Additive Manufacturing (AM) is an automated process of fabricating three-dimensional (3D) physical objects from a 3D-CAD data by adding layers of materials one upon another through a print head or nozzle without using any tooling components or machining environments. Due to freedom in design, any complex shape can be produced using this process. Fused Deposition Modeling (FDM) is one such AM technology that is commonly used for its simplicity, environment friendliness and low requirement for process monitoring. However, this technology is limited only to small-scale production due to high cost and high build time. The present work focuses on the development of a framework for parametric optimization of the FDM process using multi-objective optimization based on ratio analysis (MOORA). A CAD model of the cam follower mechanism has been prepared in the Solidworks platform and used in this experiment for optimization of build time and cost which have been considered as response variables of the experiment. The experiment has been conducted following the full factorial design of experiment (DoE) method.

To achieve lightweighting of the aircraft landing gear door hinge under opening and closing loads, a topological optimization model based on the variable density method was established, with structural stiffness as the constraint and minimum mass as the objective. The hinge was redesigned according to the optimized configuration, and the stiffness and strength of the design area were validated. The original aluminum alloy hinge material was replaced with lower-density polyetheretherketone (PEEK), which can be fabricated into complex structures via fused deposition modeling (FDM), thereby enhancing design freedom for topology optimization. However, FDM-printed PEEK's mechanical properties are influenced by printing parameters. This study conducted tensile tests on PEEK specimens printed with different FDM parameters (e.g., layer height, platform temperature, and infill pattern). The optimal printing parameters were determined as 0.1 mm layer height, 120 °C platform temperature, and tetrahedral infill. Subsequently, the best-performing specimens underwent heat treatment, and the effects of different annealing parameters on tensile strength were investigated. The results showed that annealing at 330 °C for 2 hours yielded the highest strength improvement. Furthermore, the hinge's loading conditions during door operation were simulated via multi-body dynamics analysis, while static simulations under peak loads identified stress concentration areas. Topology optimization was then performed to minimize material usage while maintaining mechanical performance, achieving the lightweight goal.

Additive manufacturing has been one of the most used techniques in the recent years because of its capabilities to fabricate complex structures as required by customer and industrial need from a 3D computer-aided design model without the usage of any tooling, dies and heavy machinery makes it a step ahead in the present manufacturing techniques. In the current study the author’s focus on the welding or joining of additive manufactured Polylactic acid (PLA) parts made by Fused Deposition Modeling (FDM). There are several techniques for welding these additive manufactured parts. This study mainly focuses on the joining of 3D printed PLA parts using a 3D pen and investigations on its mechanical properties experimentally. It is a very cheap and effective technique when compared to the other welding methods. This could overcome the drawback of small bed size in most 3D printers by joining smaller parts and it can also be used for repairing the defects caused during the 3D printing. Moreover the experimental testing of the mechanical properties also confirmed that the tensile, flexural and impact strength of 3D pen welded specimens retrieved above 70% of the strength to the original PLA specimen proving it to be a very effective method.

The application of Fused Deposition Modeling (FDM) is restricted due to limited information about the mechanical properties of printed parts. Therefore, it is required to determine the mechanical properties of the FDM properties to avail the full benefit of the FDM process. In the present study, Classic Laminate Theory (CLT) has been employed at the different configurations of layer thickness and raster width. The required elastic constant of material for CLT has been experimentally obtained through FDM printed Polylactic Acid (PLA) unidirectional specimens at 0°, 45° and 90° for different combinations of layer height and raster width. For these different combinations of layer height and raster width, constitutive models were developed to predict the tensile properties of the PLA parts. Tensile strength of the FDM printed bi-directional specimens has been experimentally obtained to validate the proposed CLT model results. The experimental tensile strength data is in good agreement with the data predicted by the proposed CLT model. Higher tensile strength and modulus were achieved with 0° raster angle compared to 90° raster angle. In the case of a bi-directional printed specimen, higher tensile strength was obtained with 45°/-45° raster angle followed by 30°/-60° and 0°/90° raster angle.