| Citation: | MIN Sikai, HUANG Xianghua, LUO Liantan, et al. Interference noise reduction research of multiple propellers based on frequency domain method[J]. Journal of Aerospace Power, 2024, 39（12）：20220997 doi: 10.13224/j.cnki.jasp.20220997
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A fast prediction method for rotational noise of multi-propellers was presented in order to study the mechanism of synchrophasing noise reduction of multi-propellers. Combined with the strip theory and the Hanson frequency domain model, this method was used to predict the noise of single propeller, and the model was extended to consider the direction of rotation in the case of multi-propellers based on linear theory. The proposed method had a single point prediction time of only 20 ms and an maximum error of 4.03 dB when compared with experiment data from literature. The parameters affecting its performance were investigated. The results indicated that the flight altitude, Mach number, and installation distance had a small impact on the noise reduction performance, ranging from 1 dB to 5 dB, while the number of blades and rotational speed had a larger impact, ranging from 8 dB to 10 dB. The noise reduction effect was more significant for multi-blade configurations and multi-rotor aircraft.
| [1] |
BLUNT D M. Altitude and airspeed effects on the optimum synchrophase angles for a four-engine propeller aircraft[J]. Journal of Sound and Vibration,2014,333(16): 3732-3742. doi: 10.1016/j.jsv.2014.03.038
|
| [2] |
BLUNT D M. Optimisation and adaptive control of aircraft propeller synchrophase angles[D]. Adelaide,Australia: The University of Adelaide,2012.
|
| [3] |
JOHNSTON J F,DONHAM R E,GUINN W A. Propeller signatures and their use[J]. Journal of Aircraft,1981,18(11): 934-942. doi: 10.2514/3.57583
|
| [4] |
GALLES M B,SCHILLER N H,ACKERMAN K A,et al. Feedback control of flight speed to reduce unmanned aerial system noise: AIAA2018-2950[R]. Reston,US: AIAA,2018.
|
| [5] |
GUTIN L. On the sound field of a rotating propeller[R]. Washington DC: National Advisory Committee for Aeronautics,1948.
|
| [6] |
PASCIONI K,RIZZI S,AUMANN A. Auralization of an unmanned aerial vehicle under propeller phase control[C]//Proceedings of INTER-NOISE and NOISE-CON Congress and Conference,Chicago,US: Institute of Noise Control Engineering,2018: 421-431.
|
| [7] |
PASCIONI K,RIZZI S A. Tonal noise prediction of a distributed propulsion unmanned aerial vehicle: AIAA2018-2951[R]. Reston,US: AIAA,2018.
|
| [8] |
PASCIONI K A,RIZZI S A,SCHILLER N. Noise reduction potential of phase control for distributed propulsion vehicles: AIAA2019-1069[R]. Reston,US: AIAA,2019.
|
| [9] |
PATTERSON A,GAHLAWAT A,HOVAKIMYAN N. Propeller phase synchronization for small distributed electric vehicles: AIAA2019-1458 [R]. Reston,US: AIAA,2019.
|
| [10] |
PATTERSON A,SCHILLER N H,ACKERMAN K A,et al. Controller design for propeller phase synchronization with aeroacoustic performance metrics: AIAA2020-1494[R]. Reston,US: AIAA,2020.
|
| [11] |
CHIRICO G,BARAKOS G N,BOWN N. Propeller installation effects on turboprop aircraft acoustics[J]. Journal of Sound and Vibration,2018,424: 238-262. doi: 10.1016/j.jsv.2018.03.003
|
| [12] |
MARINUS B,ROGER M,BRAEMBUSSCHE R V D,et al. Truncated method for propeller noise prediction up to low supersonic helical tip Mach numbers: AIAA2009-3330[R]. Reston,US: AIAA,2009.
|
| [13] |
TAN C H,VOO K S,SIAUW W L,et al. CFD analysis of the aerodynamics and aeroacoustics of the NASA SR2 propeller[C]//Proceedings of ASME Turbo Expo 2014: Turbine Technical Conference and Exposition. Düsseldorf,Germany: ASME,2014: 26779-26790.
