Distributed circle method for guided wave based corrosion detection in plate-like structures
US-2017191966-A1 · Jul 6, 2017 · US
US10197534B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10197534-B2 |
| Application number | US-201514948398-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 23, 2015 |
| Priority date | Nov 24, 2014 |
| Publication date | Feb 5, 2019 |
| Grant date | Feb 5, 2019 |
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Disclosed are a method and a device for testing a defect based on an ultrasonic Lamb wave tomography. The method includes: partitioning an imaging area of a material to be tested into grids; exciting electromagnetic acoustic transducers for emitting to emit Lamb waves with a A 0 mode in all directions, and electromagnetic acoustic transducers for receiving to receive the Lamb waves; obtaining a time-frequency analysis result and recording time-of-flights of testing waves; determining a first slowness of each grid to obtain a first defect area; establishing an extrapolation formula according to the first defect area, and iterating the extrapolation formula to trace and revise paths of the Lamb waves until a better imaging precision is obtained.
Opening claim text (preview).
What is claimed is: 1. A method for testing a defect based on an ultrasonic Lamb wave tomography, comprising following acts performed by a computer: S 1 , selecting an imaging area on a material to be tested, and partitioning the imaging area into N 1 ×N 2 grids, wherein M electromagnetic acoustic transducers for emitting are set on a first side of the imaging area, M electromagnetic acoustic transducers for receiving are set respectively opposite to the M electromagnetic acoustic transducers for emitting on a second side of the imaging area, and N 1 , N 2 , M are positive integers; S 2 , exciting the M electromagnetic acoustic transducers for emitting to emit Lamb waves with a A 0 mode in all directions and the M electromagnetic acoustic transducers for receiving to receive the Lamb waves successively, such that M×M testing waves corresponding to M×M Lamb waves are obtained; S 3 , performing a time-frequency analysis and a mode recognition on the M×M testing waves, so as to obtain time-of-flights of the M×M Lamb waves; S 4 , recording the time-of-flights of the M×M Lamb waves; S 5 , determining a first slowness of each grid according to the time-of-flights and a size of each grid to obtain a first defect area; S 6 , establishing a three-dimensional Cartesian coordinate system in the imaging area, and defining an original emission angle; S 7 , for a path of a Lamb wave through the defect, obtaining a phase velocity c p at a point P(x,y) on a forward direction of the Lamb wave through the defect and calculating ∂c p /∂x and ∂c p /∂y according to the phase velocity c p , where x is a coordinate value of the point P(x,y)in a x-direction, y is a coordinate value of the point P(x,y)in a y-direction; S 8 , calculating an extrapolation point of the Lamb wave through the defect by introducing c p , ∂c p /∂x and ∂c p /∂y into an extrapolation formula; S 9 , judging whether a coordinate value of the extrapolation point reaches or exceeds boundary coordinates of a corresponding grid, if no, using the extrapolation point of the Lamb wave through the defect as a new point on the forward direction of the Lamb wave through the defect and executing steps S 6 -S 9 , if yes, recording the coordinate value of the extrapolation point as a coordinate value of the end point of the Lamb wave through the defect; S 10 , judging whether the coordinate value of the end point of the Lamb wave through the defect reaches or is close to the electromagnetic acoustic transducers for receiving, if yes, obtaining a path with a shortest time-of-flight of the Lamb wave through the defect, if no, changing the original emission angle and executing steps S 6 -S 10 until the path with the shortest time-of-flight of the Lamb wave through the first defect area is found; S 11 , obtaining a second slowness of each grid according to the time-frequency analysis result and the shortest time-of-flight and a change of a slowness curve in the defect to obtain a second defect area and to determine a size and a distribution of the second defect area. 2. The method according to claim 1 , wherein a diameter of the electromagnetic acoustic transducer is within a range of 20 mm to 80 mm, a distance between centers of each two adjacent electromagnetic acoustic transducers at the same side is within a range of 20 mm to 100 mm. 3. The method according to claim 1 , wherein the M electromagnetic acoustic transducers for emitting are excited by a radio frequency power amplifier, in which an excitation frequency of the radio frequency power amplifier is within a range of 50 kHz to 500 kHz. 4. The method according to claim 1 , wherein the Lamb wave emitted by the electromagnetic acoustic transducer for emitting is a Lamb wave with a single A 0 mode. 5. The method according to claim 1 , wherein the first or the second slowness of each grid is determined according to formula (1): T i = ∑ j = 1 n L ij * S j , ( i = 1 , 2 , … , m ) , ( 1 ) where S j is a slowness of a j th grid, L ij is a length of a i th Lamb wave in the j th grid, T i is a time-of-flight of the i th Lamb wave, n =N 1 ×N 2 , and m =M×M . 6. The method according to claim 1 , wherein the original emission angle is within a range of 0˜180°. 7. The method according to claim 1 , wherein obtaining a phase velocity c p at a point P(x,y) on a forward direction of the Lamb wave through the defect and calculating ∂c p /∂x and ∂c p /∂y according to the phase velocity c p comprises: obtaining 16 pixels with the extradition point used as a center; obtaining 16 phase velocities corresponding to the 16 pixels; introducing the 16 phase velocities respectively into a formula (2) to perform a two-dimensional surface fitting on a distribution of the phase velocities: c p ( x p , y p ) = ∑ k = 0 3 ∑
using the magnetostrictive properties of the material to be examined, e.g. electromagnetic acoustic transducers [EMAT]; (investigating the presence of flaws using eddy currents G01N27/90, magnetostrictive transducers B06B1/08, measuring magnetostrictive properties G01R33/18) · CPC title
Flexural waves, plate waves, e.g. Lamb waves, tuning fork, cantilever · CPC title
Defect imaging, localisation and sizing using, e.g. time of flight diffraction [TOFD], synthetic aperture focusing technique [SAFT], Amplituden-Laufzeit-Ortskurven [ALOK] technique · CPC title
by acoustic tomography (medical tomography A61B8/13) · CPC title
by measuring propagation velocity or propagation time of acoustic waves · CPC title
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