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Typical wing skin joint configuration showing sealant and fastener locations. Possible crack locations are shown in black to the left and right of the fastener.

Typical wing skin joint configuration showing sealant and fastener locations. Possible crack locations are shown in black to the left and right of the fastener.

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There has been an increase in the use of composite materials in the aerospace industry which is driving a need for new NDT techniques that can rapidly scan large structures and provide quantitative data on the material integrity. In many applications there are common requirements for the ultrasonic inspection of composites for porosity, delaminatio...

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... It implements multiple ultrasonic transducers, adjusting the timing and amplitude, and combines the resulting waves. It provides high resolution and high efficiency; with the newly developed methods like the time reversal technique [10] and wheel probe [11], it can compensate for the misalignment between the probe and composite or detect curved edges and narrow components. ...
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... They also successfully developed a curved-surface transducer with a radius of curvature of 15 mm [116]. To inspect large-area aerospace composite components, Freemantle et al. [117] installed a phased array in rubber wheels to effectively detect delamination and wrinkles in aerospace composite components. Research on the application of phased arrays for damage detection in composite materials is summarized in Table 3. Owing to the complexity of wave propagation in composite materials, phased-array detection with delayed transmission, in which all the elements are fired to form a beam with a fixed focus, is rarely utilized. ...
... Pulse-Echo technique utilizes a single transducer placed along the surface which acts as a transmitter as well as a receiver. It is applicable where inspection scan is limited to as single surface [5]. A review of studies in this area confirmed that this technique is most sensitive to imperfections such as delamination which lies parallel to the surface whereas imperfections that lie perpendicular to surface such as matrix cracks and fibre fractures are hard to detect [4]. ...
... It has higher resolution and reliability compared to the traditional NDT methods and holds notable capabilities in case of aircraft components. In [5], a wheel probe is developed using this technique which scans curved edges and narrow components with high efficiency. It is used to detect impact damage, fibre lay-up and porosity in the structures. ...
... Through conventional UT testing, ultrasound waves are sent into the material through a single transducer, while PA probes have multiple transducers. 4 Through a delay generation within the pulses sent out by each transducer, the beam angle, focal point, and focal spot of the produced wavefront are affected, making PA a versatile method for the inspection of complex geometries. 5 Titanium (Ti) and its alloys due to their high corrosion and wear resistance, 6 high strength, 7 biocompatibility, 8 high melting point, non-toxicity, 9,10 resistant to chemical attacks, low thermal expansion, and excellent machinability 11,12 are utilized extensively in the industrial applications. ...
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... Phased array and some special equipment are combined to achieve better testing effect or larger testing range. Habermehl et al. [76] and Freemantle et al. [77] have combined the ultrasonic phased array system to provide a new solution for defect detection of large CFRP components (see Figure 7). The ultrasonic array is placed on a rubber-coupled wheel, and the wheel can be manually applied or scanned by the structure and automatic scanning system, which can realize the inspection of a large composite structure. ...
... The ultrasonic array is placed on a rubber-coupled wheel, and the wheel can be manually applied or scanned by the structure and automatic scanning system, which can realize the inspection of a large composite structure. The glide scanner and phased array are combined [77]. [78]. ...
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... To that end, an extreme effort is continuously invested towards the improvement of aircraft inspection worthiness and the development of reliable, automated, and synergistic techniques for capturing barely visible damage on aircraft. Currently, manual point-topoint inspection using conventional ultrasonic transducer and line-by-line Phased Array (PA) wheel probe [4] are used as a fundamental quantitative method, as per schedule-based maintenance for in-service inspections of composite skin surfaces. Such inspections are tactical and categorized in A-, C-, and D-checks, depending on the level of detail with respect to the aircraft age, hours in service, and the number of landing/take-off cycles. ...
... An ultrasonic inspection typically requires the use of free-flowing water, a film of water, local immersion, or ultrasonic gel as a coupling medium between the transducer and surface under inspection. The restriction of existing methods of couplant usage by VR platform requirements was addressed by developing a new wedge of elastomer material that is similar to a wheel probe roller material [4], which has low attenuation, low acoustic impedance, and lower couplant requirements. The wedge thickness was optimized for a 10 MHz PA transducer that is based on ultrasonic beam characteristics, near-field length, and attenuation in the elastomer material. ...
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... The ability of ultrasonic waves to propagate in composite materials enables detection of damage location and size [26]. Phased Array scanning is a handheld ultrasonic NDT technique, that can detect the presence of damage in composite structures, such as delamination and debonding [27,28]. This is achieved through the pulsing of ultrasonic waves from transducers in a linear array. ...
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... On the basis of conventional UT, more advanced methods have been developed such as phased array ultrasonic testing [75,76]. Nowadays, phased array sensors can be integrated with time reversal techniques [77] that compensates for the misalignment between the probe and composite structure (due to complex geometry of aerospace composites), and increases the coverage area of sensor [78]. ...
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... High wave attenuation associated with the composite properties and high frequency transducers limits the inspection on large complex structures. Ultrasonic phased array [7] and tomography [8] have recently been utilized more in aircraft SHM as they can produce high resolution images. However the biggest problem with these methods is the requirement of good coupling and a constant angle of incidence for reproducible inspection results. ...
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Low-velocity impact on composites typically produces a barely visible damage at the impacted surface. The internal defects can be complex, consisting of multimode damage and the extent of the impact damage normally spreads across the thickness under the impacted surface. The characterization of impact damage in composites can be very complicated and varies for every different composite structure. In this paper, independent characterization of the low-velocity impact damage on carbon-fiber/epoxy plates using three different non-destructive evaluation methods were used. The goal is to demonstrate the ability of guided ultrasonic waves imaging technique and compared to the more widely employed techniques such as X-ray imaging and ultrasonic immersion C-scan. It was demonstrated that the low frequency A0guided ultrasonic wave mode generated by a low-cost piezoelectric transducer can be successfully employed to detect impact damage in composite plates and managed to estimate the size and shape of the impact damage.