journal article·2016-06

An optimal volute spiral case design for centrifugal fan: theoretical and experimental studies

Cheng-Hung Huang, Wei-Cheng Tseng

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Abstract

An inverse design problem in determining the optimal shape of volute spiral case for a centrifugal-flow fan is examined in the present study using the Levenberg–Marquardt method and a general purpose commercial code CFD-ACE+, and based on a desired airflow rate. The desired volume airflow rate can be obtained by multiplying the airflow rate of an existing fan by a constant number which is >1. The shape of the redesigned volute case is generated using the equation of the trajectory of fluid particles in the volute, which enables the shape of the fan volute be constructed completely. Finally, prototypes of the original and optimized fan volutes as well as fan impellers are fabricated, thereafter the fan performance is tested based on the AMCA-210-85 standard to verify the validity of the design. The experimental results demonstrate that by utilizing the fabricated centrifugal optimal fan and operating at the design condition, the airflow rate can be increased by 6.5 % and the pressure drop, noise and input power of fan can be reduced by 1.6, 5.3 and 11.4 %, respectively, when compared with the original fan. As a result, the performance of optimal fan can be improved greatly.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Turbomachinery Performance and Optimization · Heat Transfer Mechanisms · Fluid Dynamics and Turbulent Flows

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (14)

Show source-provided references
1. CFD-ACE+ User’s Manual. ESI-CFD Inc., Huntsville (2005)
2. Demeulenaere, A., Van den Braembussche, R.: Three-dimensional inverse method for turbomachinery blading design. ASME J. Turbomach. 120, 247–255 (1998)10.1115/1.2841399 ↗
3. Dilin, P.A.: Computational and experimental evaluation of the performance of a centrifugal fan volute. Proc. Inst. Mech. Eng. Part A J. Power Energy 212, 235–243 (1998)10.1243/0957650981536763 ↗
4. Gardow, E.B.: On the Relationship Between Impeller Exit Velocity Distribution and Blade Channel Flow in a Centrifugal Fan. Ph.D. thesis, State University of New York at Buffalo (1968)
5. Huang, C.H., Hung, M.H.: An optimal design algorithm for centrifugal fan: theoretical and experimental studies. J. Mech. Sci. Techonol. 27, 761–773 (2013)10.1007/s12206-013-0126-7 ↗
6. Huang, C.K., Hsieh, M.E.: Performance analysis and optimized design of backward-curved airfoil centrifugal blowers. HVAC&R Res. 15, 461–488 (2009)10.1080/10789669.2009.10390846 ↗
7. Kim, J.S., Park, W.G.: Optimized inverse design method for pump impeller. Mech. Res. Commun. 27, 465–473 (2000)10.1016/S0093-6413(00)00119-1 ↗
8. Laboratory Method of Testing Fans Rating, American National Standard, Air Movement and Control Association, Inc., ANSI/AMCA standard 210 (1985)
9. Lin, S.C., Huang, C.L.: The study of a small centrifugal fan for a notebook computer. In: The 8th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, Honolulu, HI, USA, pp. 247–256 (2000)
10. Lv, Y.K., Song, B.J., Liu, H.F.: Analysis and suggestion on design methods for volute shape of centrifugal fans. Adv. Mater. Res. 550–53, 3117–3120 (2012)10.4028/www.scientific.net/AMR.550-553.3117 ↗
11. Marquardt, D.M.: An algorithm for least-squares estimation of nonlinear parameters. J. Soc. Ind. Appl. Math 11, 431–441 (1963)10.1137/0111030 ↗
12. Zangeneh, M.: Inviscid-viscous interaction method for 3d inverse design of centrifugal impellers. ASME J. Turbomach. 116, 280–290 (1994)10.1115/1.2928362 ↗
13. Zhang, L., Wang, S.L., Wu, D.F., Zhang, Q.: Numerical study for centrifugal fan based on parametric method. Appl. Mech. Mater. 55–57, 892–897 (2011)
14. Zhou, J.H., Yang, C.X.: Parametric design and numerical simulation of the axial-flow fan for electronic devices. IEEE Trans. Compon. Packag. Technol. 33, 287–298 (2010)10.1109/TCAPT.2010.2040069 ↗