Porous Structure Placement Configured For Manufacturing
20230131604 · 2023-04-27
Inventors
Cpc classification
A61F2002/3429
HUMAN NECESSITIES
A61F2002/3092
HUMAN NECESSITIES
A61F2/30942
HUMAN NECESSITIES
B33Y50/00
PERFORMING OPERATIONS; TRANSPORTING
B22F3/1115
PERFORMING OPERATIONS; TRANSPORTING
B22F10/28
PERFORMING OPERATIONS; TRANSPORTING
B33Y80/00
PERFORMING OPERATIONS; TRANSPORTING
B22F10/80
PERFORMING OPERATIONS; TRANSPORTING
A61F2002/30948
HUMAN NECESSITIES
International classification
Abstract
A computer-generated component file for fabricating an orthopedic implant is prepared. First and second select sections of an initial implant model of a computer-aided design model are set to first and second model porous sections. A remaining section of the initial implant model is left. All regions defining the first and the second select sections are spaced not more than a preset distance from a patient-specific bone model of the computer-aided design model as measured uniformly. The first and the second model porous sections are merged with a remaining section of the initial implant model to form at least a portion of a final implant model. The final implant model is stored in a component file configured to be accessed by a computer-aided manufacturing machine for use in fabricating the orthopedic implant. At least a portion of the orthopedic implant corresponds to the final implant model.
Claims
1. A method of preparing a computer-generated component file for fabricating an orthopedic implant comprising steps of: setting, via a computer processor, first and second select sections of an initial implant model of a computer-aided design model to first and second model porous sections and leaving a remaining section of the initial implant model, wherein all regions defining the first and the second select sections are spaced not more than a uniform preset distance from a patient-specific bone model of the computer-aided design model; merging, via the computer processor, the first and the second model porous sections with the remaining section of the initial implant model to form at least a portion of a final implant model of the computer-aided design model; and storing, via the computer processor, the final implant model in a component file configured to be accessed by a computer-aided manufacturing machine for use in fabricating the orthopedic implant, at least a portion of the orthopedic implant corresponding to the final implant model.
2. The method of claim 1, further comprising a step of removing, before the setting step and via the computer processor, the first and second select sections from the initial implant model, wherein the remaining section of the initial implant model remains following the removing step.
3. The method of claim 1, wherein the first and the second model porous sections have a first model porous thickness, further comprising a step of: setting, via the computer processor, a third select section of the initial implant model to a third model porous section, wherein all regions defining the third select section are spaced not more than the preset distance from the patient-specific bone model as measured uniformly, wherein first and second model implant thicknesses of the initial implant model taken along respective first and second lines through the first and the second select sections include at least a preset minimum model continuous solid thickness and a third model implant thickness of the initial implant model taken along a third line through the third select section includes less than the preset minimum model continuous solid thickness, the third model porous section having a second model porous thickness equal to a difference between the third model implant thickness and the preset minimum model continuous solid thickness when the third model implant thickness is greater than the preset minimum model continuous solid thickness or is otherwise zero, wherein the merging step comprises merging, via the computer processor, the third model porous section with the remaining section of the initial implant model to form at least the portion of the final implant model.
4. The method of claim 3, further comprising a step of removing, before the third select section setting step and via the computer processor, the third select section from the initial implant model.
5. The method of claim 2, further comprising a step of receiving, via the computer processor, an input instruction, wherein each of the removing, setting, and merging steps occur automatically in response to the input instruction.
6. The method of claim 1, wherein the first and the second select sections include first and second digital surfaces contacting the patient-specific bone model.
7. The method of claim 1, further comprising a step of removing from the select sections, before the setting step and via the computer processor, any regions of the initial implant model that are not within a porous thickness distance of any point on any surface of the initial implant model that is within an interface proximity of a bone model.
8. The method of claim 1, further comprising a step of extending, via the computer processor, the model porous sections beyond the initial implant model.
