2.3.1 Laminar conductance
Let us consider the pumping station for the drying system (Figure 2.3) and calculate the drop in pressure between the condenser and the backing pump. In this case, due to the pressure of 4,285 Pa and the pumping speed of 4,285 Pa, ππ£ of the backing pump of 107 mΒ³ h-1 = 2.97 Β· 10-2 mΒ³ s-1, a gas throughput of π = 4,285 Β· 2.97 Β· 10-2 = 127 Pa mΒ³ s-1 is specified. The DN 63 piping has an inside diameter of 0.07 m and a length of 2 m. Two 90Β° pipe bends having an equivalent length of 0.2 m each are also taken into consideration.From a pump inlet pressure of 4,285 Pa and a value for air of 6.7 Β· 10-3 Pa Β· m for πΌΒ―β π according to Chapter 1, Table 1.5 we obtain a mean free path of 1.56 Β· 10-3 m. We use the Knudsen number, Formula 1-13, to determine the flow range and obtain:
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K_{n}=\frac{\bar{l}}{d}=2.23\cdot10^{-2}
Since Kn is less than 0.01, this results in viscous flow. This can be either laminar or turbulent. For laminar flow the conductance are significantly higher than for turbulent flow, which means that significantly lower volume flow losses will occur. The Reynolds number Re must be less than 2,300 for laminar flow. To calculate the Reynolds number, we first determine the flow velocity π£ in the piping:
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v=\frac{4\cdot S_{v}}{d^2\cdot\pi}=8.66\,\text{m}\,\text{s}^{-1}
And we determine the density π of the air at 4,285 Pa from the air density π0 = 1.293 kg m-3 at atmospheric pressure
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\rho=\frac{1.293\cdot4.285}{101.325}=5.47\cdot10^{-2}\,\text{kg}\,\text{m}^{-3}
and according to Formula 1-14 with a dynamic viscosity for air of 18.2 Β· 10-6 Pa Β· s we obtain
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\text{Re}=\frac{\rho\cdot\nu\cdot l}{\eta}=1{,}820
i. e. laminar flow.
We use Formula 1-26 in Chapter 1 p1 to obtain the inlet pressure for the piping:
We use Formula 1-26 in Chapter 1 p1 to obtain the inlet pressure for the piping:
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C_{Rohr,\,lam}=\frac{\pi\cdot d^4}{256\cdot\eta\cdot l}\cdot(p_1+p_2)=\frac{\pi\cdot d^4}{128\cdot\eta\cdot l}\cdot\bar{p}
We multiply by Ξπ=π1βπ2 to obtain the gas throughput
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Q=C_{Rohr,\,lam}\cdot\Delta p=\frac{\pi\cdot d^4}{256\cdot\eta\cdot l}\cdot(p_1^2-p_2^2)
Since π2 = 4,285 Pa and π = 127 Pa Β· m3 Β· s-1 it is possible to directly determine π1 from these values:
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p_1=q_{diff}\cdot A_{d}\cdot\sqrt{p_2^2+\frac{Q\cdot256\cdot\eta\cdot l}{\pi\cdot d^4}}=4{,}287.2\,\mathrm{Pa}
We have a pressure loss of merely 2.2 Pa, a very low value.
The conductivity of the piping is obtained from Chapter 1, Formula 1-18:
The conductivity of the piping is obtained from Chapter 1, Formula 1-18:
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C=\frac{Q}{\Delta p}=58\,\mathrm{m^3\cdot s^{-1}} oder58{,}000\,\mathrm{l\cdot s^{-1}}
The effective volume flow rate
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S_{\text{eff}}=\frac{S_{v}\cdot C_{\text{Rohr, lam}}}{S_{v}+C_{\text{Rohr, lam}}}=2.9707\,\mathrm{m^3\cdot s^{-1}}
is only slightly lower than the volume flow rate without the piping: ππ£ of 2.9222 m3 s-1.
2.3.2 Molecular conductance
Now let us also consider the conductance of the same piping in the molecular flow range. The piping has a diameter of 0.07 m and a length of 2 m. The elongated length of 0.235 each of the two 90Β° pipe bends, i. e. a total length of π = 2.47 m. In accordance with Chapter 1, Formula 1-30, the piping resistance is:-
L_{R_{m}}=\frac{\dot{c}\cdot\pi\cdot d^3}{12\cdot l}=1.71\cdot10^{-2}\,\text{m}^3\text{s}^{-1}
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S_{eff}=\frac{S_{\nu}\cdot L_{R_{m}}}{S_{\nu}+L_{R_{m}}}=1.09\cdot10^{-2}\,\text{m}^3\text{s}^{-1} withS_{\nu}=2.97\cdot10^{-2}\,\text{m}^3\text{s}^{-1}
In the molecular flow range, the pumping speed of the backing pump would be reduced to nearly one third. In this range, it is absolutely necessary to pay strict attention to short runs and large piping cross sections between the pump and the vacuum chamber. This applies in particular for turbopumps that should ideally be flanged directly to the vacuum chamber.