Abstract
Abstract: Landing Gear is proved to be the most critical subsystems in aircraft. It is a crucial part in all ground operations, takeoff and landing of aeroplane. Landing gear operates as dead weight after an aircraft is in the air, burning more fuel and taking up room which can be used for other safety measures. When taking into account all the legal and safety standards, it is vital to shorten the time needed for the landing gear design and its development cycle. All aerospace sectors strive for attributes such as minimal weight and volume, great performance, and reduced life cycle costs. Our objective was to create a landing gear with the least amount of weight and volume while maintaining maximum structural integrity. To achieve this goal, we designed landing gear links using generative design. In addition to this, we also studied different parameters considered for landing gear design.
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