Dual modulus hip stem and method of making the same
11020232 · 2021-06-01
Assignee
Inventors
- John M. Armacost (Warsaw, IN, US)
- Ryan C. KEEFER (Warsaw, IN, US)
- Jeffrey A. McAnelly (Columbia City, IN, US)
Cpc classification
A61F2002/3092
HUMAN NECESSITIES
A61F2310/00029
HUMAN NECESSITIES
B23K1/0008
PERFORMING OPERATIONS; TRANSPORTING
A61F2002/3631
HUMAN NECESSITIES
A61F2310/00023
HUMAN NECESSITIES
A61F2002/30405
HUMAN NECESSITIES
B23K20/02
PERFORMING OPERATIONS; TRANSPORTING
Y10T29/49826
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
B23K20/002
PERFORMING OPERATIONS; TRANSPORTING
A61F2310/00407
HUMAN NECESSITIES
A61F2310/00413
HUMAN NECESSITIES
A61F2002/30014
HUMAN NECESSITIES
A61F2/3607
HUMAN NECESSITIES
International classification
B23K1/00
PERFORMING OPERATIONS; TRANSPORTING
B23K20/02
PERFORMING OPERATIONS; TRANSPORTING
B23K20/00
PERFORMING OPERATIONS; TRANSPORTING
Abstract
An orthopaedic prosthesis for use in a hip replacement surgery. The orthopaedic prosthesis includes a metallic foam shell and a metallic core. The metallic core includes a neck configured to receive a femoral head component and a stem extending through the metallic foam shell.
Claims
1. A method of manufacturing an orthopaedic prosthesis for a patient, comprising: producing a shed from a metallic foam material having a first elastic modulus, producing a stem core from a metallic material having a second elastic modulus greater than the first elastic modulus, the stem core including a neck configured to receive a femoral head component, a collar, and a stem body that extends from the collar to a distal tip, the stem body comprising a proximal segment that extends distally from the collar and a distal segment that extends distally from a distal end of the proximal segment to the distal tip, and securing the shell to the stem body such that (i) the shell completely encases the proximal segment of the stem body, (ii) the shell covers a lateral surface of the distal segment of the stem body from the distal end of the proximal segment through an area adjacent the distal tip, and (iii) a medial surface of the distal segment of the stem body from the distal end of the proximal segment through the area adjacent the distal Up is devoid of the shell.
2. The method of claim 1, wherein securing the shell to the stem body includes sintering the shell to the stem body.
3. The method of claim 1, wherein producing the shell from the metallic foam material includes: compressing the metallic foam material around the stem core, and machining the metallic foam material to form the shell.
4. The method of claim 1, wherein producing the shell from the metallic foam material includes: compressing the metallic foam material to form an outer geometry of the shell, and machining a channel in the metallic foam material sized to receive the stem core.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The detailed description particularly refers to the following figures, in which:
(2)
(3)
(4)
(5)
(6)
(7)
(8)
(9)
DETAILED DESCRIPTION OF THE DRAWINGS
(10) While the concepts of the present disclosure are susceptible to various modifications and alternative forms, specific exemplary embodiments thereof have been shown by way of example in the drawings and will herein be described in detail. It should be understood, however, that there is no intent to limit the concepts of the present disclosure to the particular forms disclosed, but on the contrary, the intention is to cover all modifications, equivalents, and alternatives falling within the spirit and scope of the invention as defined by the appended claims.
(11) Terms representing anatomical references, such as anterior, posterior, medial, lateral, superior, inferior, etcetera, may be used throughout the specification in reference to the orthopaedic implants or prostheses and surgical instruments described herein as well as in reference to the patient's natural anatomy. Such terms have well-understood meanings in both the study of anatomy and the field of orthopaedics. Use of such anatomical reference terms in the written description and claims is intended to be consistent with their well-understood meanings unless noted otherwise.
