AU2006218030B2

AU2006218030B2 - Method for producing a medical implant made of a beta-titanium alloy and a corresponding implant

Info

Publication number: AU2006218030B2
Application number: AU2006218030A
Authority: AU
Inventors: Sevki Baliktay; Arnold Keller
Original assignee: Waldemar Link GmbH and Co KG
Current assignee: Waldemar Link GmbH and Co KG
Priority date: 2005-02-25
Filing date: 2006-02-27
Publication date: 2012-02-02
Anticipated expiration: 2026-02-27
Also published as: MX2007010440A; ATE546111T1; AR055735A1; CN101128164A; AU2006218030A1; ES2381679T3; ZA200707588B; JP5033644B2; EP1695675A1; KR101224338B1; RU2007135065A; BRPI0608554A2; CN101128164B; EP1850801A1; TWI441623B; JP2008536535A; WO2006089791A1; EP1850801B1; CA2597249A1; RU2397738C2

Abstract

The invention relates to a joint prosthesis with a shaft made of a titanium alloy. According to the invention, at least the shaft (10) is precision cast and has a centered cubical crystalline structure. A titanium allow with this crystalline structure (so-called ß-titanium alloy) has an advantageously low modulus of elasticity, which is well-adapted to the physiological requirements. In addition, the embodiment as a finished casting enables a complex shaping. Especially effective is an embodiment as a femoral prosthesis (1) for an artificial hip joint, which has a longitudinally extended shaft (10) with grooves (14) and sawtooth-like projections (15) for bone anchoring.

