Bone substitute for training and testing and method for making

Abstract
A bone substitute that drills and cuts like bone for use in training and testing comprising an inner core of a foamable polymer or other soft material and an outer shell of a polymer such as an epoxy resin with a particulate filler such as aluminum oxide or silicon carbide added thereto together with, in some cases, titanium oxide to form a slurry for casting or molding around the inner core. Also provided is a method for making the bone substitute.
Description




BACKGROUND OF THE INVENTION




The invention relates in general to substitutes for bone, and, in particular, to a bone substitute that has the look and feel, and cutting and drilling properties of human bone thereby making it especially useful as a bone model for teaching and training medical students and for testing surgical equipment.




Drilling bone to permit use of internal screws for fixation of fractures, to implant artificial joints, to fix intramedullary implants and to utilize various other procedures is a widespread and important surgical technique. Obviously, the above surgical procedures involve precise cuts and drilling of sensitive tissues.




Unfortunately, there is a shortage of human bone tissue on which to practice new techniques and procedures. Cadaver bone is difficult and often expensive to obtain and is a serious potential biohazard as well. Currently, surgeons practice new drilling techniques on blocks of plastic or polyurethane, assuming this material closely mimics the drilling behavior of live human bone which, however, is not the case.




Previous studies on the drilling of bone have focused on orthogonal cutting and machining, and wear of machine parts, but there is currently no easy way to comprehend data concerning distinguishing drilling behavior of materials for comparison. In any event, what is needed are new materials which when molded will drill and cut like bone in order to provide better training for medical students and more realistic testing for surgical equipment manufacturers.




SUMMARY OF THE INVENTION




The invention provides a bone substitute whose properties closely mimic real bone when drilled or cut and comprises an inner core comprising a foamable polymer or other soft material to mimic cancellous bone and an outer shell formed around the inner core to mimic compact bone. The outer shell comprises a polymer such as an epoxy resin and a particulate filler such as a mineral added thereto to form a slurry for casting or molding around the inner core.




The particulate filler, which hardens the bone substitute and reduces the amount of polymer required, includes, but is not limited to, hydroxyapatite, aluminum oxide (Al


2


O


3


), silicon carbide (SiC) or mullite. For even better results, titanium oxide (Tio) can be added along with either Al


2


O


3


or SiC to modify the interaction between the polymer and the mineral and thereby reduce wear on surgical tools.




In one embodiment, the outer shell comprises an epoxy resin and from 5% to 15% by weight of Al


2


O


3


and from 20-45% by weight of TiO. In another embodiment, the outer shell comprises the epoxy resin and from 2.5% to 30% by weight of SiC and from 20% to 45% by weight of TiO.




To make a bone of the invention the first step is to make a female mold from an original (human) bone part. Then a bone substitute part is created from the female mold and reduced by a uniform thickness. A mold is created from the bone substitute part to replicate an inner core of the bone substitute; the inner core is then molded from a foamable polymer and suspended in the female mold. Finally, the outer shell is formed by pouring or injecting the epoxy resin/Al


2


O


3


(or SiC)/TiO slurry into the female mold with the inner core suspended therein.




The resulting bone substitute drills and cuts substantially like real bone thereby providing medical students with an accurate feel during surgical training, and equipment manufacturers with an accurate hardness for testing surgical devices.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

illustrates a cross-section of the bone substitute of the invention.





FIG. 2

is a bar graph illustrating drilling data from dog, lamb and cow bones and various compositions of bone substitutes of the invention.





FIG. 3

is a chart showing load as a function of particle diameter for different substances added to an epoxy resin comprising the outer shell of the invention.











DETAILED DESCRIPTION OF THE INVENTION




The invention provides a bone substitute that has the look and feel, and cutting and drilling properties that closely mimic real bone. As shown in

FIG. 1

, the invention comprises an inner core


10


made of a foamable polymer or other soft material and an outer shell


12


comprising a polymer and a particulate filler.




The filler is to increase the hardness, toughness and/or resistance of the polymer to drilling and cutting. The polymer and particulate filler form a slurry for casting around the inner core.




In laboratory tests of the invention, discussed below, two families of epoxy resins were chosen for the polymer for ease of processing: Bisphenol A and Bisphenol F. However, other thermosetting as well as thermoplastic polymers such as those listed in Table 1 below can also be used in the invention.