|
| [14] |
HAMBREY J,FESZTY D,MESLIOUI S A,et al. Acoustic prediction of high speed propeller noise using URANS and a Ffowcs Williams-Hawkings solver: AIAA2017-3917[R]. Reston,US: AIAA,2017.
|
| [15] |
FFOWCS-WILLIAMS J E,HAWKINGS D L. Sound generation by turbulence and surfaces in arbitrary motion[J]. Philosophical Transactions of the Royal Society of London Series A,Mathematical and Physical Sciences,1969,264(1151): 321-342.
|
| [16] |
KOTWICZ H,FESZTY D,MESLIOUI S A,et al. Evaluation of acoustic frequency methods for the prediction of propeller noise[J]. AIAA Journal,2019,57(6): 2465-2478. doi: 10.2514/1.J056658
|
| [17] |
KOTWICZ H,FESZTY D,MESLIOUI S,et al. Applicability of early acoustic theory for modern propeller design[C]//Proceedings of the 23rd AIAA/CEAS Aeroacoustics Conference. Denver,US: AES,2017: 3865-3884.
|
| [18] |
DEMING A F. Noise from propellers with symmetrical sections at zero blade angle[R]. Washington DC: National Advisory Committee for Aeronautics,1938.
|
| [19] |
MAGLIOZZI B,METZGER F,BAUSCH W,et al. A Comprehensive review of helicopter noise literature[R]. Washington DC: Federal Aviation Administration,1975.
|
| [20] |
HANSON D B. Near-field frequency-domain theory for propeller noise[J]. AIAA Journal,1985,23(4): 499-504. doi: 10.2514/3.8943
|
| [21] |
HUANG Xianghua,SHENG Long,WANG Yangyang. Propeller synchrophase angle optimization of turboprop-driven aircraft: an experimental investigation[J]. Journal of Engineering for Gas Turbines and Power,2014,136(11): 112606. doi: 10.1115/1.4027644
|
| [22] |
SHENG L,CAMINO F M,HUANG X H. Synchrophasing control based on tuned adrc with applications in turboprop driven aircraft[J]. Control Engineering and Applied Informatics,2018,20(2): 100-108.
|
| [23] |
曹云飞,黄向华,盛龙,等. 一种提高螺旋桨相同步噪声模型辨识精度的方法[J]. 推进技术,2018,39(11): 2571-2580. CAO Yunfei,HUANG Xianghua,SHENG Long,et al. A method for improving identification accuracy of propeller synchrophasing noise model[J]. Journal of Propulsion Technology,2018,39(11): 2571-2580. (in Chinese
CAO Yunfei, HUANG Xianghua, SHENG Long, et al. A method for improving identification accuracy of propeller synchrophasing noise model[J]. Journal of Propulsion Technology, 2018, 39(11): 2571-2580. (in Chinese)
|
| [24] |
刘沛清. 空气螺旋桨理论及其应用[M]. 北京: 北京航空航天大学出版社,2006. LIU Peiqing. Air propeller theory and its application[M]. Beijing: Beijing University of Aeronautics & Astronautics Press,2006. (in Chinese
LIU Peiqing. Air propeller theory and its application[M]. Beijing: Beijing University of Aeronautics & Astronautics Press, 2006. (in Chinese)
|
| [25] |
DITTMAR J H. Cruise Noise of the Sr-2 Propeller Model in a Wind Tunnel: NASA TM-101480[R]. Cleveland,US: NASA Lewis Research Center,1989.
|
| [26] |
DOBRZYNSKI W M,HELLER H H,POWERS J O,et al. Propeller noise tests in the german-dutch wind tunnel dnw[R]. Washington DC: Federal Aviation Administration 1986.
|
| [27] |
CHEN B,YAKOVLEV A A,MOSHKOV P A. Fast prediction method of aircraft noise with distributed propulsion in the far field[J]. Journal of Physics: Conference Series,2021,1925(1): 012007. doi: 10.1088/1742-6596/1925/1/012007
|
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