Partially Porous Tibial Component
20230132015 · 2023-04-27
Inventors
- Aiguo Wang (Wayne, NJ)
- Matthew P. Poggie (Montclair, NJ, US)
- Nicholas Nai Guang Dong (Little Falls, NJ, US)
Cpc classification
A61F2002/3092
HUMAN NECESSITIES
A61F2/30767
HUMAN NECESSITIES
A61F2/30749
HUMAN NECESSITIES
A61F2/30907
HUMAN NECESSITIES
A61F2002/30878
HUMAN NECESSITIES
A61F2002/30884
HUMAN NECESSITIES
International classification
Abstract
A method for removing a stem portion of an orthopedic implant from a bone comprises exposing an implanted orthopedic implant having a body portion, a stem portion interconnected to the body and a porous metal section forming an interconnection between the body and the stem portion. A cutting tool is mounted on a holder connected to an exposed surface of the orthopedic implant. The porous section is aligned with the cutting tool mounted on the holder. The entire porous section is cut by moving the cutting tool therethrough in a direction transverse to the stem portion axis. The implant body portion is then removed and then the stem portion is removed from the bone. The cutting tool may be a saw or chisel which may be mounted on a guide fixed to the body portion.
Claims
16. A tibial implant comprising: a baseplate; a keel extending from the baseplate in a first direction; and a plurality of pegs each extending from the baseplate in the first direction and each having a first section adjacent to the baseplate, a second section extending from the first section, and a free end extending from the second section, wherein the first section of each of the pegs has a porous outer surface, wherein the second section of each of the pegs has a solid outer surface, and wherein the free end of each of the pegs tapers to a point.
17. The tibial implant of claim 16, wherein each of the pegs includes an edge along which the second section intersects the free end.
18. The tibial implant of claim 16, wherein the keel includes a pair of flanges defining intersecting first and second planes and an additional flange defining a third plane bisecting the keel, wherein either one of or both the first plane extends between a first pair of the pegs and the second plane extends between a second pair of the pegs, and wherein the first pair of the pegs lie on a first side of the third plane and the second pair of the pegs lie on a second side of the third plane.
19. The tibial implant of claim 16, wherein the keel includes a proximal keel portion adjacent to the baseplate and a distal keel portion extending from the proximal keel portion, and wherein the proximal keel portion includes a porous outer surface and the distal keel portion is solid.
20. The tibial implant of claim 16, wherein each of the pegs has a non-circular cross-section.
21. The tibial implant of claim 16, wherein the baseplate includes a solid baseplate portion and a porous baseplate portion extending from the solid baseplate portion in the first direction and extending to an outer rim of the solid baseplate portion in directions transverse to the first direction, wherein the keel has a non-circular keel cross-section at a portion of the keel adjacent to the baseplate, wherein each of the pegs has a non-circular peg cross-section at a portion of each of the respective pegs adjacent to the baseplate, and wherein the porous baseplate portion abuts the non-circular keel cross-section and the non-circular peg cross-sections.
22. The tibial implant of claim 16, wherein the second section has a uniform cross-section along a thickness of the second section.
23. The tibial implant of claim 16, wherein outer diameters of the first section and the second section are aligned.
24. The tibial implant of claim 16, wherein the porous outer surface is produced by additive manufacturing and thereby has a randomized pore structure.
25. The tibial implant of claim 16, wherein each of the pegs defines a longitudinal axis passing through its respective point.
26. The tibial implant of claim 16, wherein both the second end and the free end of each of the pegs are solid.
27. The tibial implant of claim 16, wherein the first section includes a solid core, and wherein the porous outer surface of the first section surrounds the solid core.
28. An orthopedic implant kit comprising: the tibial implant of claim 16; and a femoral component.
29. A tibial implant comprising: a baseplate including a solid baseplate portion and a porous baseplate portion extending from the solid baseplate portion in a first direction and extending to an outer rim of the solid baseplate portion in directions transverse to the first direction; a keel extending from the porous baseplate portion in the first direction and including a pair of flanges defining intersecting first and second planes and an additional flange defining a third plane bisecting the keel; and a plurality of pegs each extending from the porous baseplate portion in the first direction and each having a first section adjacent to the baseplate, a second section extending from the first section, and a free end extending from the second section, wherein either one of or both the first plane extends between a first pair of the pegs and the second plane extends between a second pair of the pegs, wherein the first pair of the pegs lie on a first side of the third plane and the second pair of the pegs lie on a second side of the third plane, wherein the first section of each of the pegs has a porous outer surface, wherein the second section of each of the pegs has a solid outer surface, and wherein the free end of each of the pegs tapers to a point.