TABLE 1











ABS




Polyalkalene Ether






ABS/PA




Polyallomer






ABS/PC




Polyamide (Nylon)






ABS/PVC




Polybutadiene






Acetal




Polybutylene






Acrylic




Polycarbonate






Acrylonitrile Copolymer




Polyester (Saturated)






Alkyd




Polyester (Unsaturated)






Allylic Esters or Allyls (DAP,DAIP)




Polyether, chlorinated






ASA (Acrylic-styrene-acrylonitrile)




Polyethylene






Bis-maleimides




Polyimide (Polyamide-imide)






Cellulosics




Polyphenylene Sulfide






Cyanate/Cyanamide




Polypropylene






Epoxy




Polystyrene






Ethylene Vinyl Acetate




Polysulfone






Fluorocarbon Polymers :




Polyurethane






Fluorinated Ethylene-Propylene




Polyvinyl Acetate






(FEP)






Perfluoroalkoxy (PFA)




Polyvinyl Chloride






Polychlorotrifluoroethylene (CTFE)




Polyvinylidene Chloride






Polytetrafluoroethylene (TFE)




Polyxylylene






Polyvinylfluoride (PVF)




Silicone






Polyvinylidene Fluoride (PVDF)




Styrene-acrylonitrile (SAN)






Furan




Styrene-maleic-anhydride (SMA)






Ionomer




Urea-Formaldehyde






Melamine-Formaldehyde




Vinyl Ester






Phenolic














The particulate filler comprises a mineral, which, as noted above, hardens the bone substitute and reduces the amount of polymer required. Suitable minerals include, but are not limited to, hydroxyapatite, aluminum oxide (Al


2


O


3


), silicon carbide (SiC) and mullite.




In the laboratory tests, as discussed below, even better results were obtained by adding a second filler, titanium oxide (TiO), to either Al


2


O


3


or SiC to modify the interaction between the epoxy resin and the mineral and thereby reduce wear on surgical tools.




In one embodiment, the outer shell comprises an epoxy resin and from 5% to 15% by weight of Al


2


O


3


and from 20-45% by weight of TiO. In another embodiment, the outer shell comprises the epoxy resin and from 2.5% to 30% by weight of SiC and from 20% to 45% by weight of Tio. Best results were obtained with particle size for the Al


2


O


3


being 100 microns or less and for the SiC being 10 microns or less.




To fabricate a bone substitute of the invention the first step is to make a female mold from an original (human) bone part. Then a bone substitute part is created from the female mold and reduced by a uniform thickness. A mold is created from the bone substitute part to replicate an inner core of the bone substitute; the inner core is then molded from a foamable polymer and suspended in the female mold. Finally, the outer shell is formed by pouring or injecting, for example, the epoxy resin/Al


2


O


3


(or SiC)/TiO slurry into the female mold with the inner core suspended therein.




As shown in Table 2, different composite samples were formed in laboratory tests, consisting of three different epoxy resin systems, EPON® Resins 815, 826 and 862 (EPON is a registered trademark of Shell Chemical Company).












TABLE 2











Composition Table















Resin




Filler A




Filler B




Sample No.




Test Date (Drilling)


















