equal to or longer than the time period intended for the application of the plastic component. An alternative to the method to assess the aging effect is to raise the aging temperature of the plastic sample for a shorter time period. This will increase the reaction rate constants k3 and k4 significantly and shorten the aging time. It has been found that an acceptable level of residual free radicals is 1.0 x 1017/g for UHMWPE use for orthopaedic implants.
After heat treatment, the irradiated packaged plastic component is now ready to use. The package can be opened and exposed to air or moisture without causing oxidation. The oxidation resistance of the sterilized plastic component to other oxidants is similar to that of the virgin, unirradiated polymer.
Sample Preparation A surgical grade UHMWPE rod produced by ram extrusion was machined into samples of desirable shapes. Four sets of samples were prepared using these machined samples by the following methods:
Method A: an UHMWPE sample as machined and unirradiated Method B: an UHMWPE sample was heat sealed in a glycol-modified polyethylene terephthalate (PETG, made by Eastman Plastics, Inc., Kingsport, Tennessee) blister in air with an aluminum lid of 0.1 mm in thickness. The sealed blister containing the UHMWPE sheet was sterilized by irradiation of gamma-rays in a dose of 2.5 Mrad. The package was then opened and exposed to room air.
Method C: an UHMWPE sample was placed in a PETG blister and heat sealed in dry nitrogen with an aluminum lid of 0.1 mm in thickness by the Orics* Vaccum Gas Flush Heat Seal Machine (Model SLS-VGF-100M for modified atmosphere packaging, made by Orics Industries, Inc., College Point, New York.) which went through the following cycles:
i) nitrogen gas (moisture-free) flush for five second ii) vacuum to a pressure of equal to or below 3 inches of mercury iii) nitrogen gas flush (moisture-free) for five seconds iv) heat seal The oxygen concentration in the sealed blister was measured by a Mocon* Oxygen Analyzer to be 0.325% (volume by volume). The sealed blister containing the UHMWPE sample was sterilized by irradiation of gamma-rays in a dose of 2.5 Mrad.
The oxygen concentration in the sealed blister after sterilization radiation was measured to be 0.350%. The package was then opened and exposed to room air.
Method D: Same as Method C, except that after gamma-ray irradiation, the sealed blister containing the UHMWPE sample was heat treated at 50°C for 144 hours in an oven, then transferred from the oven to room temperature for cooling.
After the package was cooled to room temperature, the oxygen concentration was measured by a Mocon* Oxygen Analyzer to be 0.360%. The package was then opened and exposed to room air.
Samples prepared by the above methods were used in the following examples for evaluation.
*Trade-mark - lla -Example 1:
Two sets of 1-mm-thick UHMWPE sheets prepared by Methods A through D above mere oven aged in air at 80°C for 11 and 23 days respectively. After these sheets were cooled in room temperature, a thin film specimen of about 100 microns in thickness was cut from each of the 1-mm-thick aged UHMWPE
sheets and placed in an IR window for a standard FTIR (A
Nicolet* 710 FTIR system was used) transmission run. A total of 32 spectra (scans) were collected and averaged. To determine the extent of oxidation, the IR absorption peaks in the frequency range of between 1660 and 1800 cm-1, corresponding to carbonyl (C-O) functional groups, were integrated for the peak area. The peak area is proportional to the amount of oxidized UHMWPE in the specimen. To correct for difference in specimen thickness, the integrated peak area was then normalized to the specimen thickness, by dividing by the area of the 1463 cm-1 (methyl) peak which is proportional to the specimen thickness. The obtained ratio was defined as oxidation index. A third set of 1-mm-thick UHMWPE sheets prepared by methods A through D, but without oven aging, were also evaluated by the same FTIR method for comparison.
Oxidation indices obtained are shown in Table 1:
*Trade-mark WO 94/27651 PCT/IB94/00083 ' Sample Oxidation Index Method A / not oven aged ca. 0.

Method A / 11 day oven aging ca. 0.

Method A / 23 day oven aging ca. 0.