9. The method of claim 1, further comprising a step of setting, via the computer processor, a boundary region of the initial implant model, the boundary region being contiguous with one or more of the model porous sections as a region of gradient porosity.
10. The method of claim 1, further comprising a step of extending, via the computer processor, a model added thickness layer having a predetermined model thickness to a side of the initial implant model facing away from the bone model.
11. The method of claim 10, further comprising steps of: fabricating a component according to the final implant model; and removing at least some material from the component corresponding to the model added thickness layer to define at least a portion of the orthopedic implant.
12. The method of claim 1, wherein the first and the second select section setting step includes sending instructions, via the computer processor, to a computer-aided design model to associate a porosity with the first and the second model porous sections of the initial implant model.
13. A method of replacing a portion of a bone comprising steps of: removing one or more bone portions from one or more bones to leave, respectively, a remaining first bone portion or a remaining first plurality of bone portions; and placing an implant having a plurality of irregularly shaped porous portions and a plurality of irregularly shaped solid portions each separating at least portions of respective pairs of the plurality of irregularly shaped porous portions against only the respective remaining first bone portion or first plurality of bone portions such that none of the plurality of irregularly shaped porous portions includes a region located more than a preset distance from at least one bone portion of the respective remaining first bone portion or first plurality of bone portions, the irregularly shaped porous portions and the irregularly shaped solid portions defining all bone-facing surface portions of the implant.
14. A method of preparing a computer-generated component file for fabricating an orthopedic implant comprising steps of: forming, via a computer processor, a bone model of a first bone portion or a first plurality of bone portions; forming, via the computer processor, a first implant model with only porous regions and solid regions, all of the porous regions being formed only at locations of the first implant model within a preset distance from the bone model; and storing, via the computer processor, the first implant model in a component file configured to be accessed by a computer-aided manufacturing machine for use in fabricating the orthopedic implant, at least a portion of the orthopedic implant corresponding to the first implant model.
15. The method of claim 14, further comprising a step of extending a model added thickness layer of a predetermined thickness to a side of the initial implant model facing away from the bone model.
16. The method of claim 15, further comprising steps of fabricating a component according to the first implant model and machining away a first portion of the component corresponding to at least part of the model added thickness layer to expose a second portion of the component corresponding to at least one of the solid regions, the one or more of the solid regions corresponding to the second portion of the component being on the side of the initial implant model facing away from the bone model.
17. The method of claim 14, wherein the initial implant model forming step comprises steps of defining an axis extending through a surface facing the bone model and through the bone model and excluding the porous regions from any region a predefined distance away from the axis.
18. The method of claim 14, wherein the initial implant model forming step comprises a step of excluding the porous regions from any region at least a predefined distance away from the side of the initial implant model facing away from the bone model.
19. An orthopedic implant comprising: a first implant structure fabricated by an additive manufacturing machine using the computer-generated component file prepared using the method of claim 1, wherein the first implant structure corresponds to the final implant model and comprises porous portions corresponding to the model porous sections and a solid region corresponding to the remaining section of the initial implant model.
20. The orthopedic implant of claim 19, wherein all regions of the final implant model are within the preset distance from the bone model with the exceptions of i) regions surrounding digital holes corresponding to holes configured for receiving shafts of separate objects separate from the first implant structure and ii) regions within a minimum continuous solid thickness zone of the final implant model, the minimum continuous solid thickness zone having a boundary on a digital opposing surface of the final implant model opposite a digital bone-facing surface of the final implant model facing the bone model and having a thickness corresponding to a minimum continuous solid thickness preset within final implant model.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DETAILED DESCRIPTION
[0047] The present disclosure includes reference to processes carried out on a computer, with the illustrated example presenting steps carried out within a building application such as computer modeling or computer aided design (“CAD”) software, e.g., Ntopology, NX, Solidworks, or any substantial equivalent in which a user may interface with the building application as described, e.g., in U.S. Pat. No. 10,596,660, the disclosure of which is hereby incorporated herein by reference. However, any or all of the steps presented may optionally be carried out without any graphical presentation, particularly where such steps are carried out automatically by a computer. Any step or process in this disclosure or any combination thereof may, unless specified otherwise, be carried out by a human user of a computer carrying suitable CAD software, by a computing device having a processor and a non-transitory, computer readable medium carrying instructions that, when read by the processor, cause the processor to execute such steps or processes automatically, or by a human user in cooperation with such a computing device.
