Orthopaedic Implants Having Self-Lubricated Articulating Surfaces Designed to Reduce Wear, Corrosion, and Ion Leaching
20170258597 · 2017-09-14
Inventors
- Arnold H. Deutchman (Columbus, OH, US)
- Robert J. Partyka (Columbus, OH, US)
- Robert J. Borel (Naples, FL, US)
- Stephen White (Fort Wayne, IN, US)
Cpc classification
A61F2/4405
HUMAN NECESSITIES
A61F2310/00592
HUMAN NECESSITIES
A61F2/30767
HUMAN NECESSITIES
A61F2/30724
HUMAN NECESSITIES
A61F2310/00023
HUMAN NECESSITIES
A61F2/4014
HUMAN NECESSITIES
A61F2002/30935
HUMAN NECESSITIES
A61F2002/4233
HUMAN NECESSITIES
A61F2002/4022
HUMAN NECESSITIES
A61F2002/345
HUMAN NECESSITIES
A61F2002/30624
HUMAN NECESSITIES
C23C28/044
CHEMISTRY; METALLURGY
A61F2/3609
HUMAN NECESSITIES
A61L27/306
HUMAN NECESSITIES
A61L2400/12
HUMAN NECESSITIES
C23C14/46
CHEMISTRY; METALLURGY
C23C14/022
CHEMISTRY; METALLURGY
A61F2002/443
HUMAN NECESSITIES
A61F2310/00634
HUMAN NECESSITIES
A61F2310/00604
HUMAN NECESSITIES
A61F2310/00856
HUMAN NECESSITIES
C23C14/0031
CHEMISTRY; METALLURGY
A61F2310/0073
HUMAN NECESSITIES
A61F2002/30675
HUMAN NECESSITIES
A61F2002/30682
HUMAN NECESSITIES
A61F2310/00029
HUMAN NECESSITIES
C23C28/042
CHEMISTRY; METALLURGY
A61L2430/02
HUMAN NECESSITIES
A61L27/50
HUMAN NECESSITIES
A61F2310/00616
HUMAN NECESSITIES
International classification
A61L27/50
HUMAN NECESSITIES
A61F2/42
HUMAN NECESSITIES
C23C28/04
CHEMISTRY; METALLURGY
Abstract
An orthopaedic implant can replace a joint in a patient. The orthopaedic implant includes a first component having a first component surface and a second component having a second component surface. The first component surface and the second component surface mate at an interface. The first component surface includes a metal substrate, a nanotextured surface, a ceramic coating, and a transition zone. The nanotextured surface is disposed directly upon the metal substrate and has surface features in a size of 10.sup.−9 meters. The ceramic coating conforms to the nanotextured surface and includes a plurality of bio-active sites configured to attract and retain calcium and phosphorous cations. The transition zone is disposed between the metal substrate and the ceramic coating. The transition zone includes a concentration gradient transitioning from the metal substrate to the ceramic coating and there is no distinct interface between the metal substrate and the ceramic coating.
Claims
1. An orthopaedic implant to replace a joint in a patient, the orthopaedic implant comprising: a first component having a first component surface; and a second component having a second component surface, wherein the first component surface and the second component surface are configured to mate at an interface, wherein the first component surface includes: a metal substrate; a nanotextured surface disposed directly upon the metal substrate having surface features in a size of 10.sup.−9 meters; a ceramic coating conforming to the nanotextured surface and including a plurality of bio-active sites configured to attract and retain calcium and phosphorous cations; and a transition zone disposed between the metal substrate and the ceramic coating, wherein the transition zone includes a concentration gradient transitioning from the metal substrate to the ceramic coating and wherein there is no distinct interface between the metal substrate and the ceramic coating.
2. The orthopaedic implant according to claim 1, wherein the joint is selected from the group consisting of: a knee joint; a hip joint; a shoulder joint; an elbow joint; a finger joint; a wrist joint; a facet joint disposed between two vertebrae; a lumbar disc joint; and a toe joint.
3. The orthopaedic implant according to claim 1, wherein the metal substrate is selected from the group consisting of; stainless steels; Co—Cr—Mo alloys; Zr alloys; and Ti alloys.
4. The orthopaedic implant according to claim 1, wherein the ceramic coating is selected from the group consisting of: Al.sub.2O.sub.3 (alpha phase); zirconium oxide (Zr.sub.2O); silicon nitride (Si.sub.3N.sub.4); titanium nitride (TiN); metallic nitrides; and metallic carbides.
5. The orthopaedic implant according to claim 1, wherein the nanotextured surface is configured to improve lubricity of the orthopaedic implant in the presence of bodily fluids.
6. The orthopaedic implant according to claim 5, wherein the plurality of bio-active sites are configured to improve lubricity of the orthopaedic implant by retaining calcium and phosphorous cations from synovial fluid upon the nanotextured surface.
7. The orthopaedic implant according to claim 1, wherein the second component surface includes: a second metal substrate; a second nanotextured surface disposed directly upon the second metal substrate having surface features in a size of 10.sup.−9 meters; a second ceramic coating conforming to the second nanotextured surface and including a second plurality of bio-active sites configured to attract and retain calcium and phosphorous cations; and a second transition zone disposed between the second metal substrate and the second ceramic coating, wherein the second transition zone includes a second concentration gradient transitioning from the second metal substrate to the second ceramic coating and wherein there is no distinct interface between the second metal substrate and the second ceramic coating.
