Implant for bones or vertebrae with self-constrained flexibility
11583320 · 2023-02-21
Assignee
Inventors
Cpc classification
A61B17/80
HUMAN NECESSITIES
A61B17/7019
HUMAN NECESSITIES
A61B17/8085
HUMAN NECESSITIES
B22F2003/245
PERFORMING OPERATIONS; TRANSPORTING
B29K2071/00
PERFORMING OPERATIONS; TRANSPORTING
B29K2105/251
PERFORMING OPERATIONS; TRANSPORTING
B22F10/28
PERFORMING OPERATIONS; TRANSPORTING
B29K2871/00
PERFORMING OPERATIONS; TRANSPORTING
B22F2005/004
PERFORMING OPERATIONS; TRANSPORTING
B29K2995/0056
PERFORMING OPERATIONS; TRANSPORTING
B29L2031/7532
PERFORMING OPERATIONS; TRANSPORTING
B22F3/24
PERFORMING OPERATIONS; TRANSPORTING
Y02P10/25
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B29C64/153
PERFORMING OPERATIONS; TRANSPORTING
International classification
A61B17/86
HUMAN NECESSITIES
B22F5/10
PERFORMING OPERATIONS; TRANSPORTING
B29C64/153
PERFORMING OPERATIONS; TRANSPORTING
B22F3/24
PERFORMING OPERATIONS; TRANSPORTING
A61B17/80
HUMAN NECESSITIES
Abstract
An implant for the stabilization of bones or vertebrae is provided, the implant being a solid body including a longitudinal axis that defines a longitudinal direction and including a flexible section that has a surface and has a length in the longitudinal direction, the flexible section including at least one cavity located near the surface and having a width in the longitudinal direction that is smaller than the length of the flexible section, the at least one cavity being connected to the surface through at least one slit, and a width of the slit in the longitudinal direction being smaller than the width of the cavity.
Claims
1. An implant for the stabilization of bones or vertebrae, the implant having a longitudinal axis that extends through a center of the implant and that defines a longitudinal direction, the implant comprising: a flexible section having an outer surface, a cavity located near the outer surface and spaced apart from the longitudinal axis, and a slit that connects the cavity with the outer surface in a radial direction relative to the longitudinal axis, wherein a width of the slit in the longitudinal direction is less than a width of the cavity in the longitudinal direction; wherein the slit forms first opposing wall portions and the cavity forms second opposing wall portions that are located away from the slit, and wherein when a load is applied to the implant in a first direction transverse to the longitudinal axis, the implant is configured to be elastically flexed from a first configuration where the first opposing wall portions are spaced apart from one another and the second opposing wall portions are spaced apart from one another, to a second configuration where, at least on a first side of the implant opposite the application of the load, the first opposing wall portions abut one another such that the flexibility of the implant is limited by the closure of the slit, while a distance that the second opposing wall portions are spaced apart from one another is increased compared to the first configuration.
2. The implant of claim 1, wherein the slit and the cavity each extends continuously around the longitudinal axis from the first side of the implant to an opposite second side of the implant where the load is applied, and wherein when the implant is at the second configuration, on the second side of the implant, a distance that the first opposing wall portions are spaced apart from one another is increased compared to the first configuration, while the distance that the second opposing wall portions are spaced apart from one another is decreased compared to the first configuration.
3. The implant of claim 1, wherein the slit and the cavity on the first side of the implant are a first slit and a first cavity, and wherein a second slit and a second cavity arranged similarly to the first slit and the first cavity are located on an opposite second side of the implant where the load is applied, and wherein when the implant is at the second configuration, on the second side of the implant, a distance that the first opposing wall portions are spaced apart from one another is increased compared to the first configuration, while the distance that the second opposing wall portions are spaced apart from one another is decreased compared to the first configuration.
4. The implant of claim 1, wherein the implant has at least two stiffness zones in a load versus displacement curve, such that a stiffness of the implant is in a first stiffness zone when the implant is at the first configuration, and the stiffness of the implant is in a second stiffness zone that is higher than the first stiffness zone when the implant is at the second configuration and the load remains applied on the implant.
5. The implant of claim 4, wherein the cavity further forms third opposing wall portions separate from the first and second opposing wall portions, wherein both the first opposing wall portions abut one another and the third opposing wall portions abut one another when the stiffness of the implant is in the second stiffness zone, and wherein the stiffness of the implant is in a third stiffness zone that is between the first and second stiffness zones when only one of the first opposing wall portions or the third opposing wall portions abut one another.
