- since 1996 -
|NDT.net Issue - 2014-08 - NEWS ||NDT.net Issue: 2014-08|
Publication: e-Journal of Nondestructive Testing (NDT) ISSN 1435-4934 (NDT.net Journal)
Latest technology for non-destructive testing of compositesAshtead Technology16, Letchworth Garden City, United Kingdom
In the following article, Neil Harrap, NDT Market Manager at Ashtead Technology, explains how the latest testing technology can be employed to improve the ease and efficiency with which composite materials can be evaluated.
Most composites consist of a bulk material, the matrix, and a reinforcement which is usually in fibre form. Broadly speaking, composites can be divided into three main groups:
In contrast with most other manufactured materials, composites are non-homogenous (not uniform in structure or composition) and anisotropic (have properties that differ according to the direction of measurement). In addition, composites vary enormously in terms of shape and thickness. Testing therefore presents a number of challenges and a wide variety of testing procedures exist: compressive strength, content analysis, flexural properties, moisture absorption, shear response, tensile testing etc. However, all of these tests are destructive so Non-Destructive Testing (NDT) is required to assess materials that are either in the manufacture stage or in service.
Flaws that are not visible to the eye can have serious, if not catastrophic, effects on the ability of a composite to perform to its specification. Examples of composite flaws include delamination, disbond, translaminar cracking, voids, fibre breakage etc. These flaws can be created by incorrect manufacture or curing conditions, or they might occur as a result of operational stress, impacts or environmental factors such as temperature or humidity.
NDT Inspection Technology
Inspection work has been simplified by an intuitive step-by-step wizard that takes the operator through the process; ensuring that inspections are effective and fast. The MX2 also features the industry-standard phased array user interface with a bigger (26.4 cm) and brighter screen which has unique intuitive touch-screen capabilities, and faster data transfer. Generated images are based on 3 planes so the quality of reports is improved and with easier recording and archiving of data, higher levels of accountability are possible for composite inspection. This capability is also advantageous in situations where very low, acceptable, levels of disbond are identified and subsequently regularly monitored.
Composite testing options
Bond testing can be performed by the MX with ECA module, and BondMaster® probes. The combination of these technologies increases the probability of detection of the pitch-catch bond testing method, because live amplitude or phase C-scan images with up to 8 frequencies are created.
Any two-axis encoding scanner can be used with this system. For example, the GLIDER™ scanner is ideal for flat or slightly curved surfaces, and the WING™ scanner is specially designed for scanning curved parts (e.g., aircraft fuselages) and can even be used upside-down due to its vacuum-cup system.
Many components manufactured as composites, such as skins, stringers, and spars, consist of relatively flat sections, for which a complete inspection solution is available. For example, the Carbon-Fibre-Reinforced Polymer (CFRP) flat panel inspection solution is based on the MX2, a GLIDER™ scanner, in addition to probes and specific wedges developed for CFRP flat panel inspection. This solution offers advanced features, such as two-axis encoded C-scans with amplitude and time-of-flight (TOF) information, gate synchronisation, and data recording.
Too often, engineers are wary of new technology, fearing that its use may incur a greater need for training, in addition to a significant period of familiarisation. However, whilst the MX2 has been developed to offer new levels of inspection productivity, the designers have retained a focus on simplicity; operation is highly intuitive and new users can become fully operational very quickly.
For further information, contact: