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Vacuum Technology Know How - Triumf

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Formula 2-9<br />

Turbopump K 0<br />

Formula 2-10<br />

Turbopump<br />

pumping speed<br />

Formula 2-11<br />

Turbopump S eff<br />

Formula 2-12<br />

Specific pumping speed<br />

www.pfeiffer-vacuum.net<br />

K 0 = exp<br />

The geometric ratios are taken from Figure 2.17. The factor g is between 1 and 3 [10]. From<br />

the equation, it is evident that K increases exponentially with blade velocity v as well as<br />

0<br />

with M because<br />

8<br />

(Formula 1-7).<br />

Consequently, the compression ratio for nitrogen, for example, is significantly higher than<br />

for hydrogen.<br />

. R . T<br />

c – =<br />

p . M<br />

Pumping speed<br />

Pumping speed S is proportional to the inlet area A and the mean circumferential velocity of<br />

0<br />

the blades v, i.e. rotational speed [9]. Taking the blade angle a into account produces:<br />

1<br />

S 0 = . A . v . sin a . cos a<br />

2<br />

c<br />

Taking the entry conductivity of the flange into account, (Formula 1-19)<br />

as well as the optimal blade angle of 45°, produces the approximate effective pumping<br />

speed S of a turbopump for heavy gases (molecular weight > 20) in accordance with<br />

eff<br />

the following formula:<br />

–<br />

L = . A<br />

Bm<br />

4<br />

S 0 + L Bm A . v<br />

S eff = =<br />

S 0 . LBm<br />

v<br />

c – . g . t . sin a<br />

4 .<br />

v<br />

c –<br />

Dividing the effective pumping speed by the bladed entry surface of the uppermost disk<br />

and taking the area blocked by the blade thickness into consideration with factor d ~= 0.9<br />

f<br />

provides the specific pumping speed of a turbopump for nitrogen, for example (curve<br />

in Figure 2.18):<br />

S d eff f . v<br />

S = =<br />

A<br />

A v<br />

4 .<br />

c –<br />

+ 1<br />

In Figure 2.18, the specific pumping speed d f = 1 in l / (s . cm²) is plotted on the ordinate and<br />

the mean blade speed on the abscissa v = p .f .(R a + R i ). Moving up vertically from this point,<br />

the point of intersection with the curve shows the pump’s maximum specific pumping speed<br />

2 2 S . Multiplying this value by the bladed surface area of the inlet disk: A = (R - Ri ) . p, yields<br />

A a<br />

the pumping speed of the pumps and enables it to be compared with the catalog information.<br />

The points plotted in Figure 2.18 are determined by Pfeiffer <strong>Vacuum</strong> on the basis of the<br />

measured values of the indicated pumps. Points that are far above the curve are not realistic.<br />

+ 1<br />

Page 59<br />

<strong>Vacuum</strong><br />

<strong>Technology</strong>

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