Method B / not oven aged 0.02 Method B / 11 day oven aging 0.06 Method B / 23 day oven aging 0.11 Method C / not oven aged 0.01 Method C / 11 day oven aging 0.04 Method C / 23 day oven aging 0.08 Method D / not oven aged 0.01 Method D / 11 day oven aging 0.01 Method D / 23 day oven aging 0.01 From Table 1 results, it can be seen that the unirradiated UHMWPE sample (Method A) was free of oxidation (below the FTIR detectable level), even after days of oven aging in air at 80°C. On the other hand, the UHMWPE sample irradiated in air (Method B) showed considerable oxidation and the extent of oxidation (as indicated by the oxidation index) increased with increasing aging time.
After 23 days of oven aging, the oxidation index reached 0.11. For the UHMWPE
sample irradiated in nitrogen (Method C), the initial oxidation index before oven aging was 0.01 which was not significant. However , during the oven aging, the oxidation index increased to 0.04 for 11 days and 0.08 for 23 days respectively. The results indicate that while irradiation in an inert atmosphere is an improvement over oxidation in air, the irradiated plastic component will oxidize further over time once it is exposed to air or other oxidants. In contrast, the UHMWPE sample irradiated in nitrogen followed by heat treatment at 50°C for 144 hours (Method D), showed an WO 94/27651 ~PCT/IB94/00083 initial oxidation index of only 0.01 which did not increase after 11 or 23 days of oven aging, indicating that this sample has superior oxidation resistance than the samples prepared by Method B or C.
Example 2:
Two sets of 1-mm-thick UHMWPE sheets prepared by Methods B through D
cited in the Sample Preparation were oven aged in air at 80°C for 11 and 23 days respectively. After these sheets were cooled in room temperature, six tensile specimens with a dumbbell shape according to ASTM D638 (Type I~ were cut from each of the 1-mm-thick aged UHMWPE sheets. A standard tensile test was pertormed for each specimens at a speed of 2 inches/min. Another set of 1-mm-thick UHMWPE sheets prepared by Methods B through D cited in the Sample Preparation, but without oven aging, were also evaluated by the same tensile test method for comparison. Tensile breaking strength results (average of six tests for each condition) are shown in Table 2:

Sample Tensile Breaking Strength, psi Method B / not oven aged 6510 Method B / 11 day oven aging 5227 Method B / 23 day oven aging 3192 Method C / not oven aged 6875 Method C / 11 day oven aging 6400 Method C / 23 day oven aging 6004 Method D / not oven aged 6941 Method D / 11 day oven aging 7113 Method D / 23 day oven aging 6904 From Table 2, tensile breaking strength shows the most deterioration for the sample irradiation in air (Method B). The sample irradiated in nitrogen (Method C) shows some improvement over the sample prepared by Method B. However, the decrease in tensile breaking strength upon oven aging still occurs. In contrast, the sample irradiated in nitrogen followed by heat treatment (50°C for 144 hours, Method D), shows no change in tensile breaking strength, indicating a superior oxidation resistance.
Example 3:
Two sets of 1-mm-thick UHMWPE sheets prepared by Method B and Method D cited in the Sample Preparation were oven aged in air at 80°C for 11 and 23 days respectively.
After these sheets were cooled in room temperature, samples cut from sheets were characterized by a high temperature gel permeation chromatograph (GPC) column for molecular weight distribution. The samples were dissolved in hot trichlorobenzene (TCB). They were then run in the aforementioned solvent at 1.2 ml/min. using a Jordi* Gel Mixed Bed Column, 50 cm x 10.0 mm ID., at a column oven temperature of 145°C on the Waters* 150C Chromatograph. The injection size was 250uL of a 0.1% solution. An antioxidant (N-phenyl-2-naphthylamine) was added to all high temperature GPC samples to prevent polymer deterioration.
Prior to sample runs, the column was calibrated using narrow MW polystyrene standards. Since the samples were only partially soluble in the solvent due to cross-linking, *Trade-mark - 14a -the so-determined molecular weight distribution was for the soluble portion only. To determine the extent of cross-linking (solubility), a two hundred milligram sample cut from sheets were dissolved in 100cc of 1,2,4-trichlorobenzene.
Each sample was then heated to approximately 170°C with N-phenyl-2-naphthylamine antioxidant added for 6 hours. The samples were then hot filtered at approximately 170°C using separate preweighed high temperature filters for each sample.
After filtration, the filters were cooled to room temperature and washed individually with dichloromethane.
They were then placed in a convection oven at 105°C for 6 hours to dry and then reweighed. The weight fraction of the undissolved (cross-linked) portion was then determined based upon the initial weight of 200 mg. To determine the low molecular weight fraction present in each sample, the weight fraction of molecular weight below 105 in the soluble portion, determined by GPC, was multiplied by the percent solubility to give weight percent of low molecular weight fraction in each sample. Results are shown in Table 3:

