Submitting Campus
Daytona Beach
Department
Aerospace Engineering
Document Type
Patent
Publication/Presentation Date
11-15-2018
Abstract/Description
A system and method of noise mitigation for hybrid and electric aircraft, the aircraft having a controllable pitch propeller or rotor(s) with a plurality of blades. The propeller or rotor(s) are driven by a drive system to provide thrust for the aircraft, and the blades of the propeller or rotor(s) are further movable about pivot axis to vary a pitch thereof. A controller on-board the aircraft is operable to cause rotation or movement of the blades of the propeller or rotor(s) about their pivot axis to alter and/or focus at least one aspect of the propeller generated noise to reduce or mitigate such noise while maintaining a substantially constant thrust, altitude, and/or air speed of the aircraft.
Patent Number
US 2018/0327081 Al
Assignee
Embry-Riddle Aeronautical University
Application Number
15/975,220
Date Filed
5-9-2018
Scholarly Commons Citation
Gartenberg, L., Anderson, R. P., & Martos, B. (2018). Systems and Methods for Noise Mitigation for Hybrid and Electric Aircraft. , (). Retrieved from https://commons.erau.edu/publication/2177
