The invention relates to a method and a device for testing a component, such as a body of concrete or another building component, by means of ultrasound.
The destruction-free testing of components by means of ultrasound provides an important tool in various fields of technology. It can e.g. be used to locate reinforcements, voids, cracks or inhomogeneities in building materials, such as concrete.
A device of this type is shown in U.S. Pat. No. 7,587,943. It comprises a plurality of ultrasonic transducers arranged in a housing. Driver electronics are provided for individually sending and/or receiving signals through the transducers.
To operate the device, the user holds the same against the component to be tested, and then the transducers are operated to perform a scanning operation.
The device of U.S. Pat. No. 7,587,943 comprises a plurality of modules, each of them having several testing heads with ultrasonic transducers. One of the modules is operated as transmitter module to send out signal pulses, which are then received by the other modules.
The problem to be solved by the present invention is to provide such a method and device with improved measurement accuracy.
This problem is solved by the method and device of the independent claims.
Accordingly, the method for testing a component by means of ultrasound comprises the following steps:
In other words, the invention is based on the understanding that one major factor affecting the accuracy and robustness of the measurement is the quality of the coupling of the individual ultrasound receivers. For example, even a small amount of surface roughness, minor surface inhomogeneities, or a slight misalignment of the device when applying it to the component, may lead to some receivers coupling much better to the component than others.
To correct this inherent inaccuracy of the method of measurement, the invention exploits the fact that the surface wave is a good measure for how well a receiver couples to the component and by how much its signal should be scaled. By scaling the response signals (at least the parts of them that are of interest) as a function of the correction value, the dependence of the response signals on local surface irregularities or improper application of the device against the component can be reduced.
Once the second signal sections from the various receivers are scaled, they are advantageously combined, e.g. in a SAFT algorithm, for generating a result data set, such as an image of the inner structure of the component. Since the second signal sections are scaled according to the coupling quality of their respective receivers, the result data set will have improved accuracy and consistency.
There are various ways to identify the first signal section, i.e. the signal section describing the surface signal. These can be used independently or in combination.
Advantageously, the method comprises, for each ultrasound receiver in said group, the following steps:
In one embodiment, the temporal location of the time window is a function of the distance of the ultrasound receiver from the ultrasound emitter: Advantageously, the temporal location is proportional to this distance.
In another embodiment (which can, e.g. for consistency checking, be combined with the previous embodiment), the temporal location of the time window is selected as a function of the time at which a first pulse is detected in the response signal. In this context, the “first pulse” is the first one arriving after the probe signal has been sent into the components. This is based on the understanding that, in most components, the surface waves are the fastest signals propagating from the ultrasound emitter to the ultrasound receiver.
Advantageously, generating the probe signals and receiving the response signals takes place while a user is manually holding the device against the component to be tested. The signal scaling provided by the present invention is especially suited to compensate for issues due to a non-uniform application of pressure to the device. The invention therefore allows to obtain substantially steadier signals for those cases where the device is applied manually. This is of particular importance if images of the component's interior structure are derived from the response signals.
The invention also relates to a device for testing a component by means of ultrasound. This device comprises
Advantageously, the control unit is adapted and structured to carry out the method according to any of the method claims with the potential exception of applying a device against the component, which is typically something the user of the device will do unless the device is e.g. robot operated.
The method and device according to the present invention can be used to probe any type of component, in particular samples of concrete.
In a particular embodiment, the invention can be used for creating image representations of the inner structure of the component, in particular using Synthetic aperture focusing technique (SAFT).
The invention will be better understood and objects other than those set forth above will become apparent when consideration is given to the following detailed description thereof. This description makes reference to the annexed drawings, wherein:
The device 1 shown in
It comprises a housing 2 of e.g. substantially cuboid design.
Housing 2 has a probing side 3. Probing side 3 is advantageously flat.
A plurality of bidirectional ultrasonic transducers 4 is arranged on probing side 3 of housing 2. Each transducer 4 advantageously comprises a piezoelectric actuator equipped with a tip 5a and elastically mounted in a holder 5b, e.g. of the type described in WO 2016/029326.
The transducers 4 are advantageously located in a flat plane and adapted to be placed against a flat surface of a component to be tested.
In the embodiment shown, the transducers 4 are arranged in a rectangular matrix of rows and columns. The matrix has e.g. three such rows and eight columns. The transducers 4 in a single column can e.g. be part of a single channel of the device, as it will be described in more detail below.
