Abstract

This article presents a Siren Disk proof of concept for the dynamic excitation of pressure probes, and a method to reconstruct distorted signals due to pneumatic channels. Constraints in sensor installation require placing a pressure transducer distant from the measurement point. The transducer is usually connected through a pneumatic channel – creating a probe, which alter its dynamic response. The Siren Disk is used for the identification of transfer functions of different pressure probe geometries. The device is capable of producing pressure signals up to 10 kHz and 3.5 bara (peak-to-peak = 2.5 bars). The transfer function is obtained through the comparison of the probe signal to a flush mounted reference transducer that is subjected to the same pressure signal. The response of the probes was shown to be highly non-linear. Hence, a multi-dimensional transfer function is developed for the system identification of the probes. The function is based on the Fourier series, and consists of a set of sub transfer functions describing the average gain and phase lag for the offset and the harmonics. The approach is well suited to capture the non-linear frequency response of complex sensor installations. Experiments show that the flat response of transducers is jeopardized by the introduction of the low pass filter behavior from the pneumatic channels. The probe’s signal was significantly distorted compared to the reference signal. The inverse transfer function is used to reconstruct the probe’s signal in the time domain. Good agreement is found between the reconstructed and the reference signals even at excitation frequencies beyond the probe’s resonant frequency. Hence, highlighting a wide range of validity for the proposed method.

Highlights

  • Time resolved accurate pressure measurements are of pronounced importance in the control, monitoring and understanding of a wide range of mechanical and aerospace systems

  • Imposing the connection of the pressure transducers distant from the point of interest via pneumatic channels – creating a probe

  • Non-linear Transfer Function Identification In order to reconstruct the original signal based on the test probe signal, the latter’s dynamic response needs to be identified

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Summary

Introduction

Time resolved accurate pressure measurements are of pronounced importance in the control, monitoring and understanding of a wide range of mechanical and aerospace systems. The distance between the reference transducer and the test probe needs to be kept minimal - Figure 3 These design constraints yield a 280 mm diameter disk, with 80 holes, a pitch of 10 mm between holes, and a maximum rotational speed of 7500 rpm. Such design is able to produce a hole passing frequency (hpf) of 10 kHz. The disk holes are of a semi-oval shape having straight side walls, guaranteeing synchronized opening and closing over both the reference transducer and the test probe. An optical proximity probe is placed on top of the Siren Disk holes in order to measure the hpf

Siren Disk Qualification
29: Eq 1 where
Accuracy of Signal Reconstruction
Findings
Conclusions
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