Description

- 2 JOINT PROSTHESIS MADE FROM A TITANIUM ALLOY The invention relates to a joint prosthesis having a shaft made from a titanium alloy. 5 The major joints of the human body are subject to high mechanical stresses. For example, the joints of the locomotor apparatus have to bear a large part of the body's weight, and moreover they are moved every time a step is taken. Therefore, the bones which support the 10 joints have a powerful cortical structure. Their integrity is important for sufficient functioning of the joint. The same is true of the arm joints; although the weight which they have to support is lower, they are moved more frequently and are therefore exposed to high levels of 15 wear. Moreover, their dimensions are smaller and they are more susceptible to injury. Prostheses intended for permanent implantation (endoprostheses) not only have to have sufficient mechanical properties to ensure the desired functionality, 20 but also have to have a biocompatibility that is as high as possible to ensure that they are tolerated by the patient over a prolonged period of time. In particular the latter aspect is very important, since any incompatibilities which occur generally require 25 explanation of the prosthesis. This equates to failure of the prosthesis. It is known that inadequate transmission of load from the prosthesis to the surrounding bone can lead to degeneration of the bone tissue. This often leads to the 2994169 911211 299410_.1 (GHMettem) P64243.AU -3 prosthesis coming loose. Therefore, to avoid this degeneration, it is important to ensure loading that is as physiological as possible by the prosthesis. Tests have shown that hip prostheses with a lower modulus of 5 elasticity produce a loading situation which is more physiological than when using rigid prostheses. For example, in the case of femoral prostheses, there has been a move away from cobalt-chromium alloys, which generally have a very high modulus of elasticity in the region of 10 approx. 200 000 N/mm 2 , toward titanium alloys, which have a lower modulus of elasticity, such as for example TiAl6V4, the modulus of which is approx. 100 000 N/mm 2 . However, these levels are still well above the modulus of elasticity of the cortical bone, at approx. 25 000 N/mm. is The present invention provides in a first aspect a joint prosthesis having a shaft made from a titanium molybdenum alloy having a molybdenum content in the range of 7.5 to 25%, wherein 20 at least the shaft is investment-cast and has a body centered cubic crystal structure (known as 9-titanium alloy), and wherein the modulus of elasticity of the shaft is 68 kW/mm 2 and 59.4 kW/mm 2 . 25 It has been found that the joint prosthesis according to an embodiment of the invention can be used to achieve a significantly lower modulus of elasticity. Depending on the titanium alloy used and the heat treatment carried out, it is possible to reach moduli of elasticity of 29941699/1211 ~48l(GHPM.UOm) P54243 AU -4 approx. 60 000 N/mm 2 . This corresponds to virtually half the modulus of elasticity which has previously been achieved with titanium alloys. Furthermore, an embodiment of the invention provides for at least the shaft to be s investment-cast. This allows more complex shaping of the prosthesis. The forging processes which have hitherto primarily been used for titanium prostheses only allow the production of relatively simple structures. This restriction is overcome by the invention. Consequently, 10 the prostheses according to an embodiment of the invention can be better matched to the loads which are to be absorbed. For example, the shaping of the prosthesis may vary more finely according to the local stresses. The prosthesis only has to be of stronger and therefore more 15 rigid dimensions in specifically the regions in which high stresses occur; in the other regions, it can be of weaker and therefore more elastic design. This allows the matching of the prosthesis to the anatomical conditions to be further improved. Moreover, it is easy for securing 20 elements, such as projections, to be formed integrally with the prosthesis. It is possible to provide a greater number of and more complex securing elements. Therefore, the prosthesis is more suitable for cement-free implantation. The benefit of the invention is that complex 25 shapes which cannot be practically realized by forging processes can be achieved even for prostheses made from 9 titanium alloys. In general, it will be the case that the prosthesis together with the shaft is investment-cast and heat-treated in one piece, although the possibility of 30 assembling the prosthesis from a plurality of parts including the shaft should not be ruled out. 2994169 9/12/11 2M16l9_1 (GHMatters) P64243.AU - 5 Embodiments of the invention can advantageously be used for artificial hip joints, in particular for femoral prostheses. These are among the most highly stressed prostheses and have a shaft of complicated shape for 5 implantation in the femur. It has been found that degeneration phenomena readily occur in particular in the upper region of the femur if a prosthesis that is too rigid has been implanted. This often leads to failure of the prosthesis. In the case of a femoral prosthesis 10 according to embodiments of the invention, the modulus of elasticity is considerably lower and therefore much closer to a physiological level of the bone material in the upper region of the femur. The femoral prosthesis according to embodiment of the invention successfully counteracts the 15 risk of degeneration. The same applies to an embodiment in the form of a knee prosthesis, which generally have very long shafts. The addition of molybdenum stabilizes what is known as the S-phase of the titanium alloy. This allows the formation 20 of the desired body-centered cubic crystal structure. Molybdenum as alloying element has a lower toxicity than other alloying elements which likewise stabilize the 8 phase, in particular niobium or vanadium. The reduction in the toxicity is an important benefit of a prosthesis 25 intended for long-term implantation. The level of the molybdenum or molybdenum equivalent in the alloy is in the range from 7.5 to 25%. The result of this, in particular in the case of a molybdenum content of at least 10%, is sufficient 2994169 91211 29g41691. (GHMater) P54243.AU - 6 stabilization of the S-phase all the way down to the room temperature range. The content is preferably between 12 and 16%. This allows a meta-stable 1-phase to be achieved by rapid cooling after casting. The mean grain size of the 5 crystal structure is at least 0.3 mm, preferably 0.5 mm. There is generally no need to add further alloy-forming elements. In particular, there is no need to add vanadium or aluminum. The elimination of these elements has the advantage, which has already been mentioned above, that it 10 is possible to avoid the toxicity emanating from these alloy-forming elements. The same applies to bismuth, the biocompatibility of which likewise does not match that of titanium. Furthermore, the titanium-molybdenum alloy has the advantage of having improved mold filling properties is compared to known alloys such as TiAl6V4. This makes it possible to form sharper-edged structures by the investment casting process. It has proven particularly suitable for at least the shaft of the prosthesis according to the invention to be hot 20 isostatically pressed and solution annealed. It has been found that considerable improvements with regard to brittleness are achieved with a material which has been heat-treated in this way. The hot isostatic pressing counteracts undesirable effects of concentrating the 25 molybdenum in dendrites while deflecting the remaining melt by dissolving inter-dendritic precipitations. A temperature below the 9-transus temperature, specifically at most 100 0 C below 15 the 9-transus temperature, is expedient. Temperatures in the range from 710 0 C to 760 0 C, 30 preferably of approx. 740 0 C, have proven suitable for a titanium-molybdenum alloy with a molybdenum content of 15%. The solution annealing improves the ductility of the 2994169 9/1211 2M16ieg1 (GHMatterS) P54243AU - 7 alloy. Temperatures of at least 7000C up to 8800C, preferably in the range from 8000C to 8600C, have proven suitable for this purpose. There is no need for a preliminary age-hardening before or after the hot 5 isostatic pressing. For cooling after the solution annealing, the shaft is expediently quenched with water. The invention is explained in more detail below with reference to the drawing, which illustrates an advantageous exemplary embodiment and in which: 10 Fig. 1 shows a diagrammatic view of a first exemplary embodiment of a joint prosthesis according to an embodiment of the invention; Fig. 2 shows a diagrammatic view of a further exemplary embodiment of a joint prosthesis according to 15 an embodiment of the invention; Fig. 3 shows an image of the crystal structure immediately after the investment casting (magnified 1000 times); Fig. 4 shows an image of the crystal structure after 20 hot isostatic pressing and solution annealing; and Fig. 5 shows a table giving mechanical properties of the prosthesis according to an embodiment of the invention. 