8. The orthopaedic implant according to claim 1, wherein the ceramic coating is imbedded to a depth of about 5 nanometers below the nanotextured surface.
9. The orthopaedic implant according to claim 1, wherein a grain structure of the ceramic coating is substantially amorphous.
10. The orthopaedic implant according to claim 1, wherein the nanotextured surface is generated with a directional ion beam sputtering device.
11. The orthopaedic implant according to claim 1, wherein the ceramic coating is generated with an ion beam enhanced deposition (IBED) process.
12. An orthopaedic implant to replace a joint in a patient, the orthopaedic implant comprising: a first component having a first component surface; and a second component having a second component surface, wherein the first component surface and the second component surface are configured to mate at an interface, wherein the first component surface includes: a metal substrate; a nanotextured surface disposed directly upon the metal substrate having surface features in a size of 10.sup.−9 meters; and a ceramic coating conforming to the nanotextured surface and including a plurality of bio-active sites configured to attract and retain calcium and phosphorous cations, at least a portion of the ceramic coating being ballistically imbedded below the nanotextured surface with no distinct interface between the metal substrate and the ceramic coating.
13. The orthopaedic implant according to claim 12, wherein the joint is selected from the group consisting of: a knee joint; a hip joint; a shoulder joint; an elbow joint; a finger joint; a wrist joint; a facet joint disposed between two vertebrae; a lumbar disc joint; and a toe joint.
14. The orthopaedic implant according to claim 12, wherein the metal substrate is selected from the group consisting of; stainless steels; Co—Cr—Mo alloys; Zr alloys; and Ti alloys.
15. The orthopaedic implant according to claim 12, wherein the ceramic coating is selected from the group consisting of: Al.sub.2O.sub.3 (alpha phase); zirconium oxide (Zr.sub.2O); silicon nitride (Si.sub.3N.sub.4); titanium nitride (TiN); metallic nitrides; and metallic carbides.
16. The orthopaedic implant according to claim 12, wherein the nanotextured surface is configured to improve lubricity of the orthopaedic implant in the presence of bodily fluids.
17. The orthopaedic implant according to claim 16, wherein the plurality of bio-active sites are configured to improve lubricity of the orthopaedic implant by retaining calcium and phosphorous cations from synovial fluid upon the nanotextured surface.
18. The orthopaedic implant according to claim 12, wherein the second component surface includes: a second metal substrate; a second nanotextured surface disposed directly upon the second metal substrate having surface features in a size of 10.sup.−9 meters; and a second ceramic coating conforming to the second nanotextured surface and including a second plurality of bio-active sites configured to attract and retain calcium and phosphorous cations, at least a portion of the second ceramic coating being ballistically imbedded below the second nanotextured surface with no distinct interface between the second metal substrate and the second ceramic coating.
19. The orthopaedic implant according to claim 12, wherein the ceramic coating is imbedded to a depth of about 5 nanometers below the nanotextured surface.
20. The orthopaedic implant according to claim 12, wherein a grain structure of the ceramic coating is substantially amorphous.
21. The orthopaedic implant according to claim 12, wherein the nanotextured surface is generated with a directional ion beam sputtering device.
22. The orthopaedic implant according to claim 12, wherein the ceramic coating is generated with an ion beam enhanced deposition (IBED) process.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DETAILED DESCRIPTION
[0030] The performance of orthopaedic implants 10 of all types and particularly those that provide motion when implanted in the body can be improved dramatically through the use of embodiments of the present invention. The surface treatments described herein may reduce the generation of wear debris, corrosion products, and metal ion leaching when applied to orthopaedic implants 10 of various designs and made from a wide variety of materials. Thus, when so-treated, orthopaedic implants 10 used in patients to restore skeletal motion impaired by injury or disease may reduce or eliminate the osteolysis, inflammatory and toxic response, and carcinogenic effects that can adversely affect conventional implants. This reduction in generation of wear debris is achieved by applying coatings to the articulating counterfaces of the implants that are more wear-resistant, corrosion-resistant, and self-lubricating than the various metallic, ceramic, and plastic materials the implants themselves are made from.
[0031] According to various embodiments of the invention, surfaces of orthopaedic implants may be treated to reduce wear and improve lubrication. In general, modular orthopaedic implants suitable for use with embodiments of the invention are varied in design and may employ articulating surfaces having different combinations of materials. In some suitable designs, one element may be a metal alloy and the opposed articulating element may be a polymer. In other suitable designs one element may be a metal alloy and the opposed articulating element may be a similar metal alloy. In yet other suitable designs one element may be a ceramic material and the opposed articulating element may be a polymer. And in still another suitable design one element may be a ceramic material and the opposed articulating element may be a similar ceramic material. By treating mating surfaces of the orthopaedic implants as described herein, friction, wear, corrosion, and/or fatigue may be minimized, resulting in a reduced generation of wear debris and metal ion release; and improved lubricity.
[0032] Orthopaedic implants treated according to various embodiments of this invention exhibit reduced generation and release of wear particles, corrosion products, and metallic ions into the body. This reduction in non-biologic contaminants results in a reduced inflammatory response of the body to the implant which improves the longevity of the implant residing in the body. The various embodiments of this invention provide an orthopaedic implant that exhibits reduced generation and release of metallic, plastic, and ceramic wear particles; corrosion products; and metallic ions into the body thereby reducing the inflammatory response of the skeletal tissue to the implant. This results in reducing osteolysis leading to loosening of the orthopaedic implant in the bone into which it is implanted, and enhances its longevity.
