Design and development of the prototype of a landing gear model for demonstration purposes

This project is designed for the students to elaborate on the working of landing gear and its parts. I will be made mechanism of landing gear in which torsion link is used to reduce the drag and also be a low-cost project.

Project Title

Design and development of the prototype of a landing gear model for demonstration purposes

Project Area of Specialization

Mechatronics Engineering

Project Summary

This project is designed for the students to elaborate on the working of landing gear and its parts. I will be made mechanism of landing gear in which torsion link is used to reduce the drag and also be a low-cost project.

Project Objectives

The need to design a landing gear with minimum weight, minimum volume, high performance improve life, and reduce life cycle cost poses many challenges. Further, the design and development cycle time of landing gear should be compressed to reduce costs and to bring the product to market faster. These challenges are met, while adhering to all regulatory requirements of safety, by employing advanced technologies, materials, processes, analysis, and production methods.

Project Implementation Method

In the landing gear assembly of an aircraft, the torque links connect the two telescoping cylinders and prevent the relative rotation of the piston to maintain the wheel alignment during taxiing on the ground.

However, it contributes to the dead weight during the flight of the aircraft. Thus, reducing the weight of the torque link will turn down the overall weight of the aircraft. This can improve fuel economy which in turn will benefit the aviation industry marketable. The door’s system is installed to achieve the best aerodynamics for fuel economy.

Then we use the software-based in which coding is used in running the command circuit, by Arduino software.

Benefits of the Project

This will be beneficial for the general aviation industry for fuel economy as well as performance. This is utilized in a small RC plane.

The need to design a landing gear with minimum weight, minimum volume, high performance improve life, and reduce life cycle cost poses many challenges. Further, the design and development cycle time of landing gear should be compressed to reduce costs and to bring the product to market faster. These challenges are met, while adhering to all regulatory requirements of safety, by employing advanced technologies, materials, processes, analysis, and production methods.

Technical Details of Final Deliverable

1. Design and development of landing gear mechanical structure
2. Design and development of control circuitry
3. Development of a lab model for demonstration

Final Deliverable of the Project

HW/SW integrated system

Core Industry

IT

Other Industries

Manufacturing , Media

Core Technology

Augmented & Virtual Reality

Other Technologies

Others

Sustainable Development Goals

Industry, Innovation and Infrastructure

Required Resources

If you need this project, please contact me on contact@adikhanofficial.com