6. The implant of claim 1, wherein the first opposing wall portions formed by the slit extend from the cavity to the outer surface in an interlocking manner.
7. The implant of claim 1, wherein the implant comprises a bone anchor.
8. The implant of claim 7, wherein the bone anchor comprises a bone screw with a bone thread, and wherein the slit extends along a root of the bone thread for at least one full turn of the bone thread.
9. The implant of claim 1, wherein the implant comprises a bone plate.
10. The implant of claim 1, wherein when a load is applied to the first side of the implant in a direction opposite the first direction, the implant is configured to be elastically flexed to a third configuration where, at least on the first side of the implant, the second opposing wall portions abut one another to limit the flexibility of the implant, while a distance that the first opposing wall portions are spaced apart from one another is increased compared to the first and second configurations.
11. The implant of claim 1, wherein the first opposing wall portions and the second opposing wall portions extend substantially transverse to the longitudinal axis.
12. The implant of claim 1, wherein in a cross-sectional plane including the longitudinal axis, the cavity has a substantially S-shape or inverted S-shape, with one end of the S-shape or the inverted S-Shape formed by the slit.
13. The implant of claim 1, wherein the cavity further forms third opposing wall portions that are separate from the first and second opposing wall portions and that are configured to abut one another when the implant is flexed from the first configuration towards the second configuration to further limit the flexibility of the implant.
14. The implant of claim 1, wherein the slit is located between the cavity and the outer surface in the radial direction.
15. An implant for the stabilization of bones or vertebrae, the implant having a longitudinal axis that defines a longitudinal direction, the implant comprising: a flexible section having an outer surface, a cavity located near the outer surface, and a slit that connects the cavity with the outer surface in a radial direction relative to the longitudinal axis, wherein a width of the slit in the longitudinal direction is less than a width of the cavity in the longitudinal direction; wherein when a load is applied to the implant in a first direction transverse to the longitudinal axis, the implant is configured to be elastically flexed from a first configuration where a stiffness of the implant is in a first stiffness zone to a second configuration where a first abutment increases the stiffness of the implant to a second stiffness zone, and to be further elastically flexed from the second configuration to a third configuration where a second abutment further increases the stiffness of the implant to a third stiffness zone.
16. The implant of claim 15, wherein one of the first or second abutments is between first opposing wall portions formed by the slit, and wherein the other one of the first or second abutments is between second opposing wall portions located away from the slit and formed by the cavity.
17. The implant of claim 16, wherein the slit and the cavity each extends continuously around the longitudinal axis from a first side of the implant to an opposite second side of the implant, and wherein when the load is applied to the second side, the first opposing wall portions formed by the slit are configured to abut one another on the first side while the second opposing wall portions formed by the cavity are configured to abut one another on the second side.
18. The implant of claim 16, wherein the slit and the cavity are formed at least on a first side of the implant, and wherein when the load is applied to an opposite second side of the implant, both the first opposing wall portions formed by the slit are configured to abut one another and the second opposing wall portions formed by the cavity are configured to abut one another on the first side.
19. The implant of claim 16, wherein the slit and the cavity are a first slit and a first cavity located on a first side of the implant, and wherein a second slit and a second cavity arranged similarly to the first slit and the first cavity are located on an opposite second side of the implant, and wherein when the load is applied to the second side, the first opposing wall portions formed by the first slit abut one another on the first side while the second opposing wall portions formed by the second cavity abut one another on the second side.
20. The implant of claim 15, wherein one of the first or second abutments is between first opposing wall portions formed by the slit that are configured to abut one another when a load is applied to the implant in the first direction, and wherein the cavity forms second opposing wall portions located away from the slit that are configured to abut one another when a load is applied to the implant in a direction opposite the first direction.
21. A method of manufacturing an implant for the stabilization of bones or vertebrae, the implant having a longitudinal axis that defines a longitudinal direction and comprising a flexible section having an outer surface, a cavity located near the outer surface, and a slit that connects the cavity with the outer surface in a radial direction relative to the longitudinal axis, wherein a width of the slit in the longitudinal direction is less than a width of the cavity in the longitudinal direction, and wherein when a load is applied to the implant in a first direction transverse to the longitudinal axis, the implant is configured to be elastically flexed from a first configuration where a stiffness of the implant is in a first stiffness zone to a second configuration where a first abutment increases the stiffness of the implant to a second stiffness zone, and to be further elastically flexed from the second configuration to a third configuration where a second abutment further increases the stiffness of the implant to a third stiffness zone, the method comprising: using an additive manufacturing process to form the implant in a layerwise manner; and forming the cavity in the implant during the additive manufacturing process.