30. The tibial implant of claim 29, wherein each of the pegs includes an edge along which the second section intersects the free end.
31. The tibial implant of claim 29, wherein the keel includes a proximal keel portion adjacent to the baseplate and a distal keel portion extending from the proximal keel portion, and wherein the proximal keel portion includes a porous outer surface and the distal keel portion is solid.
32. The tibial implant of claim 29, wherein each of the pegs has a non-circular cross-section.
33. The tibial implant of claim 32, wherein the porous baseplate portion abuts the flanges of the keel and the non-circular cross-sections of the pegs.
34. The tibial implant of claim 29, wherein the second section has a uniform cross-section.
35. The tibial implant of claim 29, wherein the porous baseplate portion and the porous outer surface are produced by additive manufacturing and thereby have randomized pore structures.
36. A tibial implant comprising: a baseplate including a solid bearing support portion and a porous bone-contacting portion extending from the bearing support portion, the porous bone-contacting portion having pore structures of differing shapes; a keel including a pair of flanges extending from the baseplate and defining intersecting planes and further including an additional flange extending away from the pair of flanges within a bisecting plane bisecting the keel; and four spikes extending away from the bone-contacting portion of the baseplate at locations spaced about the keel, each of the spikes having a non-tapering section and a tapering section extending from the non-tapering section and tapering to a point, wherein the non-tapering sections of each of the spikes includes a porous outer surface adjacent the bone-contacting portion of the baseplate and the tapering sections of each of the spikes are solid, wherein a first pair of the spikes extend away from a first side of the bone-contacting portion of the baseplate and a second pair of the spikes extend away from a second side of the bone-contacting portion opposite the first side of the bone-contacting portion of the baseplate, the first and the second sides defining the entirety of the bone-contacting portion of the baseplate, and wherein the first pair of the spikes is spaced apart a greater distance than the second pair of the spikes.
37. The tibial implant of 36, wherein the first pair of the spikes lie on one side of a transverse plane transverse to the bisecting plane and the second pair of the spikes lie on the opposite side of the transverse plane.
38. The tibial implant of claim 36, wherein each of the spikes includes four free ends and four filets, each of the free ends being connected to two adjacent ones of the free ends by respective ones of the filets, and wherein the free ends taper towards the point.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DETAILED DESCRIPTION
[0061] Referring to
[0062] Plate 12 may be either solid or porous to allow bone ingrowth upon implantation of the tibial component bone connecting surface 14. As shown in
[0063] Referring to
[0064] Referring to
[0065] As shown, keel 16 and baseplate 12 have solid struts 26, which connect these two parts, two of which are shown in
[0066] Referring to
[0067] Referring to
[0068] Referring to
[0069] Referring to
[0070] Referring to
[0071] Referring to
[0072] Referring to
[0073] Referring to
[0074] The tibial component 10, 100, and 300 of the present invention as well as femoral component 400 and patella 500 are made at least in part by forming solid, porous and partially porous metallic structures. The method makes use of SLM laser technology by employing a variety of scanning strategies. Typical metal and metal alloys employed include stainless steel, cobalt chromium alloys, titanium and its alloys, tantalum and niobium, all of which have been used in medical device applications. This method can be used for medical device applications such as in the tibia where bone and soft tissue interlock with the tibial component is required, or where a controlled structure is required to more closely match the mechanical properties of the device with surrounding tissue.
[0075] The method produces a three-dimensional structure using a laser remelting process, for example, for building structures utilizing unit cells onto a premade solid tibial baseplate 12. When applied to a tibial component, the three-dimensional structure is used to provide porous spacer area 22 between the baseplate and a stem or keel 16. Keel 16 is preferably solid and is formed by the same laser remelting or fusion process as the porous spacer area 22. Thus a tibial component can be made by building porous spacer 22/solid keel 16 on premade baseplate 12 during a continuous operation to form a bone ingrowth structure and a solid keel or stem portion or a keel or stem with a solid surface and a porous core. The preferred materials used for both the baseplate and stem are titanium, cobalt chrome and tantalum but both stainless steel and niobium can also be used as well as any other suitable material. The tibial component 10 may be built from any of these materials, with the preferred material being titanium (Ti). The described method can be exploited on a commercial basis for the production of, for example, bone interlock surfaces on a device although it has many other uses.
