Abstract:Ply wrinkling in carbon fibre reinforced polymer (CFRP) laminates is often geometrically complex and difficult to quantify using non-destructive techniques. In this paper, an ultrasonic technique for mapping ply wrinkling is presented. The instantaneous-phase three-dimensional dataset obtained from a pulse-echo ultrasonic inspection is processed using the structure-tensor image processing technique to quantify the orientations of the internal plies of a CFRP laminate. It is shown that consideration must be giv… Show more
“…Many techniques for detecting fibres and measuring their orientation are seen in the literature [9], spanning many scientific fields. Examples include techniques based on structure tensor [22][23][24][25][26][27][28], Radon transform [29][30][31][32], Fast Fourier Transform (FFT) [14,[33][34][35][36][37][38], rotated filter [39][40][41][42][43][44], and image moment [45][46][47] methods.…”
Section: Fibre-orientation Measurementmentioning
confidence: 99%
“…Whilst the structure tensor has been previously used by the authors to successfully determine out-of-plane ply orientation from ultrasonic data [22], it is not an appropriate method for in-plane fibre orientation. Unlike the smoothly varying ply-orientation field, the fibre-orientation field is likely to feature abrupt changes each side of a resin layer, for example switching from a −45°to a +45°fibre angle.…”
Stacking sequence and, more generally, fibre orientation, are critical parameters in fibrous composite materials since they govern mechanical performance. This paper presents a method, based on the ultrasonic pulse-echo non-destructive technique, that can map the stacking sequence in unidirectional carbon-fibre composites. In-plane fibre orientation is measured using a Radon-transform method applied to local 2D images extracted from the 3D dataset formed from a 2D scan of pulse-echo responses. The ability to align these local 2D images to the plies in the region being assessed makes this technique suitable even in laminates where out-of-plane ply wrinkling is present. The Radon-transform method is shown to provide interpretable stacking-sequence maps, allowing ply lay-up sequence and both in-plane waviness and out-of-plane wrinkling to be visualised and quantified.
“…Many techniques for detecting fibres and measuring their orientation are seen in the literature [9], spanning many scientific fields. Examples include techniques based on structure tensor [22][23][24][25][26][27][28], Radon transform [29][30][31][32], Fast Fourier Transform (FFT) [14,[33][34][35][36][37][38], rotated filter [39][40][41][42][43][44], and image moment [45][46][47] methods.…”
Section: Fibre-orientation Measurementmentioning
confidence: 99%
“…Whilst the structure tensor has been previously used by the authors to successfully determine out-of-plane ply orientation from ultrasonic data [22], it is not an appropriate method for in-plane fibre orientation. Unlike the smoothly varying ply-orientation field, the fibre-orientation field is likely to feature abrupt changes each side of a resin layer, for example switching from a −45°to a +45°fibre angle.…”
Stacking sequence and, more generally, fibre orientation, are critical parameters in fibrous composite materials since they govern mechanical performance. This paper presents a method, based on the ultrasonic pulse-echo non-destructive technique, that can map the stacking sequence in unidirectional carbon-fibre composites. In-plane fibre orientation is measured using a Radon-transform method applied to local 2D images extracted from the 3D dataset formed from a 2D scan of pulse-echo responses. The ability to align these local 2D images to the plies in the region being assessed makes this technique suitable even in laminates where out-of-plane ply wrinkling is present. The Radon-transform method is shown to provide interpretable stacking-sequence maps, allowing ply lay-up sequence and both in-plane waviness and out-of-plane wrinkling to be visualised and quantified.
“…In general, the intention is to measure the full-thickness ultrasonic attenuation and to detect any defects that reflect ultrasound. For characterising wrinkles, a focused probe with a focal depth set at the mid-plane of the material has been shown to be optimal (17) . Whilst the phased-array and FMC/TFM methods using linear arrays were only cylindrically focusing (in one plane), the single-element probe has a spherical focus and this may offer some advantages, although the anisotropy of the material may make this a disadvantage.…”
Section: Single-element Immersion Scanning With a Spherically Focusedmentioning
confidence: 99%
“…Ultrasonic techniques providing an acceptable detail level for 3D characterisation of fibre orientation can be used on large components and allow the inspection of both glass and carbon fibre. The ply lay-up of composite materials can be imaged through the 3D ultrasonic full-waveform scans of the samples (15)(16)(17) . However, unlike Micro-CT, the raw datasets from an ultrasonic inspection do not automatically reveal the ply lay-up using the common 'gate' method of signal analysis.…”
Section: Introductionmentioning
confidence: 99%
“…Current research shows how the depths of the resin layers can be tracked using the instantaneous amplitude, phase and frequency of the ultrasonic response in 3D scans, allowing out-of-plane wrinkles to be mapped within the structure (18)(19) . These instantaneous parameters are defined via the following equation for the analytic signal (17) : (1) where A(t) is the instantaneous amplitude and ϕ(t) is the instantaneous phase at time t. The imaginary part of the analytic signal is calculated by applying a Hilbert transform to the measured (real) waveform (20) . The instantaneous frequency, f(t) is the rate of change of phase at time t in the response at the measurement location and is given (21)…”
Wrinkles, (also known as out-of-plane waviness) are, unfortunately, a common phenomenon that has caused some wind-turbine blades to unexpectedly fail in service. Being able to detect the wrinkles while in the factory will reduce the risk of catastrophic failure and characterising the wrinkles would minimise the repaired area, thus increasing the efficiency of the repair and the design. This work compares the effectiveness of three different ultrasound techniques for detecting and characterising out-of-plane wrinkles in the typical glass-carbon hybrid laminates that are used for wind-turbine blades. The tests samples were manufactured so that the laminates and the defects are representative of those used in the wind-turbine industry. Basic mechanical tests were performed to check the drop in mechanical properties due to wrinkling. The ideal probe frequency was determined as the resonance frequency of the plies using an analytical ultrasonic-propagation model. The three different ultrasound techniques used are: full-matrix capture (FMC) with the total focusing method (TFM), a commercial phased-array instrument and an immersion test with a raster-scanned single-element focused probe. When possible, severity parameters of the wrinkle were measured on the ultrasonic images and compared with the measurements of the actual sample in order to determine which method best characterises such wrinkles and which would be more appropriate to implement in an industrial environment. Not all of the techniques allowed full characterisation of out-of-plane waviness on the specimens. The FMC/TFM method gave better results whilst phased-array technology and single-element immersion testing presented more challenges. An additional enhancement to the TFM imaging was achieved using an Adapted-TFM method with an angle-dependent velocity correction.
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