22. The method of claim 21, further comprising forming the slit in the implant during the additive manufacturing process.
23. The method of claim 21, further comprising cutting the implant to form the slit between the cavity and the outer surface after the additive manufacturing process.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) Further features and advantages will become apparent from the description of some embodiments together with the accompanying drawings.
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DETAILED DESCRIPTION
(33) A first embodiment of the implant will be described with reference to
(34) The width w of the cavity 12 in the longitudinal direction is furthermore such that it is smaller than a thread pitch, i.e. the distance between the crests of the bone thread 11 in the longitudinal direction. As can be seen in particular in
(35) The slit 13 opens into the cavity 12 at a position that corresponds substantially to the center of the cavity 12 in a longitudinal direction. By this design, the helically-shaped cavity 12 exhibits a plurality of cavity portions in a cross-sectional view, as shown in
(36) The tip 30 of the bone screw may be a self-cutting tip. The self-cutting tip 30 comprises bone-thread free sections 31 that extend in a slightly twisted manner from the outermost portion of the tip 30 into the shank, thereby creating cutting edges 32. Furthermore, between the head 20 and the bone thread portion of the shank 10, there may be a neck portion 21. The head 20 shown in the embodiment is a spherically-segment shaped head 20 and comprises an engagement portion 22 for a tool.
(37) The bone screw 1, in an exemplary embodiment, is made from a biocompatible metal or a biocompatible metal or metal alloy such as stainless steel, titanium, or a nickel-titanium alloy. In particular, alloys having superelasticity such as Nitinol or superelastic β-titanuim alloys are suitable. The bone screw 1 can also be made from a biocompatible plastic material, such as, for example, from PEEK (polyetheretherketone).
(38) To obtain the monolithic, solid structure, the bone screw 1, in an exemplary embodiment, is manufactured using an additive manufacturing method, such as Selective Laser Sintering (SLS), Selective Laser Melting, or electron beam melting. With such a method, it is possible to fabricate the internal cavities 12 into the solid body and the slit 13 during the layer-wise build-up of the implant based on computer data defining the shape and size of the implant. When using Selective Laser Sintering or Selective Laser Melting, laser sinterable metals or metal alloys or laser sinterable plastic materials are used, for example, laser sinterable titanium powder or laser sinterable stainless steel powder or laser sinterable PEEK powder.
(39) In a modified method of manufacturing, the solid body with the internal cavities is made by an additive manufacturing method, in particular by SLS, while the slits remain still closed. Thereafter, the slits are cut using a conventional technique such as wire cutting.
(40) In use, when a force F that is directed transverse to the longitudinal axis L acts onto the bone screw 1, the bone screw 1 is flexible in a direction transverse to the longitudinal direction, as can be seen in
(41) Because the bone screw 1 is manufactured from a solid body and does not comprise a central longitudinal bore, the strength of the bone screw 1 may be greater than that of known flexible bone screws that comprise a spring element for providing the flexibility. This reduces a risk of failure due to cracking. Because the strength is increased, it may be possible to manufacture the bone screw 1 with a smaller core diameter compared to flexible implants with a hollow interior. Due to its structure, the implant has at least two stiffness zones in a load versus displacement curve. An initial lower stiffness due to the possible micro-motion, that resembles the stiffness of an implant with a smaller diameter and a subsequent higher stiffness that resembles the stiffness of an implant with a greater diameter. For example, a bone screw of a core diameter of X.sub.1, for example 7 mm, may have initially the lower stiffness of a bone screw with a core diameter of X.sub.2<X.sub.1, for example 3.5 mm, when the gaps are not yet closed, and may have subsequently upon further bending the greater stiffness of a bone screw with a core diameter of X.sub.1 when the slit is closed.
(42) The bone screw may be used, for example, as a pedicle screw. In this case, it can be connected to a receiving part to form a polyaxial or a monoplanar bone anchor. For the receiving part, all kinds of receiving parts can be used that allow to pivotably hold the head of the bone screw and connect the bone screw to a spinal stabilization rod. When the vertebrae move, transverse forces may act on the pedicle screw. Due to its flexibility, the pedicle screw can bend and thus prevent fracture of weak bone material.