[0033] As described herein, a surface treatment may be applied to either one or both of the articulating opposed surfaces of the implant. The surface treatment provides hardness, wear-resistance and corrosion-resistance, and has self-lubricating features that further help reduce the generation and release of wear debris. This surface treatment may be a coating that is initially alloyed into one or more of the articulating surfaces of the implant to form a transition zone starting below the surface of the substrate and then grown to a finite dimensional thickness from the alloyed surface. This transition zone includes a concentration gradient transitioning from the metal substrate to the ceramic coating that has no distinct interface between the metal substrate and the ceramic coating. This facilitates relatively greater adhesion of the coating to the articulating surfaces of the implant as compared to conventional coatings. As such, delamination of the coating from the treated articulating surfaces of the implant is reduced or eliminated. In addition, the surface treatment provides a self-lubricating property to further reduce wear between the articulating elements. This is achieved by providing biologically active sites on the surface of the coatings that attract and hold natural lubricants such as synovial fluid or other extracellular fluids present in the tissue around the articulating elements. These fluid retentive surfaces act to provide a continuous thin layer of lubrication between the treated articulating elements which reduces or eliminates physical contact between the surfaces of the elements thus reducing or eliminating the generation and release of metallic, plastic, and ceramic wear debris; corrosion products; and metallic ions into the body.
[0034] Conventional case hardening and coating methods often undesirably alter the bulk properties of the materials to which they are applied. Specifically, the hardness, toughness, fracture-resistance, and dimensionality may be altered in an undesirable manner by conventional hardening and coating techniques. Post-coating heat-treatments and/or machining may be employed to return the bulk properties to these conventionally treated articles. However, many materials cannot be heat-treated without detrimental effects. Particular examples of materials that cannot be heat treated without detrimental effects include: any of the family of stainless steels, Co—Cr—Mo alloys, Ti—Al—V alloys, Zr alloys; alumina and zirconia ceramics; and plastics. It is an advantage of embodiments of the invention that the bulk properties of the implant material are substantially unaffected by surface treatments as described herein. As such, post-coating heat-treating or machining may be avoided.
[0035] The coating provided by the various surface treatments described herein may be applied to a metal substrate. These coatings include hard ceramic material such as aluminum oxide (Al.sub.2O.sub.3, alpha phase), zirconium oxide (Zr.sub.2O), metallic nitrides (such as TiN, Si.sub.3N.sub.4, CrN, ZrN, TaN), and/or metallic carbides (such as Cr.sub.2C, TiC, WC). The use of these and other hard ceramic materials further reduces abrasion of the coating. In this manner, orthopaedic implants 10 that have high bulk fracture/fatigue-resistant properties characteristic of metallic materials, and also have the high surface wear- and corrosion-resistant properties characteristic of hard ceramic materials may be provided by various embodiments of the invention. This is achieved by applying a ceramic material to the articulating surface of a metallic implant which minimizes the chance of catastrophic failure of the implant due to fracture of the bulk material.
[0036] The method of treating one or both of the articulating opposed bearing surfaces of the implant as described herein produces a thin nanocrystalline or nearly-amorphous coating that may include multiple contiguous layers of different materials such as metals (Cr, Ni, Ti, Zr, Al, and others) and hard ceramics such as aluminum oxide (Al.sub.2O.sub.3, alpha phase), zirconium oxide (Zr.sub.2O), or metallic nitrides (such as TiN, Si.sub.3N.sub.4, CrN, ZrN, TaN), or metallic carbides (such as Cr.sub.2C, TiC, WC), each grown directly and sequentially from the previously grown layer. In general, this coating process may be carried out at a temperature of 600 degrees Fahrenheit or less. This reduces or eliminates temperature induced changes in bulk properties or dimensions of the treated element. In addition this coating process produces a thin nanocrystalline or nearly-amorphous coating on the articulating surface thereby minimizing the possibility that intergranular cracks or voids in the coating can allow corrosion and subsequent release of metal ions and/or particle wear debris into the patient. Furthermore, this thin nanocrystalline or nearly-amorphous coating on the articulating surface minimizes the possibility that intergranular cracks in the coating can propagate into the underlying substrate to cause it to fail prematurely, as by a fatigue mechanism. It is a further advantage that coating applied as described herein are resistant to the effects of gamma ray sterilization procedures. Thus, the treated implants can sterilized without degrading the wear-resistant, corrosion-resistant, and self-lubricating properties of the treated implant.
[0037] The invention will now be described with reference to the drawing figures, in which like reference numerals refer to like parts throughout.
[0038]
[0039] A variety of combinations of materials are suitable for use with the contacting articulating surfaces of elements in modular orthopaedic hips, knees and other implants according to various embodiments of the invention. These combinations include metal-polymer, ceramic-polymer, metal-metal, and ceramic-ceramic. When treated or coated as described herein, these material combinations reduce friction, wear, and corrosion in modular articulating orthopaedic implants 10. It is an advantage of embodiments of the invention that undesirable particle debris may be reduced or eliminated by the treatments described herein. Particular examples of drawbacks associated with untreated conventional materials are described in Table I and highlight the innovative features of the current invention.