The diagram schematically shows the transducers 4 grouped into channels 6. In the shown embodiment, each channel 6 has three transducers 4.
In the present embodiment, the channels 6 are arranged in a line, i.e. along one direction, even though a two-dimensional arrangement can be envisaged for imaging the component in full 3D.
A controller 7 is connected to the channels 6 to control them and to receive signals therefrom. Controller 7 e.g. comprises interface circuitry 8 for interfacing with the channels 6, a CPU 9 adapted to control the operations and a memory 10 for storing data and firmware.
Further, controller 7 can be connected to input and output circuitry as well as to user-interface circuitry for receiving commands, sending data, and displaying measurement results.
In the present embodiment, each of the channels 6 can be operated as an ultrasound emitter or as an ultrasound receiver:
In both cases, the tips 5a of the transducers 4 should be in contact with the surface of the component.
To carry out a measurement, the user places device 1 against the component to be tested such that, if possible, all transducers 4 come into contact with it.
Then, at least one, typically exactly one at a time, of the channels 6 is set to operate as an ultrasound emitter. Further, several of the channels 6, advantageously at least all of the channels except for the channel operating as emitter, are operated as ultrasound receivers.
Controller 7 instructs the ultrasound emitter to generate a probe signal. The probe signal can e.g. comprise a single pulse cycle including the application of a positive followed by a negative voltage to the transducer(s) of the ultrasound emitter. However, more complex waveforms can be used as well.
Advantageously, but not necessarily, the probe signal is comparatively short as compared to the interval between consecutive probe signals in order to leave enough time to measure all echoes from a probe signal before issuing the next probe signal.
Controller 7 then collects the response signals measured by the ultrasound receivers:
The response signals correspond to the ultrasound vibrations detected by the transducer(s) of the channels 6 configured as ultrasound receivers. These vibrations are caused by the superposition of various signal paths between the ultrasound emitter and each ultrasound receiver.
As can be seen from the left column of
As can further be seen from the left column in
Finally, as it can also be seen from the left column of
As mentioned above, such effects can be compensated for by suitable signal scaling.
In general, a channel measuring a weak amplitude of the arriving surface wave is poorly coupled to the component. Therefore, so measure the subsequently arriving reflected waves with smaller sensitivity.
In order to compensate for such variations, each ultrasound signal Ci is resealed using a scale factor Si:
Ci′=Si·Ci, (1)
with Ci′ denoting the rescaled signal. Such rescaled signals are shown in the right column of
It must be noted that the correction according to Eq. (1) does not necessarily have to be carried out over all the measured response signals. It may also be carried out over a “second signal section” (as called in the claims) only, namely over treat par of the signal that is used for further processing.
Scaling factor Si can be derived from a correction value Vi describing the strength of the response signal in its “first signal section”, i.e. the strength of the measured surface wave.
In general, scaling factor Si will be a function of the correction value Vi where the scaling factor Si becomes smaller as the correction value Vi increases. In most cases, a reciprocal relation provides best results, i.e.
Si=Ki/Vi, (2)
with Ki being a constant. Ki can be the same value for all ultrasound receivers. Alternatively, it may also take into account the natural damping of the surface wave as it propagates from the ultrasound emitter to the ultrasound receiver, for example by setting
Ki=K·exp(α·xi) (3)
with α a being a attenuation constant describing the damping of the surface wave per length and xi being the distance of the respective ultrasound receiver from the ultrasound emitter. K is a constant that is typically common to all ultrasound receivers.
In the following, we describe various ways to calculate the correction value Vi.
In a first step, the part of the response signal corresponding to the surface wave has to be identified. For this purpose, a time window W (as shown in
In one embodiment, the temporal location (i.e. the window's start and end times) can be calculated to be proportional to the distance xi of the ultrasound receiver from the ultrasound emitter. For example, the center time ti of the time window can be calculated by
ti=xi/c, (4)
with c being the velocity of the surface wave.
The length of the time window is typically a function of the length of the probe signal (pulse) emitted by the ultrasound emitter. Advantageously, the length of the time window is chosen to be at least as large as the length of the emitted pulse, advantageously somewhat larger in order to compensate for an error in the assumed velocity c of the surface wave. For example, the length of the time window is between the length of the pulse and five times the length of the pulse, in particular it is approximately twice the length of the pulse.
