Thermal treatment influence on micro hardness titanium alloy biomaterials.
Catana, Dorin ; Scarneciu, Ioan ; Popescu, Rodica 等
1. INTRODUCTION
Human desire for ameliorating his health state, affected by
diseases or accidents has imposed the idea of the use in well determined
conditions, of some artificially produced parts which are made of
naturals or artificial materials. It appeared two alternatives even by
the time of the first substitution assays:
--dead or alive tissues and organs transplantation;
--parts, devices or systems made of natural or artificial material
implants.
Present implants advantages are: functionality, availability and
the capacity of reproduction. Implants major disadvantages are
determined by nature, way of synthesis and materials different features
used in relation with alive tissues. Implant materials lack two
important characteristics of the alive tissues:
--the capacity of modifying its structure and features depending on
the solicitations that they support (for example: mechanical charging
for the osseous tissue or the blood flow for the blood-vessels);
--auto-annealing capacity.
Hip articulation has as main physiological functions: the
mechanical loads transmission between pelvis and femur, as well as the
relative movement between the system's two parts, osteo articular.
Hip articulation (cox-femoral) is a spherical type articulation, with
tree degree of movement facility: flexion-extension, abduction-adduction
and internal-external rotation. This articulation is greased with
synovial fluid, synovial cartilage--fluid combination carrying out the
diminution friction coefficients. Total replacement of the joint is made
by using prosthesis with its main purpose of taking over the
biomechanical function of natural joint.
2. THEORETICAL CONSIDERATIONS
The biomaterials are synthetic materials used for the parts,
devices and artificial systems carrying out, with the object of replace
and/or take over, totally or partially, the function of an alive tissue
for a limited or unlimited time. For the manufacture of some
articulation prothesis components, the metallic biomaterials must have:
--an elasticity module as similar as possible, to that of the long
bone;
--good fatigue resistance and lastingness;
--wear and electrochemical corrosion resistance as advanced as
possible.
The metallic materials that can be used for the hip articulations
replacement are: stainless steels, Co- Cr alloys and titan alloys
(Catana, 2002).
From all these presented metallic materials, the titanium and its
alloys are considered to be the most biocompatible, with the best
corrosion resistance in the human organism average and with the most
powerful relation between the implant and the surrounding osseous
tissue. The alloys for the implants are described in table 1 (Wusinczky
et al., 2007).
Titanium base alloys used for implants were subject of quenching
thermal treatment followed by artificial ageing. The thermal treatments
have been carried out in argon atmosphere.
Thermal treatments differentiated by the heating temperature,
cooling temperature and cooling average. Cooling time has been 1 hour
for all the tests (Wusinczky & Popescu, 2005).
To accentuate the metallurgical processing influence on the micro
hardness used as mechanic features modification indicator, there have
been carried out measurements of this, for all the materials with titan
base taken to be studied, respectively, for all the metallurgical
materials applied to these.
In the case of the Ti-6Al-4V alloy (Popescu et al., 2005) the
applied thermal treatment has been the placing into the solution with
the following parameters (micro hardness evolution is described in
figure 1):
TC1--heating at 950--970[degrees]C water cooling;
TC2--heating at 950--970[degrees]C furnace cooling;
TC3--heating at 850--870[degrees]C water cooling;
TC4--heating at 850--870[degrees]C furnace cooling.
Maintaining time has been for 1 hour and, after the hardening,
followed an ageing, its parameters being: 2 hours of heating at
700-710[degrees]C followed by air cooling.
For Ti-6Al-7Nb alloy the placing in solution hardening has been
performed in the following parameters:
TC1--heating at 920--940 [degrees]C water cooling;
TC2--heating at 920--940[degrees]C furnace cooling;
TC3--heating at 820--840[degrees]C water cooling;
TC4--heating at 570--580[degrees]C furnace cooling.
The ageing parameters were: heating at 570--580[degrees]C, 2 hours
maintenance, followed by cooling.
Alloy micro hardness evolution is described in figure 2.
For Ti-5Al-2.5Fe alloy the placing in hardening solution has been
performed in the following parameters:
TC1--heating at 1010--1030[degrees]C water cooling;
TC2--heating at 1010--1030[degrees]C furnace cooling;
TC3--heating at 900--920[degrees]C water cooling;
TC4--heating at 900--920[degrees]C furnace cooling.
Ageing parameters were: heating at 555--545[degrees]C, 2 hours
maintenance, followed by airy cooling. Alloy micro hardness evolution is
described in figure 3 (Wusinczky et al. 2005).