TABLE-US-00001 TABLE I Drawbacks of Conventional Implant Material Combinations Material Combi- Typical nation Materials Effects Metal-Polymer Metal Stainless Steel, Abrasive wear against UEMWPE Co—Cr—Mo, constantly removes passive oxide Ti—Al—V, Zr layer on the metal which releases metal ions which are potentially toxic and carcinogenic. Polymer UEMWPE Adhesive wear releases polymeric particle debris. Fatigue wear releases particulate debris, produces fatigue failure fragments, and plastic deformation and cracking of the UEMWPE. Polymeric wear debris and fragments leads to loosening of the implant. Ceramic-Polymer Ceramic Sintered Abrasive wear against UEMWPE less alumina or than that seen with metal components. zirconia Ceramic wear debris is considered biologically inert Polymer UEMWPE Adhesive wear releases polymeric particle debris. Fatigue wear releases particulate debris, produces fatigue failure fragments, and plastic deformation and cracking of the UEMWPE. Polymeric wear debris and fragments leads to loosening of the implant. Metal-Metal Metal Co—Cr—Mo, Abrasive wear against opposed Ti—Al—V, metallic surface constantly removes Zr passive oxide layer on the metal which releases metal ions which are potentially toxic and carcinogenic. Adhesive wear against opposed metallic surface will produce galling with constant generation of particulate metallic particle debris. Ceramic-Ceramic Ceramic Sintered Wear rate less than seen with metals alumina or and ceramic wear debris considered zirconia biologically inert. Bulk ceramic materials are brittle and subject to fatigue fracture producing large ceramic fragments and possible catastrophic failure.
[0040] Referring to Table I, it is seen that conventional polymeric materials such as UHMWPE are subject to abrasive, adhesive, and fatigue wear, all of which contribute to the release of polymeric particle debris. In addition the UHMWPE is soft and is subject to bulk plastic deformation and dimensional distortion. The surfaces of metallic components wearing against each other are also subject to abrasive, adhesive and fatigue failure. Abrasive rubbing of opposed metallic surfaces constantly removes passive oxide layers on both metal surfaces which release metal ions that are potentially toxic and carcinogenic. Adhesive wear between the opposed metal surfaces will produce galling and metal transfer with constant generation of particulate metallic particle debris. And under cyclic loading conditions the metal surfaces eventually show fatigue wear. Ceramic materials, when wearing against polymer and metal surfaces exhibit low coefficients of friction and generate relatively low levels of ceramic wear debris. Likewise ceramic elements wearing against each other produce relatively low levels of ceramic wear debris. However, bulk ceramic materials are brittle and subject to fatigue fracture producing large ceramic fragments and possible catastrophic failures.
[0041]
[0042] Furthermore, the IBED process allows a high degree of control over the mechanical and metallurgical properties of the ceramic coatings 76 and 78. The metallurgical composition can be maintained in a highly uniform manner throughout the ceramic coatings. As a result, properties such as hardness and wear-resistance can be optimized to reduce or eliminate wear debris generation from the metallic surface beneath the ceramic coating. The coating grain sizes can further be maintained in the nanometer (1×10.sup.−9 meter) range allowing the coatings to grow substantially void- and pinhole-free thus eliminating corrosion and ion leaching from the metallic surface beneath the ceramic coating. The metallurgical composition can also be tailored to provide biologically active sites on the external surfaces (80 and 82) of the ceramic coating that attract and hold natural lubricants (synovial or other extracellular fluids) present in the tissue around the articulating elements. These fluid retentive surfaces provide a continuously forming thin layer of lubrication 58 between the treated articulating elements that reduces or eliminates physical contact between the surfaces of the elements. In this manner, the generation and release of wear debris, corrosion products, and metallic ions into the body is reduced or eliminated.
[0043] The IBED process used to form a ceramic coating in and on the surfaces of the metallic articulating elements proceeds as a continuous, uninterrupted, two-step process described in the following Table II:
TABLE-US-00002 TABLE II Step 1 Surface Texturing) Step 2 (Coating) A B A B C D Article placed Surface Coating Initial case Thin Thicker in vacuum textured material layer of conformal coating grown chamber by ion evolved and coating coating grown while beam deposited on material while continuously sputtering surface of alloyed into continuously augmented by article surface of augmented by ion beam article ion beam
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[0046] As shown in
[0047] The IBED process used to form a ceramic coating in and on the surfaces of the metallic articulating elements proceeds as a continuous, uninterrupted, two-step process is outlined below in Table III:
TABLE-US-00003 TABLE III Step 1 (Surface Texturing) Step 2 (Coating) A B A B C D Article placed Surface Coating Initial case Thin Thicker in vacuum textured material layer of conformal coating grown chamber by ion evolved and coating coating grown while beam deposited on material while continuously sputtering surface of alloyed into continuously augmented by article surface of augmented by ion beam article ion beam
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[0049] If multiple layers of coating material are to be applied, the beam of texturing/augmenting 162 ions is simultaneously applied to the surface of the first coating layer and is used initially to mix or ballistically embed the coating material into the surface of the first coating layer forming an alloyed case layer in the first coating layer, and then used to control the composition and crystal structure of the second coating layer as it is grown out from the first coating layer. During both the cleaning and alloying/coating step, the part platen 154 may be rotated about its axis 156 and oscillated about its center 158 to facilitate uniform coverage of the articles. A thickness measuring gauge 168 is positioned near the part platen 154 in order to monitor the arrival of the evaporated coating material 166 and control formation of the alloyed surface layer and then the thicker coating grown from the alloyed surface layer.