Weight Percent Percent Weight Percent of of Soluble Portion Solubility Entire Sample Sample Below 105 in Solvent Below 105 Method B /without28.0 98.2 27.5 oven aging Method B /11 36.2 100.0 36.2 day oven aging Method B /23 48.1 100.0 48.1 day oven aging I

Method D /without22.7 80.9 18.4 oven aging Method D /11 20.5 73.6 15.1 day oven aging Method D /23 24.2 74.7 18.1 day oven aging From Table 3, it can be seen that the sample made by Method D contains more cross-linking (i.e. less soluble) than one made by Method B. Upon oven aging, the low molecular weight fraction (defined as below 105) in the sample made by Method B increases from 0.275 to 0.481 while that of the sample made by Method D remains virtually unchanged at about 0.18 after 23 days of oven aging.
The increase in low molecular weight fraction was due to chain scission caused by oxidative reactions. The results indicate that the process of method D can produce an irradiated polymer with a superior oxidation resistance.

Example 4:
UHMWPE samples of 0.5 inch cubes prepared by Methods B and Method D
cited in the Sample Preparation were evaluated for deformation under load (creep resistance). Testing procedures according to ASTM D 621 (A) (24hr/23°C/1000 psi/90 min recovery) were used. Results are summarized in Table 4:

Deformation under Sample Load, %

Method B 0.80 Method D 0.60 From Table 4, it is concluded that the sample prepared by Method D, the invention, possesses a superior creep resistance (0.6°~) to one prepared by Method B (0.8°~).
Example 5:
Two 1-mm-thick UHMWPE samples were annealed in a oven filled with air and dry nitrogen (oxygen concentration is below 0.2°~) respectively at 130°C for 20 hours in order to remove residual stress on the samples. After the sheets were cooled to room temperature in the oven, they were removed from the oven and cut into dumbbell shaped tensile specimens (ASTM D 638, Type ~ for evaluation. A
standard tensile test according to ASTM D 638 was performed at a speed of 2 inches/min for each of six specimens annealed in air and in dry nitrogen respectively. Results are shown in Table 5:

Toughness, Sample EAB, % TYS, psi TBS, psi Ibs-in/in' Air annealed 414 3547 6257 10,210 Nitrogen 485 3517 8917 18,960 annealed Note: EAB - elongation at break lYS - tensile yield strength TBS - Tensile breaking strength l?
From the above table, it is seen that the sample annealed in nitrogen exhibits a higher elongation at break, a higher tensile breaking strength, and a higher toughness, compared to one annealed in air, while the tensile yield strength is similar between the two samples. The results indicate that the sample annealed in nitrogen is more ductile than the one annealed in air. The loss of ductility in the sample annealed in air is due to oxidative chain scission.
To determine oxidation indices in these two samples, a thin film specimen of ca. 100 microns in thickness was cut from each of the 1-mm-thick annealed UHMWPE sheets and placed in an IR window for a standard FTIR (a Nicolet 710 FTIR system was used) transmission run, using the procedures and calculations employed in the Sample Preparation. Oxidation indices obtained are shown in Table 6.

Sample Oxidation Index Air Annealed 0.10 Nitrogen Annealed ca. 0.0 From the above results, it is seen that the UHMWPE sample annealed in air after ram extrusion showed significant oxidation due to free radicals generated in the forming process. In contrast, the UHMWPE sample annealed in nitrogen showed no oxidation (below the FTIR detectable level). It is concluded that annealing in nitrogen can prevent the polymer from oxidation and produce a polymer with superior ductility.
While several examples of the present invention have been described, it is obvious that many changes and modifications may be made thereunto, without departing from the spirit and scope of the invention.
t

Claims (41)