[0048] The computer-based design processes described herein can be used to create one or more manufacturing models that may be fabricated as physical products. Any fabrication method, including additive manufacturing, subtractive manufacturing, or a combination thereof, may be used as suitable for the size and shape of the output, meaning the final desired fabricated component, and the intended material or materials. An example includes using an additive manufacturing process as at least a first part of the fabrication process. In some arrangements, the additive manufacturing process may be, e.g., electron beam melting (“EBM”), selective laser sintering (“SLS”), selective laser melting (“SLM”), binder jetting, or blown powder fusion for use with metal powders.
[0049] When additive manufacturing by a PBF process such as EBM, SLM, or SLS, a first layer of metal powder is deposited onto a substrate and then scanned with a high energy beam so as to sinter or melt the powder and create a portion of one or more predetermined physical porous geometries. Successive layers of the metal powder are then deposited onto previous layers of the metal powder and also respectively scanned with the high energy beam prior to the deposition of subsequent layers of the metal powder. The scanning and depositing of successive layers of the metal powder continues the building process of the predetermined physical porous geometries. Such continuation of the building process refers not only to a continuation of a predetermined physical porous geometry from a previous layer but also a beginning of a new predetermined physical porous geometry as well as or instead of the completion of a predetermined physical porous geometry, depending on the desired characteristics of the structure or structures to be fabricated.
[0050] The structures formed using this process may be partially porous and, if desired, have interconnecting pores to provide an interconnecting porosity. In some arrangements, the physical porous geometries may be defined by physical struts connected at vertices corresponding to digitized nodes within a CAD or other modeling program. The powder and thus the additively printed porous portion or portions preferably may be made of any one or any combination of cobalt chrome alloy, titanium or alloy, stainless steel, niobium, tantalum, nitinol, zirconium, and magnesium. Additionally or in the alternative, polymers, including either or both or bioresorbable polymers and non-bioresorbable polymers may be used as additive manufacturing material. Thus, a mixture of desired mixed materials may be employed.
[0051] The high energy beam preferably may be an electron beam (e-beam) or laser beam and may be applied continuously to the powder or pulsed at a predetermined frequency. In some arrangements, the use of a laser or e-beam melting process may preclude the requirement for subsequent heat treatment of the structure fabricated by the additive manufacturing process, thereby preserving the initial mechanical properties of the additively manufactured porous portion. The high energy beam is emitted from a beam-generating apparatus to heat the metal powder sufficiently to sinter or at least partially melt the metal powder. High energy beam generation equipment for manufacturing such structures may be one of many currently available including the “Concept laser M2 Cusing” machines, GE Concept M2 Cusing Gen 2 machines, GE Arcam Q10 machines, 200W M2 Cusing (series 3), kW M2 Cusing (Series 3), Dual kW M2 Cusing (Series 5) MCP REALIZER, the EOS M270, TRUMPF TRUMAFORM 250, the ARCAM EBM S12 and Q10 machine, and the like. These machines are listed by way of example only. Thus, this list suggests what machines may have suitable capabilities for the processes described herein, but any other machines having similar capabilities may be used instead. The beam generation equipment may also be a custom-produced laboratory device.
[0052] The pore density, pore size and pore size distribution may be controlled from one location to another. It is important to note that successive powder layers may differ in porosity by varying factors used for high energy beam scanning of powder layers. Additionally, the porosity of successive layers of powder may be varied by either creating a specific type of unit cell or manipulating various dimensions of a given unit cell. In some arrangements, the porosity may be a gradient porosity throughout at least a portion of the fabricated structure. The beam generation equipment may be programmed to proceed in a random generated manner to produce an irregular porous construct but with a defined level of porosity. Pseudo-random geometries may be formed by applying a perturbation to the vertices of porous geometries when preparing model build structures corresponding to the 3D structure to be fabricated. In this manner, the shapes and sizes of the physical porous geometries may be randomized.