25 The exemplary embodiment illustrated in Fig. 1 shows a femoral prosthesis for an artificial hip joint. The femoral prosthesis 1 consists of a 9-titanium alloy, 2994169 9/12/11 29N 9_ Ig (GHMaftm~) P64243 AU -8 namely TiMol5. This alloy has a body-centered cubic crystal structure at room temperature. The femoral prosthesis 1 is intended for implantation at the upper end of the femur. It can interact with an 5 acetabulum component 2 which has been implanted in the pelvic bone. The femoral prosthesis 1 has an elongate shaft 10 as bone anchoring element and a neck 11 which adjoins it at an obtuse angle. At its end remote from the shaft there is arranged a joint head 12 which, together 10 with a bearing insert 22 of the acetabulum component 2, forms a ball joint. Implantation involves complete or partial resection of the head of the thighbone neck, opening up access to the medullary cavity of the femur. This access is used to introduce the shaft 10 of the 15 femoral prosthesis 1 into the medullary cavity, where it is anchored. Depending on the particular embodiment, cement is provided as anchoring means or the fixing is effected without the use of cement. The femoral prosthesis 1 introduces mechanical loads 20 acting on the hip joint, whether static loads when standing or dynamic loads when walking, into the femur. Physiologically compatible transmission of loads is important for permanent reliable anchoring of the femoral prosthesis 1 in the bone material of the femur. If the 25 femoral prosthesis 1 is of very rigid design, it absorbs a considerable portion of the load, thereby relieving the load on the bone material in particular in the upper region of the femur. In the longer term, this leads to degeneration of the femur in this region. This leads to 30 the risk of the femoral prosthesis 1 coming loose and 2994169 9/12111 299418g1 (GHMatters) P64243.AU -9 ultimately of the prosthesis failing. To prevent this failure mode, it is known per se for the femoral prosthesis 1 to be of less rigid, i.e. more elastic with a physiologically favorable low modulus of elasticity 5 design. In particular the shaft 10 of the femoral prosthesis 1 is critical in this respect. In the cortical region, the bone material of the femur has a modulus of elasticity of approx. 20 000 to 25 000 N/mm 2 . According to the invention, the femoral prosthesis 1 has a modulus of 10 elasticity of approx. 60 000 N/mm 2 . This is a favorable modulus which is much lower than that of materials which are conventionally used, such as TiAl6V4. These materials have a modulus of elasticity of approx. 100 000 N/mm 2 or even 200 000 N/mm 2 in the case of cobalt-chromium alloys. is Embodiments of the invention allow simple production of even complex shapes by investment casting. For example, the femoral prosthesis 1 has a multiplicity of recesses and sawtooth-like projections on its shaft 10. These are used to improve anchoring of the femoral prosthesis 1 in 20 the femur, allowing cement-free implantation. A plurality of grooves 14 are provided running in the longitudinal direction of the shaft 10. They are arranged on both the anterior and posterior side of the shaft 10 but may also be provided on the lateral sides. A plurality of rows of 25 sawtooth projections 15 are provided in the upper region of the shaft 10. Furthermore, an encircling ring 13 is provided at the transition to the neck. It can be designed as a separate element, but the invention means that it may also be integral with the shaft 10 and neck 11. In 30 general, a single-piece design of the prosthesis is preferred, with the exception of exchangeable or optional attachment parts or wearing parts. Furthermore, a fixing 2994169 9/12/11 2994169_i (GHMatters) P64243.AU - 10 projection 16 is provided on the shaft 10 adjacent to the ring 13 to prevent rotation. Such complex shapes of joint prostheses can conventionally only be produced from TiAl6V4. However, this material has a different, less 5 favorable crystal structure and therefore an undesirably high modulus of elasticity. Embodiments of the invention can advantageously also be used for other types of joint prostheses. Fig. 2 illustrates a knee prosthesis 3 as a further exemplary 10 embodiment. It comprises a femur component 31 and a tibia component 30. The femur component 31 has a long shaft 33 as bone anchoring element. It is designed for implantation in the medullary cavity of the femur, which has been opened up by section of the natural knee joint. As in the is case of the femoral prosthesis, in this case too the problem of degeneration of the surrounding cortical structure occurs if the knee prosthesis 3, in particular its shaft 33, is made too rigid. The same applies to a shaft 32 of the tibia component 30. 20 The joint prosthesis according to an embodiment of the invention can also be used for other joints, for example at the elbow or the shoulder. The text which follows describes a way of carrying out an embodiment of the invention. 25 The starting material is a 8-titanium alloy with a molybdenum content of 15% (TiMol5). This alloy is commercially available in the form of small billets (ingots). 2994169 9112111 2g910_1 (GNMatlers) P5424.ALJ - 11 A first step involves investment casting of the parts of the hip prosthesis. A casting installation is provided for the purpose of melting and casting the TiMol5. The casting installation is preferably a cold-wall crucible vacuum 5 induction melting and casting installation. An installation of this type can reach the high temperatures which are required for reliable melting of TiMol5 for investment casting. The melting point of TiMol5 is 17700C plus a supplement of approx. 600C for reliable investment 10 casting. Overall, therefore, a temperature of 1830*C needs to be reached. The investment casting of the melt is then carried out by means of processes which are known per se, for example using wax cores and ceramic molds as lost mold. Investment casting techniques of this type are known 15 for the investment casting of TiAl6V4. The result is a body-centered cubic crystal structure. An image of the microstructure is illustrated in Fig. 3. The castings, from which the casting molds have been removed after the investment casting, are subjected to a 20 heat treatment. This involves hot isostatic pressing (HIP) at a temperature just below the 9-transus temperature. This temperature may be in the range from 7100C to 760 0 C and is preferably approximately 740 0 C at an argon pressure of 1100 to 1200 bar. It is expedient for this purpose for 25 a surface zone which may have formed during casting in the form of a hard, brittle layer (known as the a-case) to be removed by pickling. This layer is usually approx. 0.03 mm thick. Following the hot-isostatic pressing, the castings have 30 only a low ductility. It is assumed that this 29941699 (12/11 2M9169_1 (GHMattlrs) P54243 AU - 12 embrittlement is attributable to secondary precipitations during the hot isostatic pressing and the subsequent, generally slow cooling from the hot isostatic pressing temperature. 5 To dissolve these disruptive precipitations, the castings are annealed in a chamber furnace under argon shielding gas atmosphere. A temperature range from approx. 700 0 C to 860 0 C for a duration of several hours, generally two hours, is selected for this purpose. In this context, there is a 10 reciprocal relationship between the temperature and the duration; a shorter time is sufficient at higher temperatures, and vice versa. After the solution annealing, the castings are quenched using cold water. The resulting microstructure is illustrated in Fig. 4. is The mechanical properties achieved after solution annealing are reproduced in the table shown in Fig. 5. It can be seen that the modulus of elasticity drops as the temperature rises during the solution annealing, specifically down to levels of as low as 60 000 N/mm 2 . 20 The ductility values improve with decreasing strength and hardness. For example, after solution annealing for two hours at 800 0 C, the result is a modulus of elasticity of 60 000 N/mm 2 with an elongation at break of approx. 40% and a fracture strength Rm of approx. 25 730 N/mm 2 . It is to be understood that, if any prior art publication is referred to herein, such reference does not constitute 2994169 912911 299418991 (GHMSIICVS) P54243 AU - 13 an admission that the publication forms a part of the common general knowledge in the art, in Australia or any other country. 2994169 9/12/11 2994169_i (GHMatlers) P54243.AU