[0050] Preferably, the two-step treatment process is carried out sequentially in the same vacuum chamber without releasing the high vacuum to atmospheric pressure between steps. If this occurs a latent oxide layer will form on the cleaned surface and will interfere with the formation of the coating. It is also preferable to accurately control the intensities of the cleaning/augmenting ion beam and the angular position of the articles to be treated relative to this directional beam such that the surface alloyed layer and coating are applied uniformly to the surface to be treated.
[0051] Embodiments of the invention are further illustrated by the following non-limiting four Examples in which examples of particular coating parameter and test data associated with the coated items is presented.
EXAMPLE 1
[0052] Samples of Co—Cr—Mo materials used to manufacture the orthopaedic implants 10 were prepared and coated with a ceramic coating as described herein. The samples were pins and disks utilized in the standard Pin-On-Disk wear test procedure (ASTM F732-00(2006) Standard Test Method for Wear Testing of Polymeric Materials Used in Total Joint Prostheses, American Society For Testing and Materials). The wear of the coated pin and disks was measured and compared to the wear found with uncoated pins and disks manufactured from the same Co—Cr—Mo material.
[0053] In this case a two-layer coating was deposited on the pins and disks using the inventive IBED process. The first (inner) layer was titanium nitride (TiN) and the second (outer) layer was aluminum oxide (Al.sub.2O.sub.3). The procedures and processing parameters utilized to deposit the two-layer coating on the pin and disk sample materials are as follows:
TABLE-US-00004 TABLE IV Step 1: Surface Texturing Description Process Parameters A Pin & Disk materials placed in vacuum Vacuum: 1.0E(−07) Torr chamber on a rotatable articulated fixture which allows programmed orientation of the device during the process. B Surface of the Pin & Disk materials Ion Species: N textured by ion beam sputtering with the Beam Energy: 1000 eV ion beam from the augmenting ion source Beam Current: 4.4 mA/cm.sup.2 and manipulating the materials such that the Angle of incidence between 45-75 sputtering angle of incidence is maintained degrees on the surfaces to be textured Part Platen Rotation: 30 RPM Time: 10 minutes Step 2: Coating by Vacuum Evaporation, TIN first (inner) layer, Al.sub.2O.sub.3 second Description Process Parameters (TiN) Process Parameters (Al.sub.2O.sub.3) A E-gun evaporator used Material: Ti Material: Al.sub.2O.sub.3 to melt and evaporate Part platen held at angle Part platen held at angle coating material between 25 and 75 between 25 and 75 degrees continuously onto degrees to evaporator flux to evaporator flux surface of Pin & Disk. Evolution Rate: 14.5 Evolution Rate: 10 Å/sec Å/sec Part Platen Rotation: 30 Part Platen Rotation: 30 RPM RPM Temperature: 750° F. Temperature: <200° F. B Augmenting ion beam Ion species: N Ion species: Ar used to alloy the first Beam Energy: 1000 eV Beam Energy: 1000 eV few layers of the Beam Current: 4.4 Beam Current: 2.7 mA/cm.sup.2 evaporated coating mA/cm.sup.2 Material: Al.sub.2O.sub.3 material into device Material: Ti Part platen held at angle surface of the Pin & Part platen held at angle between 25 and 75 degrees Disk thus forming a between 25 and 75 to evaporator flux case layer. degrees to evaporator flux Time: 30 seconds Time: 40 seconds Part platen Rotation: 30 Part platen Rotation: 30 RPM RPM Temperature: 750° F. Temperature: <200° F. C Thin conformal Ion species: N Ion species: Ar coating is grown out Beam Energy: 800 eV Beam Energy: 800 eV from the alloyed case Beam Current: 4.4 Beam Current: 2.7 mA/cm.sup.2 layer as evaporation of mA/cm.sup.2 Material: Al.sub.2O.sub.3 the coating material Material: Ti Part platen held at angle continues. Part platen held at angle between 25 and 75 degrees Augmenting ion beam between 25 and 75 to evaporator flux used to control the degrees to evaporator flux Thickness: 50 A composition and Thickness: 50 A Part Platen Rotation: 30 crystal structure of the Part Platen Rotation: 30 RPM coating as it is grown. RPM Temperature: 750° F. Temperature: <200° F. D Coating is grown out Ion species: N Ion species: Ar from the conformal Beam Energy: 800 eV Beam Energy: 800 eV coating as evaporation Beam Current: 4.4 Beam Current: 2.7 mA/cm.sup.2 of the coated material mA/cm.sup.2 Material: Al.sub.2O.sub.3 continues. Material: Ti Part platen held at angle Augmenting ion beam Part platen held at angle between 25 and 75 degrees used to control the between 25 and 75 to evaporator flux composition and degrees to evaporator flux Thickness: 50,000 Å crystal structure of the Thickness: 10,000 Å Part Platen Rotation: 30 coating as it is grown. Part Platen Rotation: 30 RPM RPM Temperature: 750° F. Temperature: <200° F.
[0054] The test conditions and results of the Pin-On-Disk testing are seen in Table V. In this test, the pin and disk sample materials coated with a two layer TiN/Al.sub.2O.sub.3 coating. As a result of a run for 2,000,000 inches of wear travel in the Pin-On-Disk tester a volumetric loss of 0.25 mm.sup.3 is shown. This compares to a volumetric loss of 2.1 mm.sup.3 measured for 2,000,000 inches of wear travel for uncoated Co—Cr—Mo material.
