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Materials Science in Additive Manufacturing                               Fast fiber orientation optimization














                              Figure 7. Distribution of the principal directions. Left: Tensile stress. Right: Compressive stress.

            sets of printed parts were tested and then compared. The   A
            first set was built with an alternation of −30° oriented
            fibers (Figure  8A)  and 0°  oriented  fibers (Figure  8B),
            corresponding to the intuitive fiber orientation. The second
            set has an alternation of the optimized angles computed
            in section 3.1 with the corresponding percentage: Seven
            layers with 2° oriented fiber, one layer at −33°, one layer
            at −17° and one layer at 13°. The parts were printed with   B
            a Markforged X7 printer using a continuous carbon fiber
            filament (blue routes on  Figure  8). A  nylon filament
            (white routes on Figure 8) was used for the roof and floor
            layers, which are mandatory with this printer.
              Each wrench contains the same fiber content, only the
            orientation of the fiber changes. To be able to estimate the
            dispersion on the test results, three wrenches were printed
            for each fiber laminate. The six parts were tested with a   Figure  8. Printing routes with −30° oriented fibers (A) and 0°
                                                               oriented fibers (B).
            compressive plate set on a Lloyds Instruments LR 50K. The
            wrench’s head was locked inside a vice and leant on a steel
            plate to be locked vertically (Figure 9).
              Figure 10 shows the force-displacement curves of the
            six tested parts. There is a low dispersion in the results
            from  one  part  to  another  of  the  same  batch,  which
            makes the results relevant. It appears that the optimized
            parts are stiffer than the non-optimized ones. In fact, the
            optimization of the layers’ fiber angles has increased the
            stiffness of the printed parts by a significant improvement
            of 18%. This proves the usefulness of the optimization
            process compared to an intuitive reinforcement (0°/−30°).

            3.3. Comparison with an optimization model
            To check whether our quick method gives a result close to
            the optimal solution, we compared it to a solution obtained        Figure 9. Testing setup.
            with an optimization model.
              A direct optimization model with a Non-linear    with 60 layers, which would require 60 parameters as well.
            Programming Quadratic Line Search (NLPQL) algorithm   However, the mechanical case was close to a 2D problem,
            was used with the Ansys Workbench software. The objective   as the load was set in the XY-plane. This was confirmed
            is to minimize the maximal displacement. Each layer’s   by the fact that our code gave the same angle sequence
            angle was set as a parameter initialized to 0° with a range   for each stack. Thus, the direct optimization method
            of variation between −90° and 90°. The main issue, which   was applied on only ten layers of the wrench. Figure 11
            led us to develop the quick method presented before in   shows the convergence of the model, which required 11
            the first place, is that it is difficult to implement this model   iterations to obtain the optimal (i.e., the lowest) maximal
            with many parameters. In our case, the wrench was built   displacement within the part. Hence, a sequence of 10° was


            Volume 2 Issue 1 (2023)                         6                        https://doi.org/10.36922/msam.49
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