Design and Analysis of mechanical link for Tejas flight actuator

Highlights 🔗

• Contributed to component design in Autonomous flight control system
• Focused on prediction of structural failure in aircraft structures
• Designed structural component in CATIA and performed analysis in ANSYS

Problem Statement 🔗

• Aim is to improve structural strength and address the issue of flight control actuator play

Ideation 🔗

Solution Methodology 🔗

Results and Conclusion 🔗

• Published research work on " Conceptual Design and Analysis of Link for Arresting
• Slat actuator Play in Tejas Aircraft " in an International Journal of Basic and Applied Engineering Research - Print ISSN: 2350-0077; Online ISSN: 2350-0255;