The last alloy studied is Ti-6Al-2Nb-1Ta-1Mo which has in
composition thallium and molybdenum, two essential chemical elements for
implants. For this alloy the placing in hardening solution has been
performed in the following parameters:
TC1--heating at 1020--1040[degrees]C water cooling;
TC2--heating at 1020--1040[degrees]C furnace cooling;
TC3--heating at 920--940[degrees]C water cooling;
TC4--heating at 920--940[degrees]C furnace cooling.
Ageing parameters were: heating at 595--605[degrees]C, 2 hours
maintenance, followed by airy cooling. Alloy micro hardness evolution is
described in figure 4. To be used in medicine, the presented treatments
have been completed with an anodization thermal treatment and a
thermochemical in electrolytic plasma in order to make the alloys
biocompatible.
3. CONCLUSIONS
For titanium base biocompatible materials the application of
adequate hardening thermal treatments will determine the improvement of
micro hardness which is essential when these materials are used for
joint prosthesis. For Ti6Al14V alloy, the TC1 treatment permits the
attainment of the highest hardness. For the Ti6Al7Nb alloy the entire
TC1 treatment is that which determine the wearing resistance. Also, the
hardness is increased, especially, due to the cooling increased speed
values, more than due to maintenance at placing in solution hardening
different temperatures. Ti5Al2.5Fe and Ti6Al2Nb1Ta1Mo alloys have a
similar behavior with the prior presented alloys at the TC1 treatment.
In order to have a significant increasing of titanium alloys micro
hardness the recommended placing in solution thermal treatment is that
one coded TC1. The researches will be completed with corrosion and
biocompatibility tests in order to determine which one is the best
solution for thermal treatment. When all test results will be available,
finally will be established which thermal treatments will increase the
micro hardness of studied titanium alloys and implicitly the best one to
produce the prostheses.
4. REFERENCES
Catana, D. (2002). Advanced Materials Processing, Lux Libris, ISBN 973-9428-73-8, Brasov
Popescu, R.; Catana, D. & Wusinczky, D. (2005). Optimal
parameters experimentally set for the temper heat treatment with laser
beam applied to steel C120, Proceedings of International Conference on
Materials Science and Engineering, pp. 125-128, ISBN 973-635-454-7,
University Transylvania, 02.2005, University Transylvania, Brasov
Wusinczky, D. & Popescu, R. (2005). New material used in the
medical area, Proceedings of International Conference on Materials
Science and Engineering, pp. 181-184, ISBN 973-635-454-7, University
Transylvania, 02.2005, University Transylvania, Brasov
Wusinczky, E.; Wusinczky, D. & Popescu, R. (2005). Hip joint
implants, Bulletin of Polytechnic Institute of Jassy, Vol. LIII, No. 4,
05.2007, pp. 333-338, ISSN 1453-1690
Wusinczky, D.; Wusinczky, E. & Popescu, R. (2007). Titan based
biomaterials behaviour used in joint replacements, Bulletin of
Polytechnic Institute of Jassy, Vol. LIII, No. 4, 05.2007, pp. 339-344,
ISSN 1453-1690
Tab 1. Main alloying elements for titanium implant alloys.
Alloy Chemical composition [%]
type
Al V Fe Nb
Ti6Al4V 5.5-6.5 3.5-4.5 0.25 --
Ti6Al7Nb 5.5-6.5 -- 0.25 6.5-7.5
Ti5Al2.5Fe 4.5-5.5 -- 2-3 --
Ti6Al2Nb1Ta1Mo 5.5-6.5 -- -- 2
Fig. 1 Average micro hardness value for Ti-6A1-4V alloy.
TAV-TC1 246,8
TAV-TC2 204,8
TAV-TC3 228,9
TAV-TC4 222,9
Note: Table made from bar graph.
Fig. 2 Average micro hardness value for Ti-6A1-7Nb alloy.
TAV-TC1 244,2
TAV-TC2 191,9
TAV-TC3 228,8
TAV-TC4 194,11
Note: Table made from bar graph.
Fig. 3 Average micro hardness value for Ti-5A1-2.5Fe alloy.
TAV-TC1 264,43
TAV-TC2 206,36
TAV-TC3 191,6
TAV-TC4 215,9
Note: Table made from bar graph.
Fig. 4 Average micro hardness value for Ti-6A1-2Nb-1Ta-1 Mo alloy.
TAV-TC1 248,36
TAV-TC2 188,74
TAV-TC3 243,12
TAV-TC4 200,5
Note: Table made from bar graph.