Imaging of porosity/voiding in carbon fibre laminate
 

 

Composites

Wavelength NDT have extensive experience of investigating many types of composite materials using standard and advanced inspection techniques. Some examples of the type of work we undertake are listed below and in our applications pages, but please contact us if you require further information for your particular application.

Impact damage

Impact damage can quickly be identified using conventional A-scan ultrasonic inspection or advanced phased array B-scan and C-scan techniques. In most cases the extent of damage can be quantified providing important information for stress and design engineers.

Porosity and void detection

Evidence of porosity can be detected in a number of ways including simple A-scan measurements through to detailed B-scan and C-scan analysis of the ultrasound echo position and amplitude.

Repair patches

Wavelength NDT routinely inspect repaired laminate and can assess the degree of bonding between the repair and original laminate and detect problems such as voiding and porosity in the repair laminate.

Fibre waviness (wrinkles)

Using the latest technology, ultrasonic imaging of in-plane and out-of-plane fibre waviness can be performed and quantitative measurement of the fibre angle made. Wavelength NDT have developed approved techniques for out-of-plane waviness assessment in carbon and glass fibre laminates.

Bonding

Depending on the structure design and material, several bondtesting techniques are possible. Wavelength NDT routinely use A-scan and C-scan ultrasound inspection techniques for monolithic carbon fibre laminates and lower frequency acoustic and digital tap testing methods for glass fibre laminates and cored structures.

Complex composites

More complex forms of composite structures such as cored materials (e.g. Rohacell/Nomex), multilayer sandwich (e.g. GLARE), or hybrid structures can present significant challenges for the NDT engineer. Wavelength NDT have experience of inspecting a range of cored laminates in the Aerospace and Marine sectors using high and low frequency ultrasound and acoustic techniques such as mechanical impedance, resonance, pitch-catch testing and digital tap testing.

Example inspection

The following interactive image shows the relationship between the raw A-scan data and the cross-section B-scan and the C-scan images. By moving the mouse over the features in the C-scan image (bottom two displays) changes in the A-scan signal and B-scan images can be observed which help the operator understand what is happening inside the structure.

Example C-scan data - move your mouse on the bottom two C-scan image and see the change in the A-scan and B-scan displays

 

 

Thickness C-scan showing depth of delaminations in impact zone

Amplitude C-scan showing edges of delaminations in impact zone

A-scan image from porous CFRP laminate

Macro photograph of ply waviness

C-scan showing variation of bonding in a carbon fibre laminate

Honeycomb panel construction

C-scan ultrasound image of honeycomb cell bonding

 

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