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The ASTM D2533-99 standard—formally recognized as an American National Standard and approved for use by the Department of Defense—establishes a procedure for measuring the volume of vapor formed at atmospheric pressure from a given volume of gasoline. The ratio of these volumes is expressed as the vapor-liquid (V/L) ratio of the gasoline at the temperature of the test. The standard explicitly states that values in both inch-pound and SI units shall be regarded separately as the standard.
Critical terminology defined in the standard includes T(V/L = 20), which represents the equilibrium temperature at which the partial pressure of a sample is equal to 101.3 kPa (14.69 psia) and the vapor-liquid ratio is 20. The standard defines the vapor-liquid ratio as the ratio, at a specified temperature and pressure, of the volume of vapor in equilibrium with liquid to the volume of liquid sample charged at 0°C (32°F).
Because the solubility of oxygenates varies, the choice of containing liquid is strictly governed by the fuel composition.
| 🟦 Containing Liquid | 📏 Applicability | 🎯 Critical Restriction |
|---|---|---|
| Dry Glycerol | Nonoxygenated fuels only | Oxygenates may be partially soluble in glycerol, invalidating results for oxygenated blends. |
| Mercury | Oxygenated and Nonoxygenated fuels | Required for gasoline-oxygenate blends. Extreme toxicity requires adherence to Section 7 and Note 11. |
A measured volume of liquid fuel, cooled to 32 to 40°F (0 to 4°C), is introduced through a rubber septum into a buret filled with glycerol or mercury. The charged buret is then placed in a temperature-controlled water bath until equilibrium is reached. The volume of vapor in equilibrium with the liquid fuel is measured at the desired temperature(s) and the specified pressure, typically 760 mm Hg (101.3 kPa). If the temperature corresponding to a given V/L is desired, the ratio is determined at several temperatures, the results are plotted, and the temperature is read directly from the plot.
| 📐 Parameter | ⚡ SI Specification | ⚡ Inch-Pound Specification |
|---|---|---|
| Sample Charging Temperature | 0 to 4°C | 32 to 40°F |
| Standard Test Pressure | 101.3 kPa | 760 mm Hg (14.69 psia) |
| Liquid Reference Temp for V/L | 0°C | 32°F |
A critical distinction outlined in the standard (see Note 2) is that this test method measures a standardized V/L ratio, not the absolute vapor-liquid ratio. The calculation explicitly does not correct for: (1) liquid sample expansion with increasing temperature, (2) the decrease in liquid sample volume by vaporization, and (3) dissolved air in the liquid sample. This approach ensures consistent, repeatable comparative data for fuel volatility specifications.
To determine the vapor-liquid (V/L) ratio of spark-ignition engine fuels at atmospheric pressure. This data is essential for assessing fuel volatility and predicting vapor lock behavior.
Oxygenates in fuels are partially soluble in glycerol. Using glycerol would absorb fuel components, leading to an inaccurate V/L ratio. Mercury is inert and suitable for both oxygenated and nonoxygenated fuel samples.
The V/L ratio is measured at several temperatures at the specified pressure (760 mm Hg). The results are plotted, and the temperature corresponding to the desired V/L is read from the resulting curve or interpolation.
Cooling the sample to this range minimizes premature vaporization during the introduction into the buret. This ensures an accurate measurement of the liquid volume charged, which is the baseline for calculating the V/L ratio.