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Modern Engineering Thermodynamics

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6.6 Throttling Devices 181<br />

For an ideal gas with constant specific heats, we can substitute Eq. (6.22) into Eq. (6.23) to obtain<br />

T out = T in + ðV 2 in − V2 out Þ/ð2g cc p Þ<br />

This equation tells us that, in the case of negligible change in specific kinetic energy, the throttling of an ideal<br />

gas is an isothermal process.<br />

The actual throttling device outlet temperature for a pure substance is dependent on its Joule-Thomson coefficient<br />

μ J , defined as<br />

μ J = ð∂T/∂pÞ h<br />

(6.25)<br />

Since μ J is defined completely in terms of intensive thermodynamic properties, it too is an intensive thermodynamic<br />

property. A throttling process that has a negligible change in specific kinetic energy is a process of constant<br />

h, so the Joule-Thomson coefficient for any pure substance can be approximated from data taken during<br />

such a throttling process as<br />

μ J ≈ ðΔT/ΔpÞ throttling<br />

process<br />

(6.26)<br />

If we take Δp = p out − p in , then Δp normally is a negative number for such a process. Clearly, a positive value for<br />

μ J means that the temperature drops during such a throttling process (ΔT = T out − T in < 0) and a negative value<br />

for μ J means that the temperature increases. For an isothermal throttling process (such as occurs with an ideal<br />

gas), μ J =0.<br />

A gaseous pure substance that has a positive Joule-Thomson coefficient could undergo a continuous decrease<br />

in temperature and eventually be liquified by a properly designed throttling process. This was the basis of<br />

a process introduced in 1895 by Karl von Linde (1842–1934) for the large-scale production of liquid air.<br />

The temperature at which μ J = 0 for a real pure substance is called its inversion temperature T inv ,andμ J > 0for<br />

T < T inv and μ J < 0forT > T inv . Thus, the temperature of a real gas decreases in a throttling process if its<br />

inlet temperature is less than its inversion temperature. However, the temperature of a gas cannot be lowered<br />

via the Joule-Thomson effect if the gas inlet temperature exceeds its “maximum” inversion temperature<br />

(see Table 6.3). 6<br />

Figure 6.6 shows the variation in the Joule-Thomson coefficient with pressure and temperature for air and<br />

carbon dioxide.<br />

Table 6.3 The Maximum Joule-Thomson Inversion Temperature for Various Common Gases<br />

Substance<br />

K<br />

Maximum Inversion Temperature<br />

Air 659 1186<br />

Argon 780 1404<br />

Carbon dioxide 1500 2700<br />

Helium 40 72<br />

Hydrogen 202 364<br />

Neon 231 416<br />

Nitrogen 621 1118<br />

Oxygen 764 1375<br />

Source: Reprinted by permission of the publisher from Zemansky, M. W., Abbott, M. M., Van Ness, H. C., 1975. Basic <strong>Engineering</strong><br />

<strong>Thermodynamics</strong>, second ed. McGraw-Hill, New York.<br />

R<br />

6 Since the condition μ J = 0 can occur at more than one temperature, a gas may have several inversion temperatures, the largest of<br />

which is its “maximum” inversion temperature.

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