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Tonal Noise Control Using Rotor Phase SynchronizationThe purpose of this study is to determine if phase synchronization can be used to reduce the net radiated sound power from two rotors. Phase synchronization implies that the rotors have the same rotational speed with a fixed relative azimuthal blade position, or phase. The concept is evaluated both experimentally and numerically. Measurements of source directivity and thrust are initially compared with predictions to confirm that the model accurately captures the relevant trends. The model is then used to explore the design space and identify relevant parameters. Both experimental and numerical results show that the radiated sound power at the blade passage frequency can be reduced by appropriately controlling the relative azimuthal phase of the rotors. Vehicle level predictions are also provided for a notional octocopter, comparing two different modes of operation. Predictions show that phase synchronization can be used to achieve a 4-5 dB reduction of the sound pressure level at the blade passage frequency nearly everywhere on the ground plane beneath the vehicle.




Document ID
20200002608
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Noah H Schiller
(Langley Research Center Hampton, Virginia, United States)
Kyle A Pascioni
(Langley Research Center Hampton, Virginia, United States)
Nikolas S Zawodny
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
April 17, 2020
Publication Date
May 13, 2019
Subject Category
Acoustics
Report/Patent Number
NF1676L-31452
Meeting Information
Meeting: Vertical Flight Society Annual Forum and Technology Display (VFS Forum 75)
Location: Philadelphia, PA
Country: US
Start Date: May 13, 2019
End Date: May 16, 2019
Sponsors: Vertical Flight Society
Funding Number(s)
WBS: 664817.02.07.03.02.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
LAR-19382-1
Patent Application
App. No. 16/597,499 Publication No. US2020/0108913
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