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A Design Tool for Aerodynamic Lens Systems - Department of ...

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324 X. WANG AND P. H. MCMURRY<br />

Furthermore, larger particles are more prone to be defocused in<br />

an assembly with more lenses. Typically, we have found that a<br />

lens assembly consisting <strong>of</strong> five lenses is sufficient to focus particles<br />

<strong>of</strong> a decade size range. Three or four lenses were used in<br />

our previous study <strong>of</strong> nanoparticle focusing (Wang et al. 2005b).<br />

Operating Pressures<br />

From Equation (4), we obtain the pressure (pfocusing) <strong>for</strong> focusing<br />

particles dp using the ideal gas law<br />

pfocusing = 2ρpd 2 p Cc ˙mRT<br />

9πµd 3 f MSto<br />

. [9]<br />

Note that Cc is a function <strong>of</strong> pfocusing. The minimum pressure <strong>for</strong><br />

flow to be subsonic (pMa) and continuum (pKn) are respectively<br />

given as (Wang et al. 2005a)<br />

and<br />

˙mc<br />

pMa =<br />

CdYc A f<br />

pKn =<br />

2 T1<br />

λr<br />

d f Kn∗ Tr<br />

� �<br />

2M<br />

pr<br />

RT1<br />

xc<br />

[10]<br />

1 + S/Tr<br />

. [11]<br />

1 + S/T1<br />

Figure 4 shows examples <strong>of</strong> pMa, pKn, and the required pfocusing<br />

to focus particles <strong>of</strong> different sizes as functions <strong>of</strong> the orifice size<br />

in Figure (4a) air and Figure (4b) helium when the flowrate is 0.1<br />

standard liter per minute (slm). The lens operating pressures are<br />

those along the pfocusing curves where pfocusing is wider than both<br />

pMa and pKn. Note that larger particles have a larger operating<br />

pressure window, and that using a lighter carrier gas can increase<br />

the operating pressures <strong>for</strong> smaller sizes which enables focusing<br />

them. Also shown in Figure 4(a) is a “Re warning line,” which<br />

corresponds to Re = 200 above which turbulence is likely to<br />

degrade focusing.<br />

As was pointed out previously (Wang et al. 2005a), increasing<br />

the operating pressure can reduce the detrimental effects <strong>of</strong><br />

nanoparticle diffusion and can reduce the pumping needs. From<br />

Figure 4, we can see that the maximum operating pressure <strong>of</strong><br />

smaller sizes occurs where the pMa curve intersects the pfocusing<br />

curve <strong>for</strong> each particle size, and its value can be derived from<br />

Equations (9) and (10),<br />

pmax = 648 ˙mµ2 St 2 o<br />

πC 3 d Y 3 c ρ2 p d4 p C2 c<br />

�<br />

M<br />

2RTx 3 c<br />

. [12]<br />

Note that this is an implicit expression because Cc is a function<br />

<strong>of</strong> pmax, and an iterative method is needed to calculate pmax.<br />

The pMa curve may not intersect the pfocusing curve <strong>for</strong> larger<br />

particles in the practical orifice diameter range. In this case any<br />

value <strong>of</strong> pfocusing larger than pKn can be used. However, Figure 4<br />

FIG. 4. The operating pressures <strong>for</strong> focusing unit density particles <strong>of</strong> different<br />

sizes as a function <strong>of</strong> orifice size using (a) air and (b) helium as the carrier gas.<br />

The flowrate is 0.1 slm. The two dash lines are the lower pressure limits pMa<br />

and pKn, respectively. The solid lines are pfocusing <strong>for</strong> indicated sizes.<br />

shows that the higher the operating pressure, the larger is the<br />

Reynolds number. It follows that Reynolds numbers tend to limit<br />

the maximum pressure at which lenses can be operated.<br />

Length <strong>of</strong> Spacers<br />

Spacers are used to separate lenses. They provide room <strong>for</strong><br />

generating the periodic converging/diverging flow pattern with<br />

orifices, which drives aerodynamic focusing. In addition to the<br />

constraints mentioned earlier (β ≤ 0.25; equal inner diameter <strong>of</strong><br />

all spacers), the spacers should be long enough so that the flow<br />

from the preceding lens can relax back to fully developed pipe<br />

flow be<strong>for</strong>e reaching the next lens (Liu et al. 1995b). Typically,<br />

spacer lengths are 10–50 times the upstream orifice diameter<br />

depending on the orifice Reynolds number (Wang et al. 2005a).<br />

However, no quantitative guideline on the spacer length has been<br />

reported.

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