There are several corrections, ranging from simple to complex, which may need to be applied during the calibration of a device under test (DUT).
If the reference standard is a pressure controller, the only correction that may need to be applied is what is referred to as a head height correction. The head height correction can be calculated using the following formula:
( ρf - ρa )gh
Where ρf is the density of the pressure medium (kg/m3), ρa is the density of the ambient air (kg/m3), g is the gravity (m/s2) and h is the difference in height (m). Typically, if the DUT is below the reference level, the value will be negative, and vice versa if the DUT is above the reference level. Regardless of the pressure medium, depending on the accuracy and resolution of the DUT, a head height correction must be calculated. Mensor controllers allow the user to input a head height and the instrument will calculate the head height correction.
Another potentially confusing correction is what is referred to as a sea level correction. This is most important for absolute ranges, particularly barometric pressure ranges. Simply put, this correction will provide a common barometric reference regardless of elevation. This makes it easier for meteorologists to monitor weather fronts as all of the barometers are referenced to sea level. For an absolute sensor, as the sensor increases its altitude, it will approach absolute zero, as expected. However, this can become problematic for a barometric range sensor as the reading will no longer be ~14.5 psi when vented to atmosphere. Instead, the local barometric pressure may read ~12.0 psi. However, this is not the case. The current barometric pressure in Denver, Colorado, for example, will actually be closer to ~14.5 psi and not ~12.0 psi. This is because the barometric sensor has a sea level correction applied to it. The sea level pressure can be calculated using the following formula:
(Station Pressure / e(-elevation/T*29.263))
Where Station Pressure is the current, uncorrected barometric reading (in inHg@0˚C), elevation is the current elevation (meters) and T is the current temperature (Kelvin).
For everyday users of pressure controllers or gauges, those may be the only corrections they may encounter. The following corrections apply mainly to piston gauges and the necessity to perform them relies on the desired target specification and associated uncertainty.
Another source of error in pressure calibrations are changes in temperature. While all Mensor sensors are compensated over a temperature range during manufacturing, this becomes particularly important for reference standards such as piston gauges, where the temperature must be monitored. Piston-cylinder systems, regardless of composition (steel, tungsten carbide, etc.), must be compensated for temperature during use as all materials either expand or contract depending on changes in temperature. The thermal expansion correction can be calculated using the following formula:
1 + (αp + αc)(T - TREF )
Where αP is the thermal expansion coefficient of the piston (1/˚C) and αC is the thermal expansion coefficient of the cylinder (1/˚C), T is the current piston-cylinder temperature (˚C) and TREF is the reference temperature (typically 20˚C).
As the temperature of the piston cylinder increases, the piston-cylinder system expands, causing the area to increase, which causes the pressure generated to decrease. Conversely, as the temperature decreases, the piston-cylinder system contracts, causing the area to decrease, which causes the pressure generated to increase. This correction will be applied directly to the area of the piston and errors will exceed 0.01% of the indicated value if uncorrected. The thermal expansion coefficients for the piston and cylinder are typically provided by the manufacturer, but they can be experimentally determined.
A similar correction that must be made to piston-cylinder systems is referred to as a distortion correction. As the pressure increases on the piston-cylinder system, it will cause the piston area to increase, causing it to effectively generate less pressure. The distortion correction can be calculated using the following formula:
1 + λP
Where λ is the distortion coefficient (1/Pa) and P is the calculated, or target, pressure (Pa). With increasing pressure, the piston area increases, generating less pressure than expected. The distortion coefficient is typically provided by the manufacturer, but it can be experimentally determined.
A surface tension correction must also be made with oil-lubricated piston-cylinder systems as the surface tension of the fluid must be overcome to “free” the piston. Essentially, this causes an additional “phantom” mass load, depending on the diameter of the piston. The effect is larger on larger diameter pistons and smaller on smaller diameter pistons. The surface tension correction can be calculated using the following formula:
πDT
Where D is the diameter of the piston (meters) and T is the surface tension of the fluid (N/m). This correction is more important at lower pressures as it becomes less with increasing pressure.
One of the most important corrections that must be made to piston-cylinder systems is air buoyancy.
As introduced during the head height correction, the air surrounding us generates pressure... think of it as a column of air. At the same time, it also exerts an upward force on objects, much like a stone in water weighs less than it does on dry land. This is because the water exerts an upward force on the stone, causing is to weigh less. The air around us does exactly the same thing. If this correction is not applied, it can cause an error as high as 0.015% of the indicated value. Any mass, including the piston, will need to have what is referred to as an air buoyancy correction. The following formula can be used to calculate the air buoyancy correction:
1 - ρa/ρm
Where ρa is the density of the air (kg/m3) and ρm is the density of the masses (kg/m3). This correction is only necessary with gauge calibrations and absolute by atmosphere calibrations. It is negligible for absolute by vacuum calibrations as the ambient air is essentially removed.
The final correction and arguably the largest contributor to errors, especially in piston-gauge systems, is a correction for local gravity. Earth’s gravity varies across its entire surface, with the lowest acceleration due to gravity being approximately 9.7639 m/s2 and the highest acceleration due to gravity being approximately 9.8337 m/s2. During the pressure calculation for a piston gauge, the local gravity may be used and a gravity correction may not need to be applied. However, many industrial deadweight testers are calibrated to standard gravity (9.80665 m/s2) and must be corrected. Were an industrial deadweight tester calibrated at standard gravity and then taken to the location with the lowest acceleration due to gravity, an error greater than 0.4% of the indicated value would be experienced. The following formula can be used to calculate the correction due to gravity:
gl/gs
Where gl is the local gravity (m/s2) and gs is the standard gravity (m/s2).
The simple formula for pressure is as follows:
P = F / A = mg / A
This is likely the fundamental formula most people think of when they hear the word “pressure.” As we dive deeper into the world of precision pressure measurement, we learn that this formula simply isn't thorough enough. The formula that incorporates all of these corrections (for gauge pressure) is as follows: