DocumentCode
3367796
Title
Centrifugal multi-wing type ventilator performance improvement and Numerical simulation
Author
Xiao-ming, Yu ; Jin-feng, Li
Author_Institution
Univ. of Shanghai for Sci. & Technol., Shanghai, China
fYear
2010
fDate
26-28 June 2010
Firstpage
3516
Lastpage
3519
Abstract
The existing and mature CFD technology is applied in this paper. Through the simulation of the prototype, it´s found that there are obvious vortices in the cochlea part of the centrifugal multi-wing type ventilator. Two schematic plans are adopt to improve efficiency of the centrifugal multi-wing type ventilator. These vortices can cause high energy loss. At the same time, they increase noise of the ventilator and affect efficiency. The first scheme is to increase radius of the cochlea. The second scheme is to change the cochlea into tilted. Some experiments of the velocity of outlet of the centrifugal multi-wing type ventilator also have been carried on which are in order to make some comparison. It can be found that unsuitable change of the cochlea radius caused more disorder airflow rather than improve the cochlea vortices. So the conclusion obtained is that the key issue is to find the suitable radius of the cochlea in design of the centrifugal multi-wing type ventilator. During the design of tilted cochlea, a satisfying outcome is obtained.
Keywords
aerospace components; aerospace computing; computational fluid dynamics; flow simulation; numerical analysis; ventilation; vortices; CFD; airflow disorder; centrifugal multiwing type ventilator performance improvement; cochlea vortices; numerical simulation; tilted cochlea; Blades; Computational fluid dynamics; Computational geometry; Costs; Energy loss; Impellers; Numerical simulation; Software tools; Testing; Virtual prototyping; airflow; multi-blades fan; numerical simulation; ventilation of air-conditioning;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechanic Automation and Control Engineering (MACE), 2010 International Conference on
Conference_Location
Wuhan
Print_ISBN
978-1-4244-7737-1
Type
conf
DOI
10.1109/MACE.2010.5536700
Filename
5536700
Link To Document