發(fā)布時(shí)間：2018-07-23 11:05

【摘要】：車載離心風(fēng)機(jī)要求結(jié)構(gòu)緊湊、重量輕、出口壓力相對(duì)較高,但傳統(tǒng)設(shè)計(jì)方法精度低、參數(shù)取值范圍大,往往不能滿足風(fēng)機(jī)優(yōu)化設(shè)計(jì)的要求,這就需要對(duì)離心風(fēng)機(jī)內(nèi)部微觀流動(dòng)進(jìn)行分析,提高風(fēng)機(jī)的設(shè)計(jì)精度。論文分析了目前風(fēng)機(jī)的設(shè)計(jì)方法以及理論研究現(xiàn)狀,以離心風(fēng)機(jī)為研究對(duì)象運(yùn)用SOLIDWORKS軟件建立了離心風(fēng)機(jī)的幾何模型,調(diào)入GAMBIT進(jìn)行網(wǎng)格化分和邊界條件設(shè)置,用FLUENT軟件對(duì)風(fēng)機(jī)流場(chǎng)進(jìn)行了數(shù)值計(jì)算,得到了風(fēng)機(jī)內(nèi)部流場(chǎng)分布,并研究了風(fēng)機(jī)結(jié)構(gòu)參數(shù)對(duì)風(fēng)機(jī)性能的影響。 通過(guò)研究表明,除葉片出口安裝角之外,葉片進(jìn)口安裝角對(duì)風(fēng)機(jī)性能的影響較顯著。在進(jìn)一步的研究中,分析了進(jìn)口安裝角、出口安裝角、葉輪寬度、蝸殼出口擴(kuò)壓角以及葉片數(shù)量等結(jié)構(gòu)參數(shù)對(duì)風(fēng)機(jī)的性能的影響。隨著葉片出口安裝角、葉輪寬度、葉片數(shù)的增加,風(fēng)機(jī)的全壓都增加;隨著風(fēng)機(jī)葉片進(jìn)口安裝角的增加,風(fēng)機(jī)全壓先增加,然后減小,存在一個(gè)極值;隨著蝸殼出口擴(kuò)壓角度的增大,風(fēng)機(jī)全壓有所增加,但當(dāng)擴(kuò)壓角超過(guò)一定值后全壓增加緩慢�；�于研究結(jié)果對(duì)風(fēng)機(jī)結(jié)構(gòu)進(jìn)行了優(yōu)化,對(duì)結(jié)構(gòu)優(yōu)化風(fēng)機(jī)流場(chǎng)的數(shù)值模擬結(jié)果顯示風(fēng)機(jī)設(shè)計(jì)合理、全壓達(dá)到使用要求,靜壓裕量為7.12%。論文研究結(jié)果為離心式通風(fēng)機(jī)的優(yōu)化設(shè)計(jì)提供了一定的理論依據(jù)和參考。
[Abstract]:Truck centrifugal fan requires compact structure, light weight, relatively high outlet pressure, but the traditional design method has low precision and wide range of parameters, so it can not meet the requirements of fan optimization design. In order to improve the design precision of centrifugal fan, it is necessary to analyze the micro flow inside the centrifugal fan. This paper analyzes the design method and the current research situation of the centrifugal fan. The geometry model of the centrifugal fan is established by using SOLIDWORKS software, and the grid division and boundary condition setting are carried out with gambit. The flow field of the fan is numerically calculated with fluent software, and the distribution of the flow field inside the fan is obtained, and the influence of the structure parameters of the fan on the performance of the fan is studied. The results show that the influence of blade inlet installation angle on fan performance is significant except for blade outlet mounting angle. In the further study, the influence of the structural parameters such as inlet installation angle, outlet installation angle, impeller width, volute outlet diffuser angle and the number of blades on the performance of the fan are analyzed. With the increase of blade outlet angle, impeller width and number of blades, the total pressure of the fan increases, and with the increase of the inlet angle of the fan blade, the total pressure of the fan first increases and then decreases, and there is an extreme value. With the increase of expanding angle at the outlet of volute, the total pressure of fan increases, but when the angle of expansion exceeds a certain value, the total pressure increases slowly. Based on the research results, the fan structure is optimized. The numerical simulation results of the fan flow field show that the fan design is reasonable, the full pressure meets the operational requirements, and the static pressure margin is 7.12. The research results provide some theoretical basis and reference for the optimization design of centrifugal fan.
【學(xué)位授予單位】：中國(guó)石油大學(xué)
【學(xué)位級(jí)別】：碩士
【學(xué)位授予年份】：2011
【分類號(hào)】：TH432

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本文編號(hào)：2139198