Thomas Menacher, summer semester 2017
The Effect of Defect (EoD) is the evaluation of defects in mainly composite materials and semi-manufactured composite forms. The measured results of a None Destructive Testing (NDT) method are analysed, to compare the data to already existing data of defects. The Effect of Defect analysis is an interaction between none destructive testing, statics and construction.[1]
For component designing three different strategies of construction are possible:
Safe life and fail safe strategies are inefficient with regard to lightweight design. Therefore, most components made out of composite materials are designed to damage tolerance if possible. Manufactured parts (e.g. composite parts) are often evaluated by none destructive testing methods. In professional practice most NDT methods and critical defects are predefined for a specific component. It’s possible that irrelevant defects are detected and relevant defects aren’t detected with this approach. A better way to assure the quality of a component is to create a database to know the appearance of a defect and how critical this specific defect is, before it is detected. [3]
If a defect has been detected while testing, it’s important to know whether the defect is relevant or not. The testing technician should be aware of the relevance of specific defects to predict a component failure or examine a part in case of doubt more precisely. A database can also be combined with an automatized inspection.
Defects in composite materials aren’t inspected with NDT methods for each case. Deliberately drilled holes in CFK laminates are standard for example in aeronautical applications. The hole is for a bolt conjunction between same or different materials. Position, location and dimensions of the defect are known. For these defects characteristic values exist for standard laminates. The effect of defect can be calculated with formulas or with FEM for simple laminate buildups. Additional to the drilled holes, defects like fringes and delamination can emerge as a result of processing steps. [3][4]
Figure 1: Failure mechanisms of bolted composite plies, by [4] |
The first three questions should be answered by none destructive testing. The fourth question can be answered by empirical data.
Defects caused by manufacturing | Defects caused by utilisation |
---|---|
porosity | impact |
ondulations | pull out of fibers |
delaminations | displacement of a layer |
accumulation of resin | bumps |
containments | notches |
missing structure | free cut edge |
cracks | |
break of fiber |
One method creating database is, to characterise systematically a defect (e.g. porosity) with an NDT method (e.g. ultrasound). A second NDT method is needed as a reference. Specimen with the defect (in figure 2: porosity) are scanned with two different NDT methods (in figure 2: ultrasound,CT ). In combination with the reference scan (from CT) the pattern of damage of the defect can be reconstructed. By change systematically the quantity of one defect, a characterisation of the NDT method is gained. The specimen now can be tested for the mechanical properties (e.g. mechanical tensile test to destruction). Mechanical tests have to be adapted to real intended purpose. There is a big difference in the material behaviour of a static load compared to a cyclic load. In figure 2 the approach is visualized. [6]
Figure 2: Characterisation of NDT method and material parameters dependent on a specific defect, by [6] |
Defects can be characterized also, by causing specific defects (e.g. drilled holes, delamination) to a laminate. The defects inside the laminate, in which all parameters are known, are verified with an NDT method. With this step, a characterisation of a specific defect is gained. To characterise the material properties (with defect), mechanical test have to be performed. It’s important to be aware that synthetic imperfections don’t exactly have the same properties like manufacturing induced fatigue induced or impact induced defects. [6]
Real defect | Approach of defect |
---|---|
porosity | hollow spheres out of glass or plastics, drilling holes, insufficient vacuum in autoclave |
foreign objects | insert various targeted materiales |
contaminants | add typical contaminants of manufacturing |
fissures | overload by mechanical load test (e.g. pull test) |
delaminations | dynamic shear loading, film for distance, air cushion |
variation of thickness | more layers at local position |
Figure 3: Two parts of a composite materials glued together, to simulate a delamination |
In contrast to usual materials in mechanical engineering, like steel and aluminium, composite materials are inhomogeneous. This inhomogeneity exacerbates to test with none destructive methods, but also exacerbates databases for particular defects and NDT methods. Because of many different types of composite prepregs , the integral design and many design criteria, almost each part made of composite materials has a different fibre-layup. With different fibre-layups it could be necessary to characterise every new part for defects.
NDT is a part of a quality assurance system. After calibrating , the NDT engineer knows about which imperfections can be detected by applying a specific NDT method. Because of uncertainties, it’s not possible to detect all defects which are theoretically detectable. The goal is, to detect a certain percentage of the detectable defects (compare Probability of Detection (PoD)). With this information and characterisation data stress analysts and statisticians calculate a risk for a manufactured part. Depending on how safety-critical a part is, the construction department has to reconstruct it.