Topology Optimization of Quadcopter Landing Gear using Ansys Mechanical Software

Topology optimization is a powerful design approach that helps engineers create lightweight, high-performance structures by optimizing material distribution based on load conditions. In aerospace applications, reducing weight is crucial for improving efficiency, flight stability, and payload capacity. For a quadcopter, the landing gear plays a vital role in absorbing impact forces during landing while maintaining structural integrity with minimal weight.

Using Ansys Mechanical™ structural finite element analysis software, topology optimization can be performed by defining design constraints, loading conditions, and objectives such as minimizing weight while ensuring sufficient strength and stiffness. Ansys Mechanical Software iteratively refines the structure by removing unnecessary material, resulting in an optimized design that meets performance requirements. This process not only enhances the overall efficiency of the quadcopter but also reduces material usage and manufacturing costs.

In this course, we will perform topology optimization of the landing gear and compare the results with the original, non-optimized geometry to ensure that it can withstand the same load while experiencing reduced stress and mass.

Download the simulation files here to follow this course.