826/V-40




None




None




7




19-Nov-96






815/V-40




None




None




8




19-Nov-96






826/V-40




35% 325 Mullite




None




11






826/V-40




56.6% 325 Mullite




None




12






815/V-40




40% 325 Mullite




None




13






815/V-40




40% 325 Mullite




None




13




21-Nov-96






815/V-40




60.8% 325 Mullite




None




14






815/V-40




60.8% 325 Mullite




None




14




21-Nov-96






862/3274




51.7% 100 Mullite




None




15






862/3274




51.7% 100 Mullite




None




15




21-Nov-96






862/3274




64.6% 100 Mullite




None




16






862/3274




64.6% 100 Mullite




None




16




21-Nov-96






815/V-40




47% 100 Mullite




None




17






815/V-40




47% 100 Mullite




None




17




21-Nov-96






815/V-40




62% 100 Mullite




None




18






815/V-40




62% 100 Mullite




None




18




21-Nov-96






826/V-40




24% 100 Mullite




None




19






826/V-40




62% 100 Mullite




None




19




21-Nov-96






826/V-40




49% 100 Mullite




None




20






826/V-40




49% 100 Mullite




None




20




21-Nov-96






826/V-40




34.2% T64-60




None




21






826/V-40




34.2% T64-60




None




21




21-Nov-96






826/V-40




52% T64-60




None




22






826/V-40




52% T64-60




None




22




21-Nov-96






815/V-40




61% T64-60




None




23






815/V-40




61% T64-60




None




23




21-Nov-96






815/V-40




38.7% T64-60




None




24






815/V-40




38.7% T64-60




None




24




21-Nov-96






862/3274




71.7% T64-60




None




25






862/3274




71.7% T64-60




None




25




21-Nov-96






862/3274




52% T64-60




None




26




22-Nov-96






826/V-40




57% T64-200




None




27




22-Nov-96






826/V-40




42% T64-200




None




28




22-Nov-96






815/V-40




43.3% T64-200




None




29




22-Nov-96






862/3274




55% T64-200




None




30




22-Nov-96






862/3274




65% T64-200




None




31




22-Nov-96






862/3274




71% AC99-325 Ll




None




32




22-Nov-96






862/3274




60.6% AC99-325 Ll




None




33




22-Nov-96






815/V-40




50% AC99-325 Ll




None




34




22-Nov-96






815/V-40




61% AC99-325 Ll




None




35




22-Nov-96






826/V-40




24.7% AC99-325 Ll




None




36




22-Nov-96






826/V-40




48% AC99-325 Ll




None




37




22-Nov-96






862/3274




52.3% A10 ung (?)




None




38




22-Nov-96






862/3274




40.4% A10 ung (?)