(12) Referring to
(13) The stem component 14 of the implant 10 includes a core 24 having a neck 26 configured to be coupled to the head component 12. In the illustrative embodiment, the neck 26 includes a plurality of external threads 28 that are configured to engage with a plurality of internal threads (not shown) lining the aperture 22 of the head component 12. It should be appreciated that in other embodiments the neck and the head component may be configured to be press fit, taper fit, or secured together by other fastening means.
(14) As shown in
(15) The stem core 24 is formed from an implant grade metallic material having a high tensile strength and a high elastic modulus (i.e., a high material stiffness). As used herein, the term “high tensile strength” refers to a tensile strength that is greater than 650 MPa. Additionally, as used herein, the term “high elastic modulus” refers to an elastic modulus or modulus of elasticity that is greater than or equal to 100 GPa. In the illustrative embodiment, the core 24 is formed from cobalt-chromium alloy (“CoCr”) having a minimum ultimate tensile strength of 650 MPa and an elastic modulus of approximately 195 GPa. It should be appreciated that in other embodiments the core 24 may be formed from any material having a high tensile strength and a high elastic modulus, including, for example, a titanium alloy such as Ti-6A1-4V, which has a minimum ultimate tensile strength of 750 MPa and an elastic modulus of approximately 105 GPa.
(16) As described above, the core 24 of the stem component 14 includes a core body 32, which lies generally in the coronal plane of a patient's body when the implant 10 is secured to the patient's femur. As shown in
(17) In the illustrative embodiment, the medial surface 38 of the core body 32 is convex. As described in greater detail below, the medial surface 38 is defined by a radius 46 (see
(18) Returning to
(19) The shell 50 of the stem component 14 is formed from a metallic foam matrix having a low elastic modulus. As used herein, a “low elastic modulus” refers to an elastic modulus or modulus of elasticity similar to that of a patient's natural femur (i.e., between 10 GPa and 20 GPa). In the illustrative embodiment, the shell 50 is formed from a foam matrix of titanium having an elastic modulus of approximately 10 GPa and an ultimate tensile strength of the foam matrix of titanium is approximately 35 MPa. In that way, the shell 50 has an elastic modulus that is closer to that of a patient's femur. It should be appreciated that in other embodiments the shell 50 may be formed any metallic foam matrix having a low elastic modulus, such as, for example, a CoCr foam matrix having an elastic modulus of approximately 19 GPa, a CoCr alloy foam matrix, a titanium foam alloy matrix, or other foam matrix.
(20) As described above, the core 24 of the stem component 14 in the illustrative embodiment is formed from CoCr having an elastic modulus of approximately 195 GPa while the shell 50 is formed from a foam matrix of titanium having an elastic modulus of approximately 10 GPa. Thus, in the illustrative embodiment, the elastic modulus of the shell 50 is approximately 1/20 of the elastic modulus of the core 24. In still other embodiments, the core may be formed from CoCr having an elastic modulus of approximately 195 GPa and the shell may be formed from a CoCr foam matrix having an elastic modulus of approximately 19 GPa. In such embodiments, the elastic modulus of the shell is approximately 1/10 of the elastic modulus of the core. In other embodiments, the core may be formed from Ti-6 Al-4V having an elastic modulus of approximately 105 GPa and the shell may be formed from a titanium foam matrix having an elastic modulus of approximately 10 GPa. In such embodiments, the elastic modulus of the shell is approximately 1/10 of the elastic modulus of the core.
(21) As shown in
(22) As shown in
(23) The core body 32 (i.e., the core segments 64, 66) and the shell 50 (i.e., the sheath 52 and cover layer 58) cooperate to define a longitudinal axis 72 of the stem component 14, which extends between the proximal end 34 and the distal end 36. The core body 32 has a longitudinal axis 74 that is defined between the ends 34, 36, and the axis 74 is offset from the axis 72. In the illustrative embodiment, the axis 74 is offset in the medial direction from the axis 72 such that the core body 32 is biased toward the medial side 80 of the stem component 14 and away from the lateral side 82 of the stem component 14. Additionally, the thickness of the shell 50 on the lateral side 82 of the stem component 14 is greater than the thickness of the shell 50 on the medial side 80 of the stem component 14.