[0076] According to the preferred method of forming a three-dimensional structure includes building the shape by laser melting powdered Ti and its alloys, stainless steel, cobalt chrome alloys, Ta or Nb using a continuous or pulsed laser beam. Individual layers of metal are scanned using a laser. Each layer or portion of a layer is scanned to create a portion of a plurality of predetermined unit cells, as will be described below. Successive layers are deposited onto previous layers and also may be scanned. The scanning and depositing of successive layers continues the building process of the predetermined unit cells. As disclosed herein, by continuing the building process refers not only to a continuation of a unit cell from a previous layer but also a beginning of a new unit cell as well as the completion of a unit cell.
[0077] The method can be performed so that the structure is either porous or solid and, if porous, the pores can be interconnecting to provide an interconnected porosity.
[0078] The method includes using a tibial baseplate of cobalt chrome alloy, titanium or alloy, stainless steel, niobium and tantalum, on which to build the porous layer of any one of the aforementioned metals and alloys by laser melting using a continuous or pulsed laser beam. Thus, a mixture of desired mixed materials can be employed.
[0079] The method includes a laser melting process which precludes the requirement for subsequent heat treatment of the structure, thereby preserving the initial mechanical properties of the baseplate metal. The equipment used for the manufacture of such a device could be one of many currently available including the MCP Realiszer, the EOS M270, Trumpf Trumaform 250, the Arcam EBM S12 and the like. The laser may also be a custom produced laboratory device.
[0080] The pore density, pore size and pore size distribution of the porous spacer area can be controlled (varied) from one location on the structure to another. It is important to note that successive powder layers can differ in porosity by varying factors used for laser scanning powder layers. Additionally, the porosity of successive layers of powder can be varied by either creating a specific type of unit cell or manipulating various dimensions of a given unit cell.
[0081] It will be appreciated that this method can, therefore, be used to produce article from the metals referred to which can be created to a desired shape and which may or may not require subsequent machining. Yet again, such an article can be produced so that it has a graded porosity of, e.g., non-porous through various degrees of porosity to the outer surface layer. Such articles could be surgical prostheses, parts or any other article to which this method of production would be advantageous.
[0082] To produce a porous spacer area structure, the nature of the material formed as a result of laser melting of powdered beads is principally dependent on the thermal profile involved (heating rate, soaking time, cooling rate); the condition of the raw material (size and size distribution of powder particles); and atmospheric conditions (reducing, inert or oxidizing chamber gas).
[0083] There have been a number of studies to determine the optimum pore structure for maximization of bone ingrowth on prostheses. The general findings suggest that optimum porosity is between approximately 20% and 40%, and aim to mid value with a mean volume percent of voids of about 70%. The preferred pore structure is interconnected, with a minimum pore size between about 80 μm and 100 μm and a maximum pore size between 80 μm and 800 μm. The structured thickness for ingrowth is 1.4-1.6mm, but can be larger or smaller depending on the application.
[0084] In the present method the porous spacer structure is built in the form of a plurality of unit cells. Many designs of unit cells are possible to give the shape, type, degree, and size of porosity required. Such unit cell designs can be dodecahedral, octahedral, diamond, as well as many other various shapes. Additionally, besides regular geometric shapes as discussed above the unit cells of the present invention may be configured to have irregular shapes where various sides and dimensions have little if any repeating sequences. The unit cells can be configured to constructs that closely mimic the structure of trabecular bone for instance. Unit cells can be space filling, all the space within a three-dimensional object is filled with cells, or interconnected where there may be some space left between cells but the cells are connected together by their edges.
[0085] The cells can be distributed within the construct a number of ways. Firstly, they may be made into a block within a computer automated design system where the dimensions correspond to the extent of the solid geometry. This block can then be intersected with the geometry representing the component to produce a porous cellular representation of the geometry. Secondly, the cells may be deformed so as to drape over an object thus allowing the cells to follow the surface of the geometry. Thirdly, the cells can be populated through the geometry following the contours of any selected surface.