None




39




22-Nov-96






815/V-40




30% A, 10 μm




None




40




3-Dec-96






815/V-40




15% A, 10 μm




None




41




3-Dec-96






826/V-40




39% A, 10 μm




None




42




3-Dec-96






826/V-40




10.75% A, 10 μm




None




43




3-Dec-96






826/V-40




29% Premalox




None




44




3-Dec-96






826/V-40




46% Premalox




None




45




3-Dec-96






815/V-40




50% Premalox




None




46




3-Dec-96






815/V-40




39.8% Premalox




None




47




3-Dec-96






862/3274




31.6% Premalox




None




48




3-Dec-96






862/3274




55.5% Premalox




None




49




3-Dec-96






862/3274




10.24% Q-Cel 2116




None




50




3-Dec-96






862/3274




5.43% Q-Cel 2116




None




51




3-Dec-96






862/3274




42.3% TiO


2






None




52




3-Dec-96






862/3274




56% TiO


2






None




53




3-Dec-96






862/3274




25.5% TiO


2






None




54




3-Dec-96






826/V-40




58.2% AC99-100




None




55




3-Dec-96






815/V-40




33.5% 3μ SiC




None




56




3-Dec-96






Sawbones




None




None




58




5-Dec-96






815/V-40




54% 3μ SiC




None




59




6-Dec-96






826/V-40




5.6% 3μ SiC




None




60




6-Dec-96






826/V-40




29% 3μ SiC




None




61




6-Dec-96






862/3274




32% 3μ SiC




None




62




6-Dec-96






862/3274




46.5% 3μ SiC




None




63




19-Nov-96






826/V-40




27.5% AC99-100




None




64




6-Dec-96






862/3274




59.85% AC99-100




None




65




6-Dec-96






862/3274




69.5% AC99-100




None




66




6-Dec-96






815/V-40




48% AC99-100




None




67




6-Dec-96






815/V-40




64% AC99-100




None




68




6-Dec-96






826/V-40




16.8% 20μ SiC




None




69




6-Dec-96






826/V-40




44.8% 20μ SIC




None




70




6-Dec-96






826/V-40




26.4% TiO


2






5.6% α Al


2


O


3


, 0.3μ




71




6-Dec-96






815/V-40




56% 20μ SiC




None




72




6-Dec-96






815/V-40




33% 20μ SiC




None




73




6-Dec-96






862/3274




55.6% 20μ SiC




None




75




6-Dec-96






862/3274




67.3% 20μ SiC




None




76




6-Dec-96






862/3274




53.3% 100μ SiC




None




77




6-Dec-96






862/3274




Neat Resin




None




78




9-Dec-96






862/3274




48.68% TiO


2






7.5% α Al


2


O


3






79




9-Dec-96






862/3274




45.71% TiO


2






None




80




10-Dec-96






862/3274




48.63% TiO


2






8.17% 3μ SiC




81




11-Dec-96






862/3274




45.24% TiO


2






14.57% 3μ SiC




82




11-Dec-96






862/3274




48.63% TiO


2






8.17% 3μ SiC




83




12-Dec-96






862/3274




25.23% 3μ SiC




23.51% TiO


2






84




13-Dec-96






862/3274




31.2% TiO


2






9.92% Premalox




85




13-Dec-96






862/3274




41.54% TiO


2






5.73% 3μ SiC




86




16-Dec-96






862/3274




42.44% TiO


2






3.82% 3μ SiC




87




16-Dec-96






862/3274




30.72% TiO


2






9.18% Premalox




88




16-Dec-96














Except in two cases, each sample was filled with a variety of particulate minerals and titanium oxide (together fillers) of different diameters, and different volume concentrations as shown in Table 3. Samples made were 1″×6″×⅛″ in size, and were allowed to cure for a minimum of two days before any experiments were performed.

















TABLE 3









Filler




Diameter




%




Resin




Curing Agent




Treatment




























A-10 Ung




100 μm




15.03




EPON 815




EPON V-40




Cure Rm. Temp. overnight






Alumina Oxide





29.9








10.75




EPON 826




EPON V-40




Blow Dry, Cure Rm. Temp.








38.98








40.39




EPON 862




EPICURE 3274








52.33






Premalox 10 SG




0.25 μm




28.64




EPON 826




EPON V-40




Cure Rm. Temp. overnight






Alumina Oxide





45.87








39.83




EPON 815




EPON V-40




Cure Rm. Temp. overnight








50.65








31.58




EPON 862




EPICURE 3274




Blow Dry, Cure 150° F. 2 hrs








55.54






Mullite




˜149 μm




24.02




EPON 826




EPON V-40




Blow Dry, Cure 150° F. 1 hr






100 Mesh





48.97








46.98




EPON 815




EPON V-40




Blow Dry, Cure Rm. Temp. overnight








62.4








51.66




862




EPICURE 3274




Blow Dry, Cure Rm. Temp. overnight








64.62






Mullite




˜44 μm




34.91




EPON 826




EPON V-40




Blow Dry, cure Rm. Temp. overnight






325 Mesh





56.62








39.69




EPON 815




EPON V-40




Blow Dry, Cure Rm. Temp. overnight








60.8








41.96




EPON 862




EPICURE 3274




Blow Dry, Cure rm. Temp. overnight








62.93






Aluchem AC99-100




˜149 μm




27.5




EPON 826




EPON V-40




Blow Dry, Cure 150° F. 2 hrs






Tabular Alumina





58.28








48.19




EPON 815




EPON V-40




Cure Rm. Temp. overnight








64.1








59.85




EPON 862




EPICURE 3274




Blow Dry, Cure Rm. Temp overnight








69.46






AC99-325 Ll




˜44 μm




24.71




EPON 826




EPON V-40




Blow Dry, Cure Rm. Temp overnight






Tab. Alumina Ground





47.99






Low Iron





50.18




EPON 815




EPON V-40




Blow Dry, Cure 15° F. 3 um








61.58








60.61




EPON 862




EPICURE 3274




Blow Dry, Cure Rm. Temp. overnight








71.15






T64-60




100 μm




34.24




EPON 826




EPON V-40




Blow Dry, Cure 150° F. 2.5 hrs.






