Tonal noise reduction by unevenly spaced blades in a forward-curved-blades centrifugal fan

被引:30
作者
Jiang, Boyan [1 ]
Wang, Jun [1 ]
Yang, Xiaopei [1 ]
Wang, Wei [1 ]
Ding, Yanyan [1 ]
机构
[1] Huazhong Univ Sci & Technol, Sch Energy & Power Engn, Wuhan 430074, Hubei, Peoples R China
关键词
Forward-curved-blades centrifugal fan; Fan tonal noise; Computational aeroacoustics; Uneven blade spacing; Blade spacing modulation; AXIAL-FLOW FANS; AERODYNAMIC NOISE; TURBULENCE;
D O I
10.1016/j.apacoust.2018.11.007
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
Tonal noise is an essential characteristic of the noise generated from a forward-curved-blades centrifugal fan. Herein, methods to unevenly arrange blades, in particular, a random modulation method, were studied to weaken the undesired tonal noise and reshape the noise spectrum. First, the balance and aerodynamic performance requirements of the impeller were considered when designing the unevenly spaced blades. The modulated blade positions had to satisfy the dynamic balance condition, while the variation of spacing between every two adjacent blades should not exceed 30% of the original spacing in the even impeller. Next, the influence of non-uniform blades on the noise spectrum characteristics of the fan was theoretically predicted by calculating the interference functions at each discrete frequency. Finally, computational fluid dynamics and computational aeroacoustics analyses were performed to investigate the acoustic performance of each uneven blade spacing scheme. Both the pressure fluctuation on the tongue and the noise frequency spectrum from the acoustic receiver demonstrated that unevenly spaced blades could reduce the tonal noise by dispersing the acoustic energy at the blade passing frequency to other specific frequencies as a form of sidebands. Compared with the existing sinusoidal modulation method, the random modulation method has no limits on the blade number. Moreover, this method has a higher degree of freedom that could overcome all limitations of blade spacing. It is shown that a reasonable blade distribution designed by this method could reduce tonal noise without negatively affecting the aerodynamic performance and the overall noise level. (C) 2018 Elsevier Ltd. All rights reserved.
引用
收藏
页码:172 / 183
页数:12
相关论文
共 26 条
[1]   Psychoacoustic Optimization of the Spacing of Propellers, Helicopter Rotors, and Axial Fans [J].
Anghinolfi, Davide ;
Canepa, Edward ;
Cattanei, Andrea ;
Paolucci, Massimo .
JOURNAL OF PROPULSION AND POWER, 2016, 32 (06) :1422-1432
[2]  
[Anonymous], 2011, ANSYS FLUENT 14 0 US
[3]   The influence of uneven blade spacing on the spl and noise spectra radiated from radial fans [J].
Boltezar, M ;
Mesaric, M ;
Kuhelj, A .
JOURNAL OF SOUND AND VIBRATION, 1998, 216 (04) :697-711
[4]   Reduction of the tonal noise annoyance of axial flow fans by means of optimal blade spacing [J].
Cattanei, Andrea ;
Ghio, Riccardo ;
Bongiovi, Alessandro .
APPLIED ACOUSTICS, 2007, 68 (11-12) :1323-1345
[5]  
Darvish M, FAN 2012 INT C FAN N, P18
[6]   Numerical and Experimental Study on the Tonal Noise Generation of a Radial Fan [J].
Darvish, Manoochehr ;
Frank, Stefan ;
Paschereit, Christian Oliver .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2015, 137 (10)
[7]   PROPELLER NOISE-REDUCTION BY MEANS OF UNSYMMETRICAL BLADE-SPACING [J].
DOBRZYNSKI, W .
JOURNAL OF SOUND AND VIBRATION, 1993, 163 (01) :123-136
[8]   REDUCTION OF INTERACTION TONES FROM AXIAL-FLOW FANS BY SUITABLE DESIGN OF ROTOR CONFIGURATION [J].
DUNCAN, PE ;
DAWSON, B .
JOURNAL OF SOUND AND VIBRATION, 1974, 33 (02) :143-154
[9]   NOISE REDUCTION BY APPLYING MODULATION PRINCIPLES [J].
EWALD, D ;
PAVLOVIC, A ;
BOLLINGER, JG .
JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 1971, 49 (05) :1381-+
[10]   REDUCTION OF BLADE PASSAGE TONE BY ANGLE MODULATION [J].
FIAGBEDZI, YA .
JOURNAL OF SOUND AND VIBRATION, 1982, 82 (01) :119-129