Systems and methods for improved dynamic pressure measurements

Abstract

A method, device, or system is provided for improving dynamic pressure measurements. In one embodiment, a method comprises receiving, at a filter structure having a restricting tube, an input pressure having a static pressure (PS), a lower-frequency dynamic pressure (PLD) and a higher-frequency dynamic pressure (PHD); filtering, by the restricting tube, the input pressure to substantially pass an output pressure having the static pressure (PS), the lower-frequency dynamic pressure (PLD), and an attenuated higher-frequency dynamic pressure (PHD); and outputting, from the filter structure, the output pressure.

Description

TECHNICAL FIELD[0001]This disclosure generally relates to pressure measurements and more particularly to systems and methods for improved dynamic pressure measurements.BACKGROUND[0002]In many environments and applications, it is often desirable to measure static pressure, dynamic pressure or both. In some instances, the static pressure may be much higher than the dynamic pressure. For example, the static pressure may be, for instance, an order of magnitude greater than the dynamic pressure. Further, the dynamic pressure may be associated with one or more distinct frequencies, which may occur at a relatively high frequency. For instance, aerodynamic engineers have long desired to measure high frequency flow and pressure in gas turbine engines and over aircraft wings. This capability is made possible using pressure transducers such as those fabricated from micro-machined silicon. Further, this capability may be associated with frequencies in the tens of kilohertz (kHz). As such, Kulit...

AI Technical Summary

Benefits of technology

The solution effectively dampens higher-frequency pressure waves, reducing measurement distortion and improving accuracy for dynamic pressure measurements across a wide frequency range, including high frequencies, while maintaining static pressure measurement integrity.

Problems solved by technology

While the pipe successfully cools the gases, it also reduces the bandwidth of the pressure measurement by the sensor due to the harmonic frequencies of the tube.

These oscillations make measuring the pressure and flow of the gases within the combustion chamber of the gas turbine difficult.

However, this tube may require a long length and precise coiling.

Further, other limitations may exist such as limited access for mounting sensors in a turbine case, discriminating against low and high frequencies, and other issues.

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