TABLE-US-00005 TABLE V Comparison of Volumetric Wear Loss (ASTM, F732) Sample Material Load (lbs/in.sup.2) # of Inches Loss (mm.sup.3) IBED Coated Co—Cr—Mo 11,700 2,000,000 0.25 Co—Cr—Mo 1 11,700 2,000,000 2.1
EXAMPLE 2
[0055] A 5 micron thick single layer coating of chromium nitride (Cr.sub.2N) was deposited on a 304 stainless steel panel using the inventive process described in U.S. Ser. No. 11/042,150 and then tested for resistance to abrasive wear using a standard Taber Abraser Test. The test was applied using the procedure defined by Military Test Specification (MIL-A-8625F) in which an abrasive wheel (Taber, CS-10), impregnated with 50 micron diameter corundum grits, is rubbed against the coating surface with a loading of 2.2 pounds of force, and run for 10,000 abrasion cycles. The wear loss is measured and presented as the number of microns of coating lost per 10,000 wear cycles.
[0056] The procedures and processing parameters utilized to deposit the single layer Cr.sub.2N coating on the 304 stainless steel panel are described in Table VI as follows:
TABLE-US-00006 TABLE VI Step 1: Surface Texturing Description Process Parameters A Panel material placed in vacuum Vacuum: 1.0E(−07) Torr chamber on a rotatable articulated fixture which allows programmed orientation of the device during the process. B Surface of the Panel material Ion Species: N textured by ion beam sputtering Beam Energy: 1000 eV with the ion beam from the Beam Current: 4.4 augmenting ion source and mA/cm.sup.2 manipulating the materials such Angle of incidence that the sputtering angle of between 45-75 degrees incidence is maintained on the Part Platen Rotation: 30 surfaces to be textured RPM Time: 10 minutes Step 2: Coating by Vacuum Evaporation, Cr.sub.2N Process Parameters Description (Cr.sub.2N) A E-gun evaporator used to melt Material: Cr and evaporate coating material Part platen held at angle continuously onto surface of the between 25 and 75 Panel degrees to evaporator flux Evolution Rate: 12 Å/sec Part Platen Rotation: 30 RPM Temperature: <200° F. B Augmenting ion beam used to Ion species: N alloy the first few layers of the Beam Energy: 1000 eV evaporated coating material into Beam Current: 3.4 device surface of the Panel thus mA/cm.sup.2 forming a case layer. Material: Cr Part platen held at angle between 25 and 75 degrees to evaporator flux Time: 40 seconds Part platen Rotation: 30 RPM Temperature: <200° F. C Thin conformal coating is grown Ion species: N out from the alloyed case layer Beam Energy: 800 eV as evaporation of the coating Beam Current: 3.4 material continues. Augmenting mA/cm.sup.2 ion beam used to control the Material: Cr composition and crystal Part platen held at angle structure of the coating as it is between 25 and 75 grown. degrees to evaporator flux Thickness: 50 A Part Platen Rotation: 30 RPM Temperature: <200° F. D Coating is grown out from the Ion species: N conformal coating as Beam Energy: 800 eV evaporation of the coated Beam Current: 3.4 material continues. Augmenting mA/cm.sup.2 ion beam used to control the Material: Cr composition and crystal Part platen held at angle structure of the coating as it is between 25 and 75 grown. degrees to evaporator flux Thickness: 50,000 Å Part Platen Rotation: 30 RPM Temperature: <200° F. 1 (R.A. Poggie, “A Review Of The Effects Of Design, Contact Stress, And Materials On The Wear Of Metal-On-Metal Hip Prostheses,” from Alternate Bearing Surfaces In Total Joint Replacement, American Society for Testing and Materials, Special Technical Publication STP 1346, 1998)
[0057] The result of the Taber Abrasive Wear Testing is seen in Table VII. The MED Cr.sub.2N coating, showed a loss of 0.15 microns (μ) in thickness for the 10,000 cycles of abrasive wear. This compares to a thickness loss of 2.82 microns measured for 10,000 cycles of abrasive wear on uncoated Co—Cr—Mo material with a Rockwell “C” Scale Hardness of 45, that typical of material used for orthopaedic hip and knee implant components.
TABLE-US-00007 TABLE VII Taber Wear Measurement (MIL-A-8625F) Material Abrasive # of Cycles Wear (μ) IBED Cr.sub.2N Coating CS-10 10,000 0.15 Co—Cr—Mo (R.sub.C 45) CS-10 10.000 2.82
EXAMPLE 3
[0058] A 5 micron thick single layer coating of aluminum oxide (Al.sub.2O.sub.3) was deposited on a 304 stainless steel panel as described herein and then tested for resistance to abrasive wear using a standard Taber Abraser Test. The test was applied using the procedure defined by Military Test Specification (MIL-A-8625F) in which an abrasive wheel (Taber, CS-10), impregnated with 50 micron diameter corundum grits, is rubbed against the coating surface with a loading of 2.2 pounds of force, and run for 10,000 abrasion cycles. The wear loss is measured and presented as the number of microns of coating lost per 10,000 wear cycles.
[0059] The procedures and processing parameters utilized to deposit the single layer Al.sub.2O.sub.3 coating on the 304 stainless steel panel are illustrated in Table VIII as follows:
TABLE-US-00008 TABLE VIII Step 1: Surface Texturing Description Process Parameter A Panel material placed in vacuum Vacuum: 1.0E(−07) Torr chamber on a rotatable articulated fixture which allows programmed orientation of the device during the process. B Surface of the Panel material Ion Species: Ar textured by ion beam sputtering Beam Energy: 1000 eV with the ion beam from the Beam Current: 4.4 augmenting ion source and mA/cm.sup.2 manipulating the materials such Angle of incidence that the sputtering angle of between 45-75 degrees incidence is maintained on the Part Platen Rotation: 30 surfaces to be textured RPM Time: 10 minutes Step 2: Coating by Vacuum Evaporation, Al.sub.2O.sub.3 Process Parameters Description (Al.sub.2O.sub.3) A E-gun evaporator used to melt Material: Al.sub.2O.sub.3 and evaporate coating material Part platen held at angle continuously onto surface of the between 25 and 75 Panel degrees to evaporator flux Evolution Rate: 12 Å/sec Part Platen Rotation: 30 RPM Temperature: <200° F. B Augmenting ion beam used to Ion species: Ar alloy the first few layers of the Beam Energy: 1000 eV evaporated coating material into Beam Current: 2.7 device surface of the Panel thus mA/cm.sup.2 forming a case layer. Material: Al.sub.2O.sub.3 Part platen held at angle between 25 and 75 degrees to evaporator flux Time: 40 seconds Part platen Rotation: 30 RPM Temperature: <200° F. C Thin conformal coating is grown Ion species: Ar out from the alloyed case layer Beam Energy: 800 eV as evaporation of the coating Beam Current: 2.7 material continues. Augmenting mA/cm.sup.2 ion beam used to control the Material: Al.sub.2O.sub.3 composition and crystal Part platen held at angle structure of the coating as it is between 25 and 75 grown. degrees to evaporator flux Thickness: 50 A Part Platen Rotation: 30 RPM Temperature: <200° F. D Coating is grown out from the Ion species: Ar conformal coating as Beam Energy: 800 eV evaporation of the coated Beam Current: 2.7 material continues. Augmenting mA/cm.sup.2 ion beam used to control the Material: Al.sub.2O.sub.3 composition and crystal Part platen held at angle structure of the coating as it is between 25 and 75 grown. degrees to evaporator flux Thickness: 50,000 Å Part Platen Rotation: 30 RPM Temperature: <200° F.
[0060] The result of the Taber Abrasive Wear Testing is seen in Table IX. The IBED Al.sub.2O.sub.3 coating, showed a loss of 0.07 microns (μ) in thickness for the 10,000 cycles of abrasive wear. This compares to a thickness loss of 2.82 microns measured for 10,000 cycles of abrasive wear on uncoated Co—Cr—Mo material with a Rockwell “C” Scale Hardness of 45, that typical of material used for orthopaedic hip and knee implant components.
TABLE-US-00009 TABLE IX Taber Wear Measurement (MIL-A-8625F) Material Abrasive # of Cycles Wear (μ) IBED Al.sub.2O.sub.3 Coating CS-10 10,000 0.07 Co—Cr—Mo (R.sub.C 45) CS-10 10.000 2.82
EXAMPLE 4
[0061] Pin and disk samples were prepared from Co—Cr—Mo material used to manufacture orthopaedic implants, and then coated with a ceramic coating as described herein in order to test the fluid retentive properties of the deposited ceramic. In this case a two-layer coating was deposited on the Co—Cr—Mo pin and disk using the inventive MED process. The first (inner) layer was titanium nitride (TiN) and the second (outer) layer was aluminum oxide (Al.sub.2O.sub.3). The procedures and processing parameters utilized to deposit the two-layer coating on the Co—Cr—Mo pin and disk samples are illustrated in Table X as follows:
TABLE-US-00010 TABLE X Step 1: Surface Texturing Description Process Parameters A Pin & Disk materials placed in vacuum Vacuum: 1.0E(−07) Torr chamber on a rotatable articulated fixture which allows programmed orientation of the device during the process. B Surface of the Pin & Disk materials Ion Species: N textured by ion beam sputtering with the Beam Energy: 1000 eV ion beam from the augmenting ion Beam Current: 4.4 mA/cm.sup.2 source and manipulating the materials Angle of incidence between 45-75 such that the sputtering angle of degrees incidence is maintained on the surfaces Part Platen Rotation: 30 RPM to be textured Time: 10 minutes Step 2: Coating by Vacuum Evaporation, TiN first (inner) layer, Al.sub.2O.sub.3 second Description Process Parameters (TiN) Process Parameters (Al.sub.2O.sub.3) A E-gun evaporator Material: Ti Material: Al.sub.2O.sub.3 used to melt and Part platen held at angle Part platen held at angle evaporate coating between 25 and 75 between 25 and 75 degrees material degrees to evaporator flux to evaporator flux continuously onto Evolution Rate: 14.5 Evolution Rate: 10 Å/sec surface of Pin & Å/sec Part Platen Rotation: 30 Disk. Part Platen Rotation: 30 RPM RPM Temperature: 750° F. Temperature: <200° F. B Augmenting ion Ion species: N Ion species: Ar beam used to alloy Beam Energy: 1000 eV Beam Energy: 1000 eV the first few layers Beam Current: 4.4 Beam Current: 2.7 mA/cm.sup.2 of the evaporated mA/cm.sup.2 Material: Al.sub.2O.sub.3 coating material Material: Ti Part platen held at angle into device surface Part platen held at angle between 25 and 75 degrees of the Pin & Disk between 25 and 75 to evaporator flux thus forming a degrees to evaporator flux Time: 30 seconds case layer. Time: 40 seconds Part platen Rotation: 30 Part