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Investigation of Solid Solution Hardening in Molybdenum Alloys

Investigation of Solid Solution Hardening in Molybdenum Alloys

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RM 18/6 17th Plansee Sem<strong>in</strong>ar 2009, Vol. 1 Wesemann, H<strong>of</strong>fmann et al.<br />

The effect <strong>of</strong> dielastic <strong>in</strong>teraction was characterised by the measurement <strong>of</strong> change <strong>in</strong> modulus <strong>of</strong><br />

rigidity. The modulus <strong>of</strong> rigidity G can be determ<strong>in</strong>ed by velocity <strong>of</strong> transversal ultrasonic waves cT <strong>in</strong> a<br />

metal with known density ρ. Transversal ultransonic waves show a low transmittance. Therefore an<br />

attempt was made to derterm<strong>in</strong>e G without direct measurement <strong>of</strong> cT at room temperature. Such a<br />

method is described by M. B. Reynolds [11]. Sample diameter d and the time Δt between the 1 st and 2 nd<br />

back wall echo and the velocity <strong>of</strong> longitud<strong>in</strong>al ultrasonic waves cL have to be determ<strong>in</strong>ed. For the<br />

verification <strong>of</strong> the ultra sonic measurements additional measurements were carried out with the<br />

ELASTOMAT. The ELASTOMAT excites the sample with different ultra sonic frequencies and the<br />

resonance frequencies are determ<strong>in</strong>ed. Thereby the modulus <strong>of</strong> elasticity E and the Poisson ratio ν can<br />

be determ<strong>in</strong>ed and the modulus <strong>of</strong> rigidity can be calculated. This comparitive measurement was done<br />

for molybdenum-titanium and molybdenum-tungsten alloys.<br />

The effect <strong>of</strong> gra<strong>in</strong> size harden<strong>in</strong>g was determ<strong>in</strong>ed with a pure molybdenum reference sample as well as<br />

on PLANSEE standard molybdenum rods with a total degree <strong>of</strong> deformation <strong>of</strong> φtotal = 3.4. The gra<strong>in</strong> size<br />

on the molybdenum rods was altered by variation <strong>of</strong> the anneal<strong>in</strong>g temperature between 1300°C and<br />

2300°C. Anneal<strong>in</strong>g time was constant for 1 hour. These samples were tested by Vickers hardness HV10<br />

−3<br />

−1<br />

at room temperature and compression tests at 500°C with a deformation rate <strong>of</strong> ε& = 2.<br />

0 ⋅10<br />

s .<br />

Results<br />

Except for the molybdenum-titanium alloys chemical analysis revealed <strong>in</strong>terstitial impurities below 1 ppm<br />

for hydrogen and below 5 ppm for nitrogen, and carbon. The molybdenum-titanium alloys with titanium<br />

content above 2% showed oxygen content <strong>of</strong> 150-350 ppm. SEM analysis <strong>in</strong> comb<strong>in</strong>ation with EDX<br />

revealed oxygen conta<strong>in</strong><strong>in</strong>g titanium particles (presumably titanium oxide) for these alloys even after<br />

apply<strong>in</strong>g a 2300°C anneal<strong>in</strong>g.<br />

Even at 2300°C a complete homogeneous distribution <strong>of</strong> the alloy<strong>in</strong>g elements could not be achieved for<br />

the molybdenum- tungsten and molybdenum-rhenium alloys, although the whole alloy<strong>in</strong>g content was <strong>in</strong><br />

solid solution (EPMA measurements <strong>in</strong> fig. 5 and fig. 6). Particles were observed for molybdenumtantalum<br />

and molybdenum-titanium alloys with high alloy<strong>in</strong>g content after a 2000°C anneal<strong>in</strong>g. After an<br />

additional 2300°C anneal<strong>in</strong>g the molybdenum- tantalum alloys were completely homogenised (EPMA<br />

measurements <strong>in</strong> Fig. 3 and Fig. 4) while very few particles rema<strong>in</strong>ed present <strong>in</strong> the high content<br />

molybdenum-titanium alloys.

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