CL-415 Retractable Landing Gear - McGill University Mechanical Engineering
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The design of a retractable landing gear system is crucial for the next generation of short takeoff and landing (STOL) aircraft. Our team at McGill University has successfully developed a novel system, dubbed CL-415, to address this challenge. Key Components: * Actuator: A compact electric motor coupled with a high torque reduction gearbox powers the retraction and extension of the gear. * Gearbox: A custom-designed gearbox enables efficient transmission of power while minimizing weight. * Retraction Mechanism: A dual-cylinder system ensures smooth, controlled movement of the gear. Advantages: * Reduced drag: By retracting the landing gear during flight, aerodynamic performance is significantly improved. * Increased safety: The CL-415 system provides an additional layer of protection in emergency situations. * Enhanced maneuverability: The compact design allows for more agile flight operations.
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