[0086] The unit cell can be open or complete at the surface of the construct to produce a desired effect. For instance, open cells with truncated lattice struts produce a surface with a porosity and impart the surface with some degree of barb.
[0087] Modifying the lattice strut dimensions can control the mechanical strength of the unit cell. This modification can be in a number of key areas. The lattice strut can be adjusted by careful selection of build parameters or specifically by changing the design of the cross-section of each strut. The density of the lattice can similarly be adjusted by modification of the density of the unit cells as can the extent and shape of porosity or a combination thereof. Clearly the overall design of the unit cell will also have a significant effect of the structural performance of the lattice. For instance, dodecahedral unit cells have a different mechanical performance when compared to a tetrahedral (diamond) structure.
[0088] The two key parameters used to define the relations regarding height, surface area, space height, volume of tetrahedron, and the dihedral angle of a tetrahedron are the strand length of the tetrahedron and, i.e., the diameter or height and width, cross section area of the strand, i.e., strut. These two parameters control the pore size and porosity of the structure. The parameter editor and relation editor within a typical CAD system can be used to control these parameters. Hence, by changing the parameters one can change the fundamental properties of the porous structure. The diamond or octahedral structure may have a circular cross-section strands or square cross-section strands.
[0089] A diamond or octahedral lattice structure can be made with and without laser beam compensation. Laser beam compensation essentially allows the diameter of the beam to be taken into account. Without it the constructed geometry is one beam diameter too wide as the beam traces out the contour of the particular section being grown. When laser beam compensation is utilized, the contour is offset half a beam diameter all around the constructed geometry which is represented in the CAD file. Although various parameters may be used, the parameters employed to create the porous ingrowth spacer include a laser power of 90-100 watts with an exposure time of 1,000 μsec from a point distance of about μm.
[0090] As shown in
[0091] In a method of use, a CAD model of the truncated octahedron is constructed using the sweep feature and calculations of between 10 and 1000 um and dimensions are incorporated using basic trigonometry. To tessellate the unit cell, the unit cell is first reoriented to enable easy tessellation and to reduce the number of horizontal struts in the model. Further, the model can be modified to remove all of the horizontal struts as shown in
EXAMPLE
[0092] The following is a method for making a partially porous implant and porous area by near-net shape building of a modular tibial tray component 10 of
[0093] A solid (non-porous) tray preform (e.g., forging) is partially or entirely machined to the final implant shape for example a tibial baseplate.
[0094] A layer-by-layer (additive manufacturing) direct build onto the solid tray preform 12 (e.g., Selective Laser Melting-SLM).
[0095] The construct is a hybrid SLM-built structure that is a combination of (a) porous SLM with a preferred porosity between 4-80% and a pore size in the range of 10 μm to 1000 μm, in which 100-400 μm is preferred for bone ingrowth and a “fully dense” SLM-built material that is less than 20% porous. This porous structure 22 is between 1 and 5 mm thick followed by a solid keel section 16. Both structures 16 and 22 may have a v-shape.
[0096] The SLM-built structure consists of a fully porous area 22 and a bone fixation keel 16, extending from the metaphyseal seating surface 14 of an orthopedic implant (such as tibial component 10) comprised of a porous portion adjacent to the metaphyseal porous seating surface and a fully dense portion extending to the diaphysis. Additionally, the fully dense keel portion 16 may be another hybrid structure where the center may be porous to reduce implant stiffness.
[0097] The SLM-built structure and the substrate the SLM-built structure is built onto are both integral parts of the implant. There is not removal of the SLM-built structure from the substrate (no EDM). That is, the fixturing for the additive manufacture process (SML) is part of the implant.
[0098] The SLM process uses only localized heating and, therefore, there is little to no affect from the heat on the underlying substrate mechanical properties. Further details of this manufacturing process are described in commonly owned U.S. patents and applications 2006/0147332, 2007/0142914, 2008/0004709, 2010/0010638, 2010/0291286, 2011/0014081, and U.S. Pat. No. 7,537,664, all the disclosures of which are incorporated herein by reference.
[0099] Although the invention herein has been described with reference to particular embodiments, it is to be understood that these embodiments are merely illustrative of the principles and applications of the present invention. It is therefore to be understood that numerous modifications may be made to the illustrative embodiments and that other arrangements may be devised without departing from the spirit and scope of the present invention as defined by the appended claims. [0100] 1-15. (canceled)