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Electric Motor Noise for Small Quadcopters: Part I - Acoustic MeasurementsThere is increased interest in using electric motors to drive propulsors across a range of small air vehicle classes. Applications include both vertical lift and conventional takeoff and landing systems for Small Unmanned Aircraft Systems. Mission profiles call for integrating these systems into urban airspaces exposing populated areas to new noise sources. In addition to the propulsor noise from rotors and propellers, electric motors are expected to contribute to the overall sound levels and possibly human annoyance. This work presents acoustic measurements of electric motors used for small quadcopters to characterize the sound and identify sources with and without a propeller. Free field microphone measurements were used to determine directivity and a phased microphone array was used to identify sound sources. A companion paper (Part II – Source Characteristics and Prediction) compares the far field results with current probe measurements of the signal driving the motor, the structural response of the motor case, and describes prediction methods of electric motor noise.
Document ID
20180005231
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Huff, Dennis L.
(NASA Glenn Research Center Cleveland, OH, United States)
Henderson, Brenda S.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 12, 2018
Publication Date
June 25, 2018
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN56469
Meeting Information
Meeting: AIAA Aviation Forum 2018
Location: Atlanta,GA
Country: United States
Start Date: June 25, 2018
End Date: June 29, 2018
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 664817.02.03.02.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Aircraft Noise
Unmanned Aircraft Systems
Electric Propulsion
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