DESIGN OF OPTIMIZED KINEMATIC LINKAGES FOR MAIN ROTOR CONTROL SYSTEM FOR HELICOPTER TO HAVE SIMPLIFIED MECHANISM

摘要

In order to transfer the pilot inputs to the Main Rotor, design of kinematics for Main rotor controls with introduction of a lever in between MRA and NRSP helps in: Reducing the lower flight control loads Reducing out stroke of Main Rotor Actuator Reducing weight of the Main Rotor Actuator Simplifies the NRSP design Simplified and weight reduced upper and lower flight control mechanism.