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Pfeiffer <strong>Vacuum</strong><br />
Page 62<br />
Formula 2-13<br />
Holweck stage<br />
pumping speed<br />
Formula 2-14<br />
Holweck stage<br />
compression ratio<br />
<strong>Vacuum</strong> <strong>Technology</strong><br />
The pumping speed S 0 of the Holweck stages is equal to:<br />
Where b . h is the channel cross section and v . cos a the velocity component in the<br />
channel direction.<br />
The compression ratio increases exponentially as a function of channel length L and<br />
velocity v . cos a [4]:<br />
K 0 =<br />
1<br />
S 0 = . b . h . v . cos a<br />
2<br />
v . cos a . L<br />
c – . g . h<br />
mit 1 < g < 3<br />
The values yielded by this formula are much too large, because backflow over the web from<br />
the neighboring channel dramatically reduces the compression ratio, and this influence is not<br />
taken into account in Formula 2-14.<br />
In order to use small dry backing pumps, e.g. diaphragm pumps having ultimate pressures<br />
of less than 5 mbar, turbopumps are today equipped with Holweck stages. These kinds of<br />
pumps are termed turbo drag pumps. Since the Holweck stages require only low pumping<br />
speeds due to the high pre-compression of the turbopump, the displacement channels and,<br />
in particular, both the channel height as well as the clearances to the rotors can be kept<br />
extremely small, thus still providing a molecular flow in the range of 1 mbar. At the same<br />
time, this increases the compression ratios for nitrogen by the required factor of 10 3 . The<br />
shift of the compression ratio curves to higher pressure by approximately two powers of<br />
ten can be seen from Figure 2.22.<br />
Compression ratio<br />
10 12<br />
10 11<br />
10 10<br />
10 9<br />
10 8<br />
10 7<br />
10 6<br />
10 5<br />
10 4<br />
10 3<br />
10 2<br />
10 1<br />
Classical turbopump 520: Nitrogen<br />
Classical turbopump 520: Hydrogen<br />
Turbo drag pump: Hydrogen<br />
Turbo drag pump: Nitrogen<br />
10 - 3 10 - 2 10 - 1 10 0 10 1 10 2<br />
mbar<br />
Backing vacuum pressure<br />
Figure 2.22: Compression ratios of pure turbopumps and turbo drag pumps<br />
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