(24) For example, as shown in
(25) As shown in
(26) As shown in
(27) As shown in
(28) Returning to
(29) The core segment 66 has a medial surface 134 that forms a distal section of the medial surface 38 of the core body 32. The core segment 66 also has a lateral surface 136 that forms a distal section of the lateral surface 40 of the core body 32. As shown in
(30) As shown in
(31) As shown in
(32) In use, the implant 10 is inserted into a proximal end of a patient's surgically-prepared femur. The elongated stem component 14 is received in the intramedullary canal and the sheath 52 and the cover layer 58 of the shell 50 engage the portion of the patient's femur surrounding the canal. The core 24 is sized and shaped to meet the minimum strength requirements of the implant 10, while the shell 50 is configured to possess the external geometry necessary to fit into the intramedullary canal. The combination of the high tensile strength/high elastic modulus core 24 with the low modulus shell 50 results in a reduced stiffness for the implant 10 such that stress shielding of the patient's bone is reduced.
(33) Referring now to
(34) In block 210, the performance requirements of the stem component 14 are determined. The performance requirements for the stem component 14 may vary between different patients such that a customized stem component 14 may be required. The performance requirements include the external geometry and the minimum endurance and performance requirements, such as, for example, the minimum tensile strength and the minimum stiffness of the stem component 14.
(35) In block 212, the core 24 of the stem component 14 is selected. The core 24 may be an off-the-shelf, generic core that may be used with multiple implant sizes. The core 24 may be a customized, patient-specific component designed to satisfy the performance requirements of a particular patient. Whether the core 24 is generic or custom, the selected core 24 of the component 14 is sized and shaped to provide the minimum strength of the implant 10. The minimum strength of the core 24 is determined in accordance with International Organization for Standardization Standard No. 7206-4:2010 “IMPLANTS FOR SURGERY—PARTIAL AND TOTAL HIP JOINT PROSTHESES—PART 4: DETERMINATION OF ENDURANCE PROPERTIES AND PERFORMANCE OF STEMMED FEMORAL COMPONENTS” and Standard No. 7206-6:1992 “IMPLANTS FOR SURGERY—PARTIAL AND TOTAL HIP JOINT PROSTHESES—PART 6: DETERMINATION OF ENDURANCE PROPERTIES OF HEAD AND NECK REGION OF STEMMED FEMORAL COMPONENTS.”
(36) In block 214, the stem component 14 is assembled. To do so, a metallic foam matrix, which will form the shell 50 of the stem component 14, is procured. The metallic foam matrix may be compressed around the core 24 such that the core 24 is received in a channel within the foam matrix. The foam matrix may then be machined to the required external geometry of the shell 50. Alternatively, the metallic foam matrix may be compressed separately into the shape of shell 50. After the matrix is compressed, a channel sized to receive the core 24 may be machined in the shell 50 before the shell 50 is assembled with the core 24.
(37) A sintering operation may be used to secure the shell 50 to the core 24. It should also be appreciated that the shell 50 and the core 24 may be secured via a brazing operation, a press-fit, or other securing means.
(38) While the disclosure has been illustrated and described in detail in the drawings and foregoing description, such an illustration and description is to be considered as exemplary and not restrictive in character, it being understood that only illustrative embodiments have been shown and described and that all changes and modifications that come within the spirit of the disclosure are desired to be protected.
(39) There are a plurality of advantages of the present disclosure arising from the various features of the method, apparatus, and system described herein. It will be noted that alternative embodiments of the method, apparatus, and system of the present disclosure may not include all of the features described yet still benefit from at least some of the advantages of such features. Those of ordinary skill in the art may readily devise their own implementations of the method, apparatus, and system that incorporate one or more of the features of the present invention and fall within the spirit and scope of the present disclosure as defined by the appended claims.