Alternatively, or in addition thereto, the time window can be positioned by searching for the first strong pulse (e.g. a pulse whose amplitude exceeds a given threshold amplitude) in the response signal. Such a first pulse typically indicates the arrival of the surface wave. In other words, the temporal location of the time window is selected as a function of the time of arrival of the first pulse in the response signal after the probe signal has been emitted.
This analysis of the time of arrival of the first pulse can be combined with the calculation of Eq. (4) in order to check the two methods for consistency. If the results of the two methods are inconsistent, rescaling can, for example, be suppressed, or a different (e.g. longer) time window can be used.
Once a suitable time window W has been determined, the correction value Vi can be derived from the strength of the signal therein. Again, there are various ways to do that:
In one example, the envelope of the signal of the response signal can be calculated, at least in the time window W. Such an envelope is shown in dotted lines in Figs. C1 and C2.
Algorithms for calculating the envelope of an oscillating signal are known to the skilled person. For example, the signal can be rectified (i.e. the absolute value of the signal is used) and then low-pass filtered, with a low pass filter.
The low pass filter can e.g. be dimensioned by assuming that the probe signal is an amplitude modulated signal having a carrier frequency corresponding to the pulse frequency (e.g. 50 kHz) and that the bandwidth of this signal is B. After rectification, the spectrum of the raw signal is split into a base band signal at 0 Hz and a signal at the double central frequency of the pulse (i.e. at e.g. 100 kHz). Spectral components around the double central frequency (i.e. around 100 kHz) are undesired and to be filtered out. Hence, the cut-off frequency of the low pass filter should advantageously be around B/2. This also ensures that the base band signal (i.e. the envelope) is not influenced by the filter, while the undesired frequency components the double central frequency are suppressed).
Once the envelope has been calculated, its maximum, or another quantity describing its strength, can be used for deriving the correction value Vi. For example, the correction value Vi can be set to be equal to the highest value A of the envelope, as shown in the top left graph of
Alternatively, or in addition thereto, the correction value can be a function of, in particular be proportional to, the maximum value of the response signal itself, without calculating the envelope first. In particular, the search of the maximum value is again limited to the window W.
It must be noted, though, that using the envelope is more robust against erratic signal noise than using an individual peak value of the response signal.
It must further be noted that the window W is not necessarily a “rectangular” window in the sense that any signals outside it are ignored. It may also be a “weighted” window in the sense that it is represented by a distribution function to be multiplied with the response signal, wherein the distribution function has a flat maximum over a region centered on the expected time of arrival of the surface wave and gradually decays to zero on both sides thereof.
Further, methods not or not explicitly relying on a time window can be used, e.g. by simply searching for the highest signal values in the response signal.
In the embodiment shown here, the calculation of the correction value as well as the rescaling is carried out by controller 7, e.g. implemented as operations in the programming of CPU 9. Alternatively, or in addition thereto, some or all of these steps can be carried out at the level of the individual channels and/or at a processing unit outside housing 2.
The transducers of the ultrasound emitter are advantageously operated to generate shear waves, i.e. their tips 5a are moved in a direction parallel to probing side 3 and parallel to the column of transducers 4 in the ultrasound emitter channel. However, different oscillations can be used, too.
The device can be equipped with user input controls that allow the user to selectively enable or disable the signal scaling described here.
In the example above, it was assumed that one channel 6 was the ultrasound emitter, while the other channels 6 were the ultrasound receivers. In most modes of operation, the role of the ultrasound emitter is subsequently attributed to all channels 6, while each time the other channels 6 will be used as receivers.
Advantageously, the ultrasound emitter and/or each ultrasound receiver comprises several ultrasonic transducers 4, all of which are positioned to contact the component to be tested.
As mentioned, the present method and device are particularly suited for probing concrete and other hard materials that might exhibit surface irregularities.
Also, it works well without any coupling liquid or paste applied between the transducers and the component. Conventional methods are typically very sensitive to surface irregularities in the absence of such coupling liquid or paste.
Advantageously, each ultrasound receiver comprises one or more tips that are applied to the component while receiving the response signals. Such a design provides a good channel signal separation and is well suited for individually scaling the response signals.
While there are shown and described presently preferred embodiments of the invention, it is to be distinctly understood that the invention is not limited thereto but may be otherwise variously embodied and practiced within the scope of the following claims.
Filing Document | Filing Date | Country | Kind |
---|---|---|---|
PCT/CH2016/000135 | 10/19/2016 | WO | 00 |