[0053] In some arrangements, additively manufactured porous structures may be in the form of overlapping lines of solidified powder as disclosed in U.S. Pat. No. 7,537,664, the disclosure of which is hereby incorporated by reference herein. In some arrangements, additively manufactured porous structures may be in the form of cellular structures defined by repeating formed porous geometries corresponding to digitized unit cells as disclosed in U.S. Pat. Nos. 10,525,688 and 9,180,010, the disclosures of which are hereby incorporated by reference herein. In some arrangements, additively manufactured porous structures may be in the form of a mesh or chainmail as disclosed in U.S. Pat. Nos. 10,596,660 and 10,888,362, the disclosure of which is hereby incorporated by reference herein as if fully set forth herein. In some arrangements, additively manufactured structures may be formed to have flanges in the manner as disclosed in U.S. Pat. No. 10,456,262, the disclosure of which is hereby incorporated by reference herein.
[0054] Referring now to
[0055] Scanned bone model 100 can be acquired in any way known for acquiring digital images of a bone within a patient's body, such as, for example, computerized tomography (“CT”) or magnetic resonance imaging (“MRI”). Bone model 100 may be initially acquired in a preoperative or post-operative state. If acquired preoperatively, bone model 100 may be manipulated as necessary to resemble a planned postoperative state in which the implant being designed is implanted upon the bone.
[0056] Initial implant model 108 is a digital model having a shape and dimensions of a physical implant being designed but, unless desired, does not include any representation of material or structural variations, such as differences in porosity, throughout the implant. Initial implant model 108 may be off-the-shelf or patient-specific. If patient-specific, initial implant model 108 may be constructed entirely or at least partially by reference to the patient's bone or bones, such as by conforming the initial implant model to a difference between the post-resection state of bone model 100 and either an ideal shape or a preoperative bone model. For example, if the bone from which bone model 100 was derived already had significant preoperative deformities, initial bone model 108 may be shaped according to a difference between the planned post-resection state of bone model 100 and a theoretical ideal shape.
[0057] With reference to
[0058] Body portion 110 typically represents a portion of the output that will have the implant's base material type such as, for example, titanium, cobalt chrome, stainless steel, or PEEK and structure, though special features or local variations may be manually added to the body portion at any time if desired, such as before, after, or between any of the steps described herein. Such base material may be any biocompatible material of sufficient strength and durability for the type of implant being designed, such as, variously, metals or metal alloys, with titanium, stainless steel, or Nitinol being some examples, ceramics, or polymers, with high-density polyethylene (“HDP”), polymethylmethacrylate (“PMMA”), or polyetheretherketone (“PEEK”) being some examples. Features of the implant being designed other than such features as represented by body portion 110 may be constructed of the same material as or of different material than the material of the body portion features, and may be of the same porosity or of differing porosity.
[0059] As shown in
[0060] Initial implant model 108 may be provided in a state already including holes corresponding to separate model components 114. Alternatively, initial implant model 108 may be provided without holes corresponding to separate model components 114, and such holes may be created within body portion 110.
[0061] At a modeling stage as illustrated in
[0062] As shown in
[0063] An interface side of body portion 110 may be identified before or after holes 118 are created. The interface side in the illustrated example is an upper side of body portion 110, referring to all surfaces of the body portion that would be visible in a plan view of the body portion from a perspective looking in downward direction 124. However, the interface side may be identified as surfaces facing in any direction, or any plurality of directions, relative to vertical reference 122 in other arrangements.
