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76<br />

<strong>the</strong> Weber-Schmidt equation [Weber et al. (1936)], although also <strong>the</strong> experimental tables of<br />

Roberts and Sydoriak (1956), or <strong>the</strong> calculation of Bennett and Tompkins (1957) can be<br />

used <strong>for</strong> <strong>the</strong> two helium isotopes. The Weber-Schmidt equation is<br />

P<br />

ln<br />

P<br />

1<br />

2<br />

where<br />

=<br />

1 T1<br />

ln<br />

2 T<br />

2<br />

+<br />

y =<br />

0.<br />

18131ln<br />

X<br />

RP<br />

y<br />

y<br />

1<br />

2<br />

+<br />

+<br />

( ) n 1+<br />

T / 273.<br />

1<br />

0.<br />

1878<br />

0.<br />

1878<br />

X = 1.8087, n = 0.147 <strong>for</strong> helium,<br />

+<br />

0.<br />

41284 ln<br />

X = 1.1470, n = 0.195 <strong>for</strong> hydrogen.<br />

y<br />

y<br />

1<br />

2<br />

+ 1.<br />

8311<br />

−<br />

+ 1.<br />

8311<br />

0.<br />

15823 ln<br />

y<br />

y<br />

1<br />

2<br />

+<br />

+<br />

4.<br />

9930<br />

4.<br />

9930<br />

Index 1 indicates <strong>the</strong> hot end of <strong>the</strong> tube, index 2 <strong>the</strong> cold end; R designates <strong>the</strong> tube<br />

radius in cm, P <strong>the</strong> pressure in Pa, and T <strong>the</strong> <strong>temperature</strong> in K.<br />

al. (1982)].<br />

The trend of <strong>the</strong> effect is shown in Fig. 6.10 [Roberts and Sydoriak (1956), Durieux et<br />

Some <strong>temperature</strong> values <strong>for</strong> a vapour pressure <strong>the</strong>rmometer using He or H2 are<br />

shown in Table 6.1<br />

With oxygen, <strong>the</strong> correction reaches 20 mK near 54 K (when P = 100 Pa), but it is<br />

already less than 0.05 mK at 64 K <strong>for</strong> an Inconel tube 1.6 mm in diameter [Tiggelman<br />

(1973)]. For neon near 20 K it is less than 1 mK [Tiggelman (1973)].<br />

In general, <strong>the</strong>se calculations can be 10% to 25% in error [McConville et al. (1966)<br />

and McConville (1972)], since <strong>the</strong> correction depends upon <strong>the</strong> material used <strong>for</strong> <strong>the</strong> tube<br />

and <strong>the</strong> physico-chemical conditions of its inner surface, which may also vary with time.<br />

They can be calculated [McConville et al. (1966)] as a function of <strong>the</strong> reflection coefficient of<br />

<strong>the</strong> tube but, un<strong>for</strong>tunately, <strong>the</strong> latter is never well known and may change after long<br />

exposure to <strong>the</strong> gas.<br />

The <strong>the</strong>rmomolecular effect can be measured with an additional tube [Berry (1979)].<br />

Ano<strong>the</strong>r solution, which eliminates <strong>the</strong> correction, is to use a diaphragm transducer located<br />

in <strong>the</strong> lower <strong>temperature</strong> region [Gonano and Adams (1970)] (see Fig. 6.7).<br />

Current practice consists of using pressure tubes of <strong>the</strong> largest section possible<br />

compatible with keeping heat transfer losses reasonably small (and to include some means<br />

of blocking radiation (gains, not losses) and damping oscillations). If <strong>the</strong> calculated<br />

correction is to be realistic, it is indispensable to have a constant diameter in <strong>the</strong> parts of <strong>the</strong><br />

tube where <strong>the</strong> <strong>temperature</strong> is ill-defined.<br />

The two corrections from Secs. 6.3.4 and 6.3.5 are usually small and in many cases<br />

<strong>the</strong> only significant uncertainty is that due to <strong>the</strong> reading of <strong>the</strong> pressure.

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