Claims

1. A joint prosthesis having a shaft made from a titanium molybdenum alloy having a molybdenum content in the range of 7.5 to 25%, 5 wherein at least the shaft is investment-cast and has a body centered cubic crystal structure, and wherein the modulus of elasticity of the shaft is 68 kW/mm 2 and 59.4 kW/mm 2 . 10

2. The joint prosthesis as claimed in claim 1, wherein the joint prosthesis is designed as a femoral prosthesis.

3. The joint prosthesis as claimed in claim 1, wherein 15 the joint prosthesis is designed as a knee prosthesis. 29941991211 2994I891 (GHMatlrn3) P84243.AL - 15

4. The joint prosthesis as claimed in any one of the preceding claims, characterized in that the mean grain size of the crystal structure is at 5 least 0.3 mm, preferably 0.5 mm.

5. The joint prosthesis as claimed in any one of the preceding claims, wherein at least the shaft is hot isostatically pressed and 10 solution annealed.

6. The joint prosthesis as claimed in claim 5, wherein the hot isostatic pressing takes place at a 15 temperature which is at most equal to a beta-transus temperature of the titanium alloy and is at most 100 0 C below the beta-transus temperature.

7. The joint prosthesis as claimed in any one of the preceding claims, 20 wherein the titanium alloy is free of vanadium and aluminum.

8. The joint prosthesis as claimed in any one of the preceding claims, wherein 25 the titanium alloy is free of bismuth. 294169_1 (GHMatters) P64243.AU - 16

9. A joint prosthesis substantially as herein described with reference to one or more of the drawings. 2994169 9/12/11 294189_1 (GHMatters) Pe4243.AU