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Design Challenges

                                                                                                         IDETC/CIE/AM3D











              National Taiwan University – R.O.C                      Seoul National University – S. Korea
              Team: Chih-Yu Chen (Team leader), Hung-Chen Yu, Chien-Yen Hsu   Team: Jaejeong Shin (Team leader), Chanjin Park (Team: Heaven Blade)
              (Team: 3D Papa)                                         Topic: Heaven Blade
              Topic: Soft Transformers: A Versatile Platform for Extreme Shape Transfor-
                                                                      From the idea applying the seed’s shape to VAWT (Vertical Axis Wind
              mation
                                                                      Turbine), we suggested a model which is productive and suitable for either
              We propose a novel 3D product manufacturing process by buckling a 2D   accommodation area or appropriate technology. We used CFD (Computa-
              precursor, which came from the idea of 3D pop-up cards, originated from   tional Fluid Dynamics, OPENFOAM) as a simulation tool to evaluate the
              Kirigami, the Japanese art of cutting and folding paper. We aim to   validity of suggested model.
              transform a 2D model into a 3D structure that serves a specific function by
              simply buckling it.
                                                                      B.V.Bhoomaraddi College – India
                                                                      Team: Nikhil Nayak (Team leader), R.B. Lohit, N.N. Anoop (Team: Nikhil)
                                                                      Topic: Design and Study of Wind Solar Hybrid System for Domestic
                                                                      Applications in Rural Areas
                                                                      The proposed work aims at design of wind-solar hybrid system for light
                                                                      load decentralized applications. The computational tools were used to
                                                                      model and analyze wind turbine (WT) blade structure for low power
              Delhi Technological University – India
                                                                      applications to suit decentralized power generation based on renewable
              Team Members: Salman Javed, Farhan Javed (Team: Psi Phi)
                                                                      energy. The comparative studies of test aerofoil with standard NACA0018
              Topic: Design of Multiple Airfoil HAWT Blade Using Programming
                                                                      aerofoil indicated conformance of the test aerofoil as a profile for WT
              The project presents the design and optimization of a small-scale   blades. The test aerofoil has the feature of easier manufacturability as
              horizontal axis wind turbine (HAWT) that is capable of operating efficiently   against standard NACA0018 profile adopted in commercial WT blades.
              at low wind speeds. The self-created code based on BEM theory serves to
              generate an optimum blade profile by making use of multiple airfoils. This
              helps to reduce the design time and hence the manpower cost. The code
              offers the possibility for a common man to set up a small-scale wind
              turbine by using 3D printing.


                                                                      PES University – India
                                                                      Team: Madhavaram Sai Krishna  (Team leader), M.N. Kishore (Team:
                                                                      The Clockworkers)
                                                                      Topic: Optimization of Landing Gear for UAV Applications

                                                                      The project involved design, optimization and development of a UAV
              Notre Dame University – Lebanon                         landing gear structure. Starting with a basic design, topology optimization
              Team: Elie Najem (Team leader), Jad Yazbeck, Ziad Rizk (Team: The   was performed. The objective was to reduce the mass with a constraint to
              Cedars)                                                 maximize the specific strength under operating conditions. In all the main
              Topic: Automated Parking: The Paternoster               landing gear, mass was reduced by 29.2% and the nose landing gear was
                                                                      reduced by 19%.
              Vehicles have become a great part of our lives. However, with the increase
              of the number of automobiles, a parking deficiency problem is arising. To
              overcome this rising issue, this project consists of designing an automated
              parking system.




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