Method and system for detecting a leak in a pipeline
US-9500554-B2 · Nov 22, 2016 · US
US10168302B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10168302-B2 |
| Application number | US-201415028661-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 13, 2014 |
| Priority date | Oct 11, 2013 |
| Publication date | Jan 1, 2019 |
| Grant date | Jan 1, 2019 |
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Embodiments relate to a signal processing system and method in particular for determining the location of a feature within a hollow body using deconvolution of measured acoustic waves.
Opening claim text (preview).
The invention claimed is: 1. A pipe inspection method to identify characteristic acoustic impedance associated with a pipe; the method comprising the steps of resolving a plurality of measured resultant pressure waveforms, p x1 (t), p x2 (t), . . . , p xn (t) and p x2 (t),associated with the pipe into a number of associated waveforms; the number of associated waveforms being a function of the plurality of measured resultant pressure waveforms measured at respective positions; the plurality of measured resultant pressure waveforms representing measurements by a plurality of acoustic detection devices positioned at the respective positions of a launch body for exciting the pipe using an excitation waveform; deriving one or both of an impulse response, h(t),of the pipe and a corresponding-transfer function of the pipe from the number of associated waveforms; the one or both of the impulse response and the transfer function bearing the characteristic acoustic impedance associated with the pipe, wherein the step of deriving the one or both of the impulse response and the transfer function comprises evaluating h(t) from h(t)*[p x1 (t)−p x2 (t)*h m12 (t)]=[p x2 (t)*h m12 −1 (t)−p x1 (t)], where h m12 (t) represents the transfer function between a first and second acoustic detection devices of the plurality of acoustic detection devices. 2. The method of claim 1 , further comprising exciting the pipe using the excitation waveform via the launch body. 3. The method of claim 1 , further comprising taking a plurality of measurements via the acoustic detection devices; the plurality of measured resultant pressure waveforms being associated with the plurality of measurements. 4. The method of claim 1 , further comprising filtering the plurality of measured resultant pressure waveforms prior to said resolving. 5. The method of claim 4 , wherein the step of filtering applies one or more than one filter associated with a possible characteristic acoustic impedance. 6. The method of claim 1 , wherein the step of resolving the plurality of measured resultant pressure waveforms into the number of associated waveforms comprises resolving the plurality of measured resultant pressure waveforms into the number of associated waveforms representing differences between the measured resultant pressure waveforms. 7. The method of claim 6 , wherein the differences between the measured resultant pressure waveforms have an associated linear function or represent time shifted versions of the measured resultant pressure waveforms. 8. The method of claim 7 , wherein the linear function or differences take the form f ( p ( t ))= p ( t +τ)− p ( t −τ) where p(t) represents a measured resultant pressure waveform at time t; and τ is associated with the separation between acoustic measuring devices. 9. The method of claim 1 , wherein the step of deriving the one or both of the impulse response and the transfer function comprises evaluating h(t) from h(t)*[p x1 (t)−p x2 (t−τ)]=[p x2 (t+τ)−p x1 (t)]. 10. The method of claim 9 , wherein the step of deriving the one or both of the impulse response and the transfer function comprises evaluating h ( t ) = IFFT { FFT [ p x 2 ( t + τ ) - p x 1 ( t ) ] FFT [ p x 1 ( t ) - p x 2 ( t - τ ) ] } where FFT represents a Fourier Domain Transform and IFFT represents an Inverse Fourier Domain Transform. 11. The method of claim 1 , wherein the step of deriving the one or both of the impulse response and the transfer function comprises evaluating h ( t ) = IFFT [
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