• Dr. Arun Kumar Marandi

Unmanned Aerial Vehicles (UAVs) have been created for a variety of military and civilian purposes, including reconnaissance, attack missions, pipeline monitoring, and interplanetary exploration. The goal of this study is to create rapid adaptive UAV design technologies for nimble, fuel-efficient, and flexible structures that can adapt and operate in a variety of situations. The goal of this study is to investigate existing design techniques and understanding of deployable technologies in the field of engineering design and manufacturing in order to create adaptive design technologies. According to the Hashin & Shtrikman theoretical limits, this study aims to find one truss lattice with the best elastic performance for deployable UAV wing design. Three lattice structures are proposed: a 3D Kagome structure, a 3D pyramidal structure, and a hexagonal diamond structure. The suggested lattice structure designs are printed on an Objet 350 3D printer with a polypropylene-like photopolymer named Objet DurusWhite RGD430 as the material. The suggested inflatable wing design, based on compression testing, would combine the benefits of compliant mechanisms and deployable structures to enhance movement flexibility in UAV design and development.

Aerial vehicle, 3D Printing, Manufacturing Industry, Structure, Unmanned Aerial.

"Application of 3D Printing Technology for Designing Light-weight Unmanned Aerial Vehicle Wing Structures ", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.6, Issue 3, page no.549-555, March-2019, Available :http://www.jetir.org/papers/JETIRFT06104.pdf

"Application of 3D Printing Technology for Designing Light-weight Unmanned Aerial Vehicle Wing Structures ", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.6, Issue 3, page no. pp549-555, March-2019, Available at : http://www.jetir.org/papers/JETIRFT06104.pdf