Tabular Alumina





52.05








38.68




EPON 815




EPON V-40




Blow Dry Cure rm. Temp overnight








61.19








52.05




EPON 862




EPICURE 3274




Blow Dry, Cure 150° F. 3 hrs








71.77






Silicon Carbide




3 μm




5.64




EPON 826




EPON V-40




Cure Rm. Temp. overnight








29.05








31.9




EPON 862




EPI-CURE 3274




Blow Dry, Cure 150° F. 2 hrs








46.51








33.52




EPON 815




EPON V-40




Blow Dry, Cure Rm. Temp. overnight








54.1






Silicon Carbide




100 μm




44.06




EPON 882




EPI-CURE 3274




Blow Dry, Cure 150° F. 3 hrs








62.35








38.24




EPON 815




EPON V-40




Blow Dry, cure 150° F. 2 hrs.








53.33







20 μm




32.74




EPON 815




EPON V-40




Blow Dry, Cure 150° F. 3.5 hrs.








56.29








16.79




EPON 826




EPON V-40




Blow Dry, Cure Rm. Temp. overnight








44.8








55.6




EPON 862




EPI-CURE 3274




Blow Dry, Cure Rm. Temp. overnight








67.31






Titanium (IV) Oxide





25.55




EPON 862




EPI-CURE 3274




Blow Dry, Cure rm. Temp. overnight








43.54








42.3






Cure Rm. Temp. overnight








56.2






Same





47.57




EPON 862




EPICURE 3274




Cure Rm. Temp. overnight






(Dried 150° F. 2 hrs)





65.71








25.77




EPON 826




EPON V-40




Cure Rm. Temp. overnight








61.29








56.8




EPON 815




EPON V-40




Cure Rm. Temp. overnight








71.17






Q-Cell 2116





5.43




EPON 862




EPICURE 3274




Blow Dry, Cure Rm. Temp overnight








10.24






T64-200




20 μm




55.12




EPON 862




EPICURE 3274




Blow Dry, Cure Rm. Temp. overnight






Tabular Alumina





64.88








43.32




EPON 815




EPON V-40




Blow Dry, Cure Rm. Temp. overnight








67.85






T64-200





41.89




EPON 826




EPON V-40




Blow Dry, Cure Rm. Temp. overnight






Tabular Alumina





57














Bone specimens tested for comparison were bovine, lamb and dog, the bovine and lamb obtained from a local store, kept cold, and used within one week. The length of time the canine bone had been frozen was unknown. Bovine bone tissue has previously been shown to be similar to human bone tissue with respect to many physical and structural properties. Also tested was a bone substitute product manufactured by Pacific Research Laboratories, Inc., called Sawbones®.




A standard surgical drill, the Maxidriver, was obtained and used for all drilling tests. A standard ⅛″ twist drill bit was used, a new bit for each sample. The drill was driven by nitrogen gas and all tests were performed at 110 psi, which results in a speed of approximately 900 rpm. The drill was clamped to the bottom of an INSTRON tensile machine, and samples were attached to a load cell and lowered onto the rotating drill.




Data was recorded for a given feed rate (usually two in/min) and fed to a personal computer. Information retrieved was load versus percent extension. A minimum of six holes were drilled in each sample with the same drill bit. A new drill bit was used for each bone or composite sample.





FIG. 2

provides comparative results between the dog, lamb and cow samples, the Sawbones® sample and ten samples of the invention (the sample numbers refer to the numbers in Table 2).

FIG. 3

with its accompanying legend illustrates in chart form the performance of each sample from Table 2 as a function of filler particle diameter. The area where real bone falls is indicated by the hash marked area between approximately 7.5 and 12.5 on the load or y-axis. The legend can be used in conjunction with Table 4 to determine the performance of each sample.





