platen Rotation: 30 RPM RPM Temperature: 750° F. Temperature: <200° F. C Thin conformal Ion species: N Ion species: Ar coating is grown Beam Energy: 800 eV Beam Energy: 800 eV out from the Beam Current: 4.4 Beam Current: 2.7 mA/cm.sup.2 alloyed case layer mA/cm.sup.2 Material: Al.sub.2O.sub.3 as evaporation of Material: Ti Part platen held at angle the coating Part platen held at angle between 25 and 75 degrees material between 25 and 75 to evaporator flux continues. degrees to evaporator flux Thickness: 50 A Augmenting ion Thickness: 50 A Part Platen Rotation: 30 beam used to Part Platen Rotation: 30 RPM control the RPM Temperature: 750° F. composition and Temperature: <200° F. crystal structure of the coating as it is grown. D Coating is grown Ion species: N Ion species: Ar out from the Beam Energy: 800 eV Beam Energy: 800 eV conformal coating Beam Current: 4.4 Beam Current: 2.7 mA/cm.sup.2 as evaporation of mA/cm.sup.2 Material: Al.sub.2O.sub.3 the coated Material: Ti Part platen held at angle material Part platen held at angle between 25 and 75 degrees continues. between 25 and 75 to evaporator flux Augmenting ion degrees to evaporator flux Thickness: 50,000 Å beam used to Thickness: 10,000 Å Part Platen Rotation: 30 control the Part Platen Rotation: 30 RPM composition and RPM Temperature: 750° F. crystal structure of Temperature: <200° F. the coating as it is grown.
[0062] An additional set of pin-on-disk samples was prepared from solid, single crystal, alpha phase Al.sub.2O.sub.3. The counter facing surfaces of this pin-on-disk set would not have the same surface nanostructure, and thus fluid-retentive properties, as would the Al.sub.2O.sub.3 coating deposited on the Co—Cr—Mo samples using the inventive process.
[0063] Both sample pin and disk sets were tested according to the standard pin-on-disk wear test procedure (ASTM F732-00(2006) “Standard Test Method for Wear Testing of Polymeric Materials Used in Total Joint Prostheses, American Society for Testing and Materials”). The samples were immersed in defined bovine calf serum as a lubricant (Hyclone Labs: Cat. No. SH30073.04) during the entirety of the test. After completion of 2,000,000 cycles in the pin-on-disk test, both sample sets were carefully dried and the surface the pins imaged using scanning electron microscopy (SEM), and the surface composition analyzed with energy dispersive X-ray analysis (EDAX).
[0064] No residue was detected by either SEM imaging or EDAX analysis on the surface of the single crystal, alpha phase, pin indicating that the surface of the solid Al.sub.2O.sub.3 pin did not have the properties of a fluid-retentive surface. The IBED-coated Co—Cr—Mo pin surface did however show remnants of a film that had been retained on the surface of the Al.sub.2O.sub.3 coating.
[0065] Conclusions:
[0066] The orthopaedic implants 10 with surface treatments provided by this invention will generate less debris in the form of wear products, corrosion products, and metallic ion leaching which are liberated and transported to bone, blood, the lymphatic system, and other internal organs. This will result in less inflammation, toxicity, and immune response resulting in increased longevity of the orthopaedic implant 10 and less adverse effects on the patient. The surface treatments can be applied to a variety of the materials used to fabricate the articulating elements of the modular orthopaedic implants 10, and are useful for a variety of combinations of metal, ceramic, and polyethylene articulating elements.
[0067] In addition to orthopedic implants where the inventive process is applied to both mating surfaces of an articulating joint there are other devices which articulate in which it is appropriate to apply the inventive process to only one mating surface. These devices include, and are not be limited to, the knee, the hip, the shoulder, the elbow (ulna), the wrist, the ankle, spine disc, spine facet, the finger, and the toe.
[0068] The design of another typical modular articulating orthopaedic implant, for example an artificial shoulder, is shown in
[0069] The design of another typical modular articulating orthopaedic implant, for example an elbow, is shown in
[0070] The design of another typical modular articulating orthopaedic implant, for example a wrist, is shown in
[0071] The design of another typical modular articulating orthopaedic implant, for example an ankle, is shown in
[0072] The design of another typical modular articulating orthopaedic implant, for example a facet joint replacement, is shown in
[0073] The design of another typical modular articulating orthopaedic implant, for example a lumbar disc replacement, is shown in
[0074] The design of another typical modular articulating orthopaedic implant, for example a finger, is shown in
[0075] The design of another typical modular articulating orthopaedic implant, for example a toe, is shown in
[0076] The many features and advantages of the invention are apparent from the detailed specification, and thus, it is intended by the appended claims to cover all such features and advantages of the invention which fall within the true spirit and scope of the invention. Further, since numerous modifications and variations will readily occur to those skilled in the art, it is not desired to limit the invention to the exact construction and operation illustrated and described, and accordingly, all suitable modifications and equivalents may be resorted to, falling within the scope of the invention.