[0064] An interface side projection 126 is shown in
[0065] Referring now to
[0066] At the completion of the design process described herein, optimized model 150 (see
[0067] With reference to
[0068] A thickness of each location or zone of interface model 130 along a corresponding interface line 134 may be set for that location. At this stage, thickness of the interface model 130 is increased away from bone model 100, generally increasing a distance between points originally identified as part of the interface side of body portion 110 and the transition from the interface model to the body portion. Thus, as thickness of interface model 130 along interface lines 134 increases, thickness of body portion 110 reduces correspondingly.
[0069] Thickness added at each location of interface lines 134 may be uniform across interface model 130, to the extent that such thickness would not cause the interface model to extend below the location of any lower surfaces (which may be surfaces on the added thickness side 141 as discussed below) of body portion 110, or may vary across the interface model according to manual inputs or predefined patterns and gradients. The thickness may be added uniformly in all directions in some arrangements, only in directions along interface lines 134 in some other arrangements, only in directions normal to the interface lines in some other arrangements, or uniformly in other predefined directions in still some other arrangements. Where the thickness varies across interface model 130, such variance may be among the foregoing values or generally within the same range as the foregoing values. However, the thickness of interface model, and as a result, the depth of the osseointegrative region of the fabricated implant, may differ from the foregoing examples depending on such factors as physician's preference, feasibility of manufacture, and the portion of bone being replaced by the implant.
[0070] If an initial thickness in a direction parallel to vertical reference 122 was given to implant model 130 before the thickness created in directions parallel to interface lines 134, such initial thickness may be discarded when the normal thickness is added. Alternatively, the initial thickness may be retained in any areas not reached by the thickness created in directions parallel to interface lines 134.
[0071] Optionally, interface model 130 may be cut to omit any portions of the identified interface side that are unlikely to contact bone in the fabricated implant. Such omitted portions of the interface side may be either any portions that do not directly contact bone model 100 at the intended placement of the implant as represented by the arrangement of initial implant model 108 relative to the bone model as shown in
[0072] Additionally, a minimum vertical thickness of body portion 110 along the axis of vertical reference 122 may optionally be designated. As interface model 130 is thickened as described above, it may be prevented from extending to any area that would put the vertical thickness of body portion 110 at that location below the designated minimum vertical thickness of the body portion. If a thickness of body portion 110 was below the designated minimum vertical thickness at a given location before the creation of interface model 130, the interface model may be excluded from that location altogether.
[0073] With reference to
[0074] In the illustrated example, such cutting back is performed after holes 118 are placed in body portion 110 and interface model 130 is thickened along interface lines 134, but in other arrangements, the cutting back may occur before either or both of the definition of holes 118 and the thickening along interface lines 134.
[0075] As shown in
[0076] Boundary regions 131, 132 as shown in
[0077] Application of boundary regions 131, 132 is optional, and either one or both may be omitted or ignored. However, applied, an outer boundary region 131 is a volume adjacent to interface model 130 that does not intersect body portion 110. Modified interface model 130A may expand to fill outer boundary region 131 and become final interface model 130B such that the osseointegrative portion of the output corresponding to optimized model 150 (see
[0078] Where inner boundary region 132 is applied, the inner boundary region is a volume adjacent to modified interface model 130A that intersects body portion 110. Inner boundary region 132 may correspond to a transition area in the fabricated implant between the base material and structure of the implant and that of the osseointegrative portion. As such, portions of the output corresponding to inner boundary region 132 may be any type of structure that facilitates secure attachment of the osseointegrative portion. Where the osseointegrative portion is a porous structure, the portions of the output corresponding to inner boundary region 132 may have an intermediate or gradient porosity transitioning from the high porosity of the osseointegrative portion to a relatively lower or lack of porosity of the remainder of the implant. Thus, either one or both of inner boundary region 131 and outer boundary region 132 may be identified as second, third, fourth, or later porous portions and merged into interface model 130.
[0079] In the illustrated example, boundary regions 131, 132 are applied to modified interface model 130A as described above. However, in other examples, boundary regions 131, 132 may instead be applied to interface model 130, and the cutting back or exclusions applied to transition interface model 130 to modified interface model 130A may also be applied to boundary regions 131, 132 themselves or whatever features would be populated into boundary regions 131, 132.