THE EMBODIMENTS OF THE INVENTION IN WHICH AN EXCLUSIVE
PROPERTY OR PRIVILEGE IS CLAIMED ARE DEFINED AS FOLLOWS:
1. A method for producing a polymeric medical implant having improved oxidation resistance, which method comprises the steps of:
forming the implant from a polymeric material;
sealing the formed implant in a package in an oxygen reduced atmosphere having an oxygen content of no more than 1%;
radiation sterilizing the packaged implant; and heating the packaged implant for a predetermined time and temperature sufficient to form cross-links between free radicals in neighboring polymeric chains.
2. The method as set forth in claim 1, wherein the predetermined temperature is between about 37°C and about 70°C.
3. The method as set forth in claim 2, wherein the predetermined time is at least forty eight hours.
4. The method as set forth in claim 3, wherein the predetermined temperature is 50°C and the predetermined time is 144 hours.
5. The method as set forth in any one of claims 1 to 3, wherein the polymeric material is ultra high molecular weight polyethylene having a molecular weight between 400,000 and 10,000,000.
6. The method as set forth in claim 5, wherein the predetermined temperature is 50°C and the predetermined time is 144 hours.
7. The method as set forth in any one of claims 1 to 6, wherein the radiation sterilization is performed by gamma ray, x-ray or electron beam radiation.
8. The method as set forth in any one of claims 1 to 7, wherein the implant is formed from the polymeric material by ram extrusion or compression molding.
9. The method as set forth in any one of claims 1 to 8, wherein the oxygen reduced atmosphere is made up of a gas selected from the group consisting of nitrogen, helium, argon, and neon and a combination thereof.
10. The method as set forth in any one of claims 1 to 8, wherein the reduced oxygen atmosphere is produced by a vacuum of less than 3 inches of mercury.
11. The method as set forth in any one of claims 1 to 10, wherein the sealing in the reduced oxygen atmosphere is produced by first flushing the package with a gas selected from the group consisting of nitrogen, helium, argon, neon and a combination thereof, then applying a vacuum of less than 3 inches of mercury to the package, and flushing the package with a gas selected from the above-mentioned group.
12. A medical implant made of a polymeric material comprising polymeric chains having a free radical concentration of less than 1 x 10 17/g achieved by heating the implant to a temperature of between about 37°C and about 70°C
for at least forty eight hours in an oxygen reduced atmosphere prior to the oxidation of the free radicals, wherein the oxygen reduced atmosphere has no more than 1% oxygen.
13. The medical implant as set forth in claim 12, wherein the polymeric material is polyethylene having a molecular weight of between 400,000 and 10,000,000.
14. A method for producing raw polymeric material having improved oxidation resistance from a plastic resin powder for a medical implant, which method comprises the step of:
placing the resin in a sealed container;
reducing a level of oxygen in the sealed container to no more than 1% (volume by volume);
re-pressurizing the sealed container with a gas selected from the group consisting of nitrogen, argon, helium and neon and a combination thereof;
then transferring the resin to a forming device which both melts and forms the resin in an oxygen reduced atmosphere having an oxygen content of no more than 1% to produce the raw material; and thereafter annealing the raw material for a predetermined time at a predetermined temperature.
15. The method as set forth in claim 14, wherein raw material is a rod or slab.
16. The method as set forth in claim 14 or 15, wherein the forming device operates in an atmosphere of less than 1%
oxygen.
17. The method as set forth in claim 14, 15 or 16, wherein the resin material is polyethylene having a molecular weight of between 400,000 and 10,000,000.
18. The method as set forth in any one of claims 14 to 17, wherein the reduction of the oxygen level in the container involves applying vacuum, flushing with an inert gas, using an oxygen absorbent or a combination thereof.
19. The method as set forth in any one of claims 14 to 18, wherein the annealing step takes place at a temperature between about 37°C and about 135°C for at least four hours in an oxygen reduced atmosphere having no more than 1% oxygen.
20. A method for producing a medical implant having improved oxidation resistance from a plastic resin powder, which method comprises the steps of:

placing the resin in a sealed container;
reducing a level of oxygen in the sealed container to no more than 1% (volume by volume);
re-pressurizing the sealed container with a gas selected from the group consisting of nitrogen, argon, helium, neon and a combination thereof;
then transferring the resin to a forming device which both melts and forms the resin in an oxygen reduced atmosphere to produce a polymeric raw material;
thereafter annealing the raw material for a predetermined time at a predetermined temperature;
forming the implant from the polymeric raw material;
sealing the formed implant in a package in an oxygen reduced atmosphere;
radiation sterilizing the packaged implant; and heating the packaged implant for a predetermined time and temperature sufficient to form cross-links between free radicals in neighboring polymeric chains, wherein the oxygen reduced atmosphere has an oxygen content of no more than 1%.
21. The method as set forth in claim 20, wherein the removal of oxygen from the container involves a method selected from the group consisting of applying a vacuum, flushing with an inert gas, using an oxygen absorbent and a combination thereof.
22. The method as set forth in claim 20 or 21, wherein the annealing step takes place at a temperature between about 37°C and about 135°C for at least four hours in an oxygen reduced atmosphere.
23. A method for producing a polymeric medical implant material having improved oxidation resistance, which method comprises the steps of:
forming the implant from the polymeric material;
packaging the formed implant in an oxygen reduced atmosphere having an oxygen content of no more than 1%, radiation sterilizing the packaged implant while maintaining the oxygen reduced atmosphere; and heating the packaged implant while maintaining the oxygen reduced atmosphere for at least 48 hours at a temperature of about 37°C to about 70°C.
24. The method as set forth in claim 23, wherein the polymeric material is ultra high molecular weight polyethylene having a molecular weight between 400,000 and 10,000,000.
25. The method as set forth in claim 23 or 24, wherein the heating of the packaged implant is conducted at a temperature of 50°C for 144 hours.
26. The method as set forth in any one of claims 14 to 19, wherein the reduction of the oxygen level is produced by a vacuum of less than 3 inches of mercury.
27. The method as set forth in claim 23, wherein the heating step is performed in an inert atmosphere.
28. A medical implant made of an olefinic polymeric material, the material having been irradiated in an atmosphere with no more than 1% oxygen v/v to form free radicals in the material and then heated to form cross-links between the free radicals in neighboring polymeric chains in an atmosphere having no more than 1% oxygen v/v at a temperature of between 25°C and the melting point of the material, and for a sufficient time to inactivate any residual free radicals.
29. The medical implant as defined in claim 28, wherein the free radicals include peroxy and hydroperoxy groups on the polymer chains.
30. The medical implant as defined in claim 28, wherein the atmosphere comprises an inert gas or a vacuum.
31. A medical implant of an olefinic polymeric material having a molecular weight of 400,000 to 10,000,000, the material having been irradiated while in an atmosphere having no more than 1% oxygen v/v and heated in an atmosphere having no more than 1% oxygen v/v for a sufficient time and at a temperature of between 25°C and the melting point of the material to form cross-links between free radicals in neighboring polymeric chains.
32. The medical implant of claim 31, wherein the free radicals include peroxy and hydroperoxy groups of the polymer chains.
33. The medical implant of claim 31, wherein the atmosphere comprises an inert gas or a vacuum.
34. A medical implant made of an olefinic polymeric material having a molecular weight of 400,000 to 10,000,000 comprising polymeric chains having a free radical concentration of less than 1 x 10 17/g achieved by a combination of irradiating the material and heating the material to a temperature of between 25°C and about 140°C for at least about four hours in an atmosphere having no more than 1% oxygen v/v prior to oxidation of the free radicals.
35. The medical implant as set forth in claim 34, wherein the polymeric material is polyethylene.
36. A medical implant comprising an olefinic polymeric material having improved properties resulting from first creating free radicals in the material by irradiating the material in an atmosphere with no more than 1% oxygen v/v and forming cross-links between the free radicals by using heat while the material is in an atmosphere having no more than 1%
oxygen v/v at a temperature between 25°C and the melting point of the material.
37. The medical implant of claim 36, wherein the free radicals include peroxy and hydroperoxy groups on polymer chains.
38. The medical implant of claim 36, wherein the atmosphere comprises an inert gas or a vacuum.
39. The medical implant of claim 38, wherein the irradiating is electron beam irradiation.
40. The medical implant of any one of claims 28 through 39, wherein the polymeric material is ultra-high molecular weight polyethylene.
41. A method for producing a medical implant from powdery ultra high molecular weight polyethylene (UHMWPE) having a molecular weight between 400,000 and 10,000,000 which method comprises the steps of:
placing the powdery UHMWPE in a sealed container;
applying a vacuum of less than 76 torr to the powdery UHMWPE in the sealed container for a prescribed time to reduce a level of oxygen to no more than 1% (volume by volume) and a level of moisture to no more than 20% relative humidity;
re-pressurizing the sealed container with an inert gas selected from the group consisting of nitrogen, argo, helium, neon and a combination thereof;
transferring the powdery UHMWPE to a forming device which both melts and forms the powdery UHMWPE in an atmosphere of the inert gas to produce a UHMWPE raw material;
annealing the UHMWPE raw material for a predetermined time of at least 4 hours at a temperature between 25°C and 140°C in an atmosphere of the inert gas;
matching the annealed UHMWPE raw material to form the implant in an atmosphere of the inert gas;
sealing the formed implant in an air-tight package in an atmosphere of the inert gas, wherein air and moisture have been removed from the package prior to the sealing step;
sterilizing the packaged implant by irradiation of gamma ray, x-ray or electron beam; and heating the sterilized packaged implant at a temperature between 37°C and 70°C for a predetermined time in an inert atmosphere to cause free radicals to form cross-links without oxidation.
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