Cycloidal Propulsion for UAV VTOL Applications

The proposed effort will result in the development and wind tunnel validation of a universal pitch cycloidal propeller system which can provide efficient vertical takeoff or landing (VTOL) UAV propulsion. This form of propulsion is currently in use in marine applications, and has been studied by major aircraft manufacturers and the military. Study and wind tunnel test results support the concept; however, until the advent of the micro-computer and associated motion control technologies, efficient cycloidal propellers were only feasible for relatively narrow speed ranges. This effort will capitalize on computer control to provide a universal pitch cycloidal propeller that will allow efficient flight across a wide range of flight speeds and conditions. Cycloidal propulsion provides a unique 360-degree directional flight capability through use of a low-velocity, high-volume flow technique of exceptional efficiency. The cycloidal propeller, which provides both thrust and lift, can make near instantaneous change in thrust direction without re-orientation of the propellers plane of rotation. Major advantages of this system include efficient hovering flight, low-noise signature, near-instantaneous change in thrust direction, wide speed range, safety, and packaging. BOSCH Aerospace, Inc., has teamed with the Raspet Flight Research Center of Mississippi State University to conduct Phase 1. The research will encompass systems engineering, mechanical design, computer modeling, control algorithm development, fabrication, and wind tunnel tests. A fully functional propeller and control system will be completed and tested during Phase 1. Documentation from this effort will include study, design, and tests results.