TABLE 4











862/3274




%




826/V-40




%




815/V-40




%




826/3234




%
































TiO


2






A1




42.3




B1




45.5






C1




54.71







A2




56







A3




25.5






Premalox




F1




31.6




D1




29




E1




50







F2




55.5




D2




46




E2




39.8






SiC-3 um




I1




32




H1




29




G1




33.5







I2




46.5




H2




32




G2




54






SiC-20 um




P1




55.6




N1




16.8




O1




56







P2




67.3




N2




44.8




O2




33






T64-200




M1




55




K1




57




L1




43.3







M2




65




K2




42






Mullite-325




Q1




63




R1




35




S1




40







Q2




42




R2




56.5




S2




60.8






AC99-325 Ll




T1




71




V1




24.7




U1




50







T2




60.6




V2




48




U2




61






Mullite-100




W1




51.7




Y1




24




X1




47







W2




64.6




Y2




49




X2




62






T64-60




BB1




71.7




Z1




34.2




AA1




61







BB2




52




Z2




52




AA2




38.7






A10-Ung




CC1




52.3




EE1




39




DD1




30







CC2




40.4




EE2




10.8




DD2




15






SIC-100 um








FF1




53.3






AC99-100




HH1




59.85




GG1




58.2




II1




48







HH2




69.5




GG2




27.5




II2




64






Sand




KK1




66




LL1




61.3




JJ1




70







KK2




47.5




LL2




25.8




JJ2




56.8














Finally, Table 5 excerpts the best performing combination of epoxy resin, mineral and, in some cases TiO, for forming the outer shell of the substitute bone of the invention.

















TABLE 5












Filler 2





Table 2






Resin




Filler 1





(weight





Sample






(resin/hardner)




(weight %)




(test data)




%)




(test data)




Nos.











Shell Epon 815/V40




35%-60%




39%-50% 0.25 um Al


2


O


3






none





46, 47






100/44 pbw




30%-35%




33.5% 3.0 um SiC




none





56







60%-65%




61% 100 um T64-60 tabular Al


2


O


3






none





23







25%-35%




30% 10 um A-10 Al


2


O


3






none





40






Shell Epon 826/V40




35%-60%




35%-56.6% 44 um mullite




none





11, 12






100/100 pbw




20%-35%




24% 100 um mullite




none





19







20%-55%




24.7%-48% 44 um AC99-325




none





36, 37








ground tabular Al


2


O


3









25%-35%




29% 0.25 um Al


2


O


3






none





44







10%-50%




16.8%-44.8% 20 um SiC




none





69, 70






Shell Epon 862/3274




35%-55%




40.4%-52.3% 10 um A-10 Al


2


O


3






none





38, 39






100/44 pbw




25%-40%




31.6% 0.25 um Al


2


O


3






none





48







30%-50%




32%-46.5% 3 um SiC




none





62, 63







 5%-15%




9.2%-9.9% 0.25 um Al


2


O


3






45%-20%




31.2%-30.7% TiO


2






85, 88







2.5%-30% 




3.8%-25.2% 3 um SiC




45%-20%




42.4%-23.5% TiO


2






84, 86, 87














The resulting bone substitute of the invention drills and cuts substantially like real bone thereby providing medical students with an accurate feel during surgical training, and equipment manufacturers with an accurate hardness for testing surgical devices.



Claims
  • 1. A bone substitute useful as a bone model for teaching and training students and for testing surgical equipment, the bone substitute comprising:an inner core comprising a foamable polymer; and an outer shell formed around the inner core, the outer shell comprising an epoxy resin and silicon carbide (SiC) added to the epoxy resin.
  • 2. A bone substitute useful as a bone model for teaching and training students and for testing surgical equipment, the bone substitute comprising:an inner core comprising a foamable polymer; and an outer shell formed around the inner core, the outer shell comprising a polymer, and silicon carbide (SiC) and titanium oxide (TiO) added to the polymer to form a slurry for casting or molding around the inner core, said bone substitute exhibiting properties substantially like real bone useful for training and testing.
  • 3. A bone substitute comprising:an inner core comprising a foamable polymer; and an outer shell formed around the inner core, the outer shell comprising an epoxy resin and from 2.5% to 30% by weight of silicon carbide (SiC) and from 20% to 45% by weight of titanium oxide (TiO) added to the epoxy resin to form a slurry for casting or molding around the inner core, said bone substitute exhibiting properties substantially like real bone useful for training and testing.
CROSS-REFERENCE TO RELATED APPLICATION

This is a divisional of prior filed application Ser. No. 08/825,192, filed Mar. 27, 1997 now U.S. Pat. No. 6,116,911.

STATEMENT OF GOVERNMENTAL INTEREST

This invention was made with Government support under Contract No. N00039-94-C-0001 awarded by the Department of the Navy. The Government has certain rights in the invention.

US Referenced Citations (4)
Number Name Date Kind
3662405 Bortz et al. May 1972 A
4106219 Schneider et al. Aug 1978 A
4662888 Field May 1987 A
5314492 Hamilton et al. May 1994 A