(43) Further modifications of the embodiments described may be contemplated. For example, the bone screw is not limited to the embodiment shown. For example, the bone screw may have a non-self-cutting tip, and/or it may have a different head, such as a lens-shaped head or a disc-shaped head or any other head. It may even be provided without a head. The bone screw may also be used together with a bone plate.
(44) A second embodiment of the implant will be described with reference to
(45) The rod 100 may be manufactured through a manufacturing method as described above with respect to the bone screw 1, such as an additive manufacturing method, such as Selective Laser Sintering.
(46) The rod may be used to connect two bone anchoring devices, for example two pedicle screws screwed into the pedicles of adjacent vertebrae. Due to the flexible characteristics of the rod 100 based on the helically-shaped cavity 12 with the helically-shaped slit 13, the rod 100 permits a controlled motion of the adjacent vertebrae. The motion is limited by the self constrained flexibility of the rod 100.
(47) Referring to
(48) Referring to
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(50) A third embodiment of the implant will be described with reference to
(51) In the embodiment shown, a plurality of first cavities 120 is provided, and the first cavities 120 may extend along the width (e.g., the entire width) from one side to the opposite side of the bone plate 1000. The first cavities 120 are arranged near the lower surface 1002 and open into the lower surface 1002 through slits 130 as shown in
(52) As in the previous embodiments, the size, shape, number and position of the cavities 120, 121 and the slits 130 determine the flexible characteristics of the bone plate 1000. Hence, by selecting the appropriate design, position and number of the cavities, the bone plate can be rendered flexible according to specific requirements.
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(54) With the design according to
(55) Providing cavities 120 only on one side, for example near to the lower surface 1002 as shown in
(56) The bone plate 1000 may be manufactured using a conventional manufacturing process. That means, also the cavities and the slits can be manufactured using a conventional manufacturing process, such as electrical discharge machining (EDM). This is possible because the cavities have a straight configuration. Alternatively, or in addition, additive manufacturing methods, such as Selective Laser Sintering may be used also to manufacture the bone plate 1000.
(57) Also, for embodiments of the bone plate, the modified design of the cavities as shown in
(58) A fourth embodiment of the implant in the form of a bone screw 1′ will be described with reference to
(59) Following the slit 13, the cavity 12′ comprises a substantially L-shaped section 14, that has opposing wall portions 14a, 14b forming the bottom of the L-shape that are substantially parallel to the opposing wall portions 13a, 13b of the slit 13 in the cross-sectional view. The upper portion of the L-shaped section 14 that is adjacent to the slit 13 is connected to the slit 13. Seen as a whole, the slit 13 and the L-shaped section 14 of the cavity resemble a groove and a projection that engages the groove with a gap 14c between the bottom of the groove and the side walls of the groove on the one hand and the projection on the other hand. The gap 14c allows the projection to move within the groove. Following the L-shaped section 14, the cavity 12′ comprises a substantially straight section 15 that extends substantially parallel to the longitudinal axis L. A width of the substantially straight section 15 in the longitudinal direction may be smaller than a width ws of the slit 13. Finally, the straight section 15 extends to an end section 16 that has a substantially oval-shaped cross section with its long sides substantially perpendicular to the longitudinal axis L. Seen in the cross-sectional view as shown in
(60) Also, in this embodiment, a width of the cavity 12′ in the longitudinal direction is smaller than a length of the flexible section of the bone screw 1′.
(61) The opposing wall portions 13a, 13b of the slit 13 form first opposing surfaces and provide a first stop at the compression side P when they are abutting against each other when the bone screw is flexed, as described below. The opposing wall portions 14a, 14b of the L-shaped section 14 form second opposing surfaces that provide a second stop when they are abutting against each other when the bone screw experiences tensile strain on the tension side T. In the longitudinal direction, the end section 16 of the cavity 12′ may extend in the longitudinal direction until a position corresponding to a crest of the bone thread 11.
(62) By the helical design of the cavity 12′ as described above, the cavity 12′ exhibits a plurality of cavity portions in a cross-sectional view, as shown in
(63) The function of the bone screw 1′ in use will be described with reference to
(64) When a force F that is directed transverse to the longitudinal axis L acts onto the bone screw 1′, the bone screw 1′ is flexible in a direction transverse to the longitudinal direction.