[0080] Turning to
[0081] Referring now to
[0082] Added thickness model 140 has the potential to serve multiple purposes. Added thickness model 140 may be fabricated as additional material, optionally of the same, greater, or lesser porosity as the portions of the implant corresponding to body portion 110. Because added thickness model 140 is added to a lower surface of body portion 110, the additional material provided by the added thickness will act as a base upon which the implant itself may be built up. The portion of the output that corresponds to added thickness model 140 may therefore reinforce the implant as it is being constructed. Further, because added thickness model 140 represents excess material, all or some of which must be cut away to put the implant in a finished state, the material of the added thickness can compensate for the poor surface finish and fidelity common to undersides of parts fabricated according to certain additive manufacturing processes which may include or result in build direction issues, pore structure issues, and manufacturing distortion. By machining away the portion of the output that corresponds to added thickness model 140, either manually or by computer numerical control (“CNC”), the lower side of the fabricated implant may have a smoother surface finish than certain additive manufacturing processes are capable of producing on any side of a part. Added material corresponding to added thickness model 140 may therefore be machined away entirely, or may be machined at least out of any holes for separate model components 114 and articulating features such as acetabular socket 114. Here, articulating features refers generally to any features of the implant that will form a joint with another implant or a bone after the implant is placed in the patient's body. Articulating features therefore include sockets, any ball intended for a ball-and-socket joint, and any condyles.
[0083] Referring now to
[0084]
[0085]
[0086] At added thickness side identification step 224, which may occur after at least body portion 110 is received, surfaces of body portion 110 facing toward a direction from which support from sacrificial material may be advantageous during fabrication are designated as added thickness side 141 as described above with regard to
[0087] A separate model component clearance step 228 may be executed before, after, between, or during any of added thickness side identification step 224, added thickness modeling step 226, interface thickening step 216, and expansion step 218, but must be executed after added thickness side identification step 214. At separate model component clearance step 228, interface model 130, at whatever stage of development interface model 130 may be, is excluded from separate model components 114 by a predetermined distance as described above with regard to
[0088] Osseointegration optimization process 210 and structural optimization process 220 according to the illustrated example are somewhat mutually interdependent due to the effects each has on the outcome of the other. Local reinforcements may be added to body portion 110 to support osseointegrative features, and osseointegrative features of the model are excluded from areas where stronger structures are needed or where the osseointegrative features would present undue manufacturing difficulty. A design method having such interdependence between processes serving different considerations has the potential to result in implants that are satisfactory from both medical and engineering perspectives.
[0089] Osseointegration optimization process 210 and structural optimization process 220 may be integrated into a “digital thread” process 310 illustrated in
[0090] At an input step 314, the digital thread begins with three-dimensional models of an implant and a bone, such as initial implant model 108 and bone model 100 as illustrated in
[0091] Following input step 314, initial implant model 108 becomes body portion 110 and proceeds through an optimization stage 318. Optimization stage 318 includes osseointegration optimization process 210 and structural optimization process 220 and generally corresponds to the procedures described above with regard to
[0092] Optimized computer model 150 produced by optimization stage 318, which may be a body portion 110, final interface model 130B, and added thickness model 140 arranged as shown in
[0093] After the model is advanced for manufacturing at advancement step 334, the model may optionally pass through a modification step 338. During modification step 338, manual or automated adjustments to any geometry of the model are made for medical or manufacturing purposes as necessary. Adjustments during modification step 338 are typically, though not necessarily, relatively minor in nature. At the conclusion of modification step 338, or at the conclusion of advancement step 334 if modification step 338 is skipped, the model is finalized for manufacturing in finalizing step 342. Either one or both of the finalized digital model itself and an actual implant fabricated according to optimized model 150, which includes body 110, final interface model 130B, and added thickness model 140, may be used to create a new or updated surgical plan in planning step 346.
[0094] Although the concepts herein have 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 disclosure. 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 disclosure as defined by the appended claims.