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(66) A second stop is provided by the abutment of the opposing wall portions 14a, 14b on the cavity portion that opens to the tension side T as shown in
(67) The stiffness of the implant is controlled by the geometric design, such as the volume of the cavity portions, the width of the slit 13 and the distance between the opposing wall portions 14a, 14b. The first stop and the second stop provided by the abutting opposing wall portions 13a, 13b and 14a, 14b provide a self-constraining characteristic to the implant. Therefore, no external or separate part that provides a flexibility constraining effect is required.
(68) A fifth embodiment of the implant in the form of a stabilization rod 100′ will be described with reference to
(69) The rod may be manufactured through a manufacturing method as described above with respect to the rod 100, such as an additive manufacturing method, such as Selective Laser Sintering.
(70) In use, the shape of the cavity 12′ with the first opposing wall portions 13a, 13b and the second opposing wall portions 14a, 14b allows the rod to perform a constrained motion when a transverse load is applied.
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(72) The cavity 12′ according to the fourth and the fifth embodiment or the modified cavity 12″ may also be provided in a bone plate (not shown). The cavity 12′ or 12″ is arranged in the bone plate in a transverse direction and extends from one side to the other side similar to the cavity 120 in the bone plate 1000 shown in
(73) An implant according to a sixth embodiment in the form of a bone screw 1″ is shown in
(74) A seventh embodiment of an implant will be described with reference to
(75) The end portions 401 of the slits 400 may be drilled from the side of the tip into the shank in a longitudinal direction. Thereafter, the outer portions of the slits 400 that are open to the outer surface may be cut by, for example, wire cutting. Alternatively, the whole implant can be made by additive manufacturing, for example by Laser Sintering. In a third alternative, the implant with the cavities is formed by additive manufacturing and the slits are cut by wire cutting, for example.
(76) The slits can also be provided at a portion of the shank that is positioned apart from the tip. For example, the slits can start at a distance from the tip and end at a distance from the head. The position of the slits in the longitudinal direction may vary from one slit to another slit. In use, the slits 400 with the cavities 401 lead to a self-constrained torsional flexibility. When a torsional load acts on the implant, the slits 400 will be closed at a position along the shank where the torsional load becomes too large. This prevents further torsion of the implant.
(77) As in the previously described embodiments, the implant, due to its structure, has at least two stiffness zones in a load versus twisting curve, that is, an initial lower stiffness due to the possible micro-motion that resembles the torsional stiffness of an implant with a smaller diameter, and a subsequent higher torsional stiffness that resembles the torsional stiffness of an implant with a greater diameter. For example, a bone screw of a core diameter of X.sub.1, for example 7 mm, may have initially the lower torsional stiffness of a bone screw with a core diameter of X.sub.2<X.sub.1, for example 3.5 mm, when the slit is not yet closed, and may have subsequently upon further twisting the greater torsional stiffness of a bone screw with a core diameter of X.sub.1 when the slit is closed.
(78) The implant according to the seventh embodiment can also be a rod or any other implant that may experience torsional loads.
(79) Various other modifications of the embodiments can be contemplated. For example, the implants may be flexible along a length that corresponds only to a portion of the implant, wherein in this case a flexible section is defined by the presence of the cavities and the slits. The implant can also be realized through any bone anchor, with or without a threaded shank, such as a bone nail, for example.
(80) The slits need not have exactly parallel opposing surfaces. It suffices that an abutment takes place when the slit narrows, that prevents or constrains against further flexion.
(81) The interlocking structure of the slit 13′, 13″, as shown in
(82) Instead of the helix-shaped cavities and slits for the bone anchor and the rod, the at least one cavity and the at least one slit may be realized by several annular cavities with annular slits extending around the central axis. Also, the cavities with slits can be axial cavities with axial slits for any of the implants. The cavities with slits can also have interruptions along their length. Furthermore, the shape of the cavity, in particular the depth of the cavity, can vary along a length of the implant. For example, there can be a deep cavity on a first portion of the screw length, such as adjacent to the tip, and a shallow cavity along a second portion of the screw length.
(83) While the implants according to the embodiments shown have a straight shape, in particular in the longitudinal direction, the invention is not limited to implants having a straight shape. For example, the bone plate may have a curvature along its length and/or width and may be formed with an irregular outer contour. For example, a humerus plate may have such a curvature in at least a portion of its length. In addition, also curved rods, straight nails, and curved nails may be contemplated. If the implant has a curvature along at least a portion of its length, the longitudinal axis is defined as a curved central line extending through the implant along its length.
(84) A number of different embodiments are disclosed herein. It is to be appreciated that the different components or methods described with respect to one or more of the different embodiments can be mixed and matched to produce other different embodiments.