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基于葉片彎掠技術(shù)的優(yōu)化設(shè)計(jì)

來源:新能源網(wǎng)
時(shí)間:2018-09-04 23:21:37
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基于葉片彎掠技術(shù)的優(yōu)化設(shè)計(jì)  摘要在三維粘性流場的數(shù)值計(jì)算程序平臺(tái)上,利用BP神經(jīng)網(wǎng)絡(luò)和遺傳算法,通過葉片彎掠技術(shù)對(duì)一軸流風(fēng)機(jī)的轉(zhuǎn)子葉片的周向彎曲角度進(jìn)行尋優(yōu),以使風(fēng)扇的氣動(dòng)性能進(jìn)

  摘要在三維粘性流場的數(shù)值計(jì)算程序平臺(tái)上,利用BP神經(jīng)網(wǎng)絡(luò)和遺傳算法,通過葉片彎掠技術(shù)對(duì)一軸流風(fēng)機(jī)的轉(zhuǎn)子葉片的周向彎曲角度進(jìn)行尋優(yōu),以使風(fēng)扇的氣動(dòng)性能進(jìn)一步提高。通過對(duì)比優(yōu)化前、后的葉輪發(fā)現(xiàn),優(yōu)化之后的葉片呈現(xiàn)明顯的周向前彎曲特征。測試結(jié)果顯示,其全壓和氣動(dòng)效率分別提高了3.56%和1.27%,失速裕度大幅度拓寬36%以上,上、下端部的損失進(jìn)一步降低。

  關(guān)鍵詞周向前彎葉片,人工神經(jīng)網(wǎng)絡(luò),遺傳算法,優(yōu)化設(shè)計(jì)

  中圖分類號(hào)TH432.1 文獻(xiàn)標(biāo)識(shí)碼A

  

  Optimization Design based on Skewed and Swept Blade TechniqueLI Yang OU YANG-Hua DU Zhao-Hui

 ?。═urbomachinery Laboratory of Shanghai Jiaotong University, Shanghai 200030, China)

  Abstract based on a program for solving 3D viscous flow fields, an aerodynamic optimization design was conducted to the rotor blade (archetypal rotor blade) of anaxial flow fan with back-propagation neural network andgenetic algorithm. By skewed and swept blade technique, the optimized rotor blade having better aerodynamic performance is obtained. The results show that the optimized rotor blade is circumferential forward-skewed blade. Compared with the archetypal rotor blade, the total pressure rise and the total pressure efficiency of the optimized rotor are increased by 3.56% and 1.27% respectively. Its stall margin is greatly extended by more than 36%. At the same time, the loss in the upper and lower endwalls of the fan is reduced further.中國風(fēng)電材料設(shè)備網(wǎng)

  Key words Circumferential forward-skewed blade; Artificial Neural Network (ANN); Genetic Algorithm (GA); Optimization design

  1前言

  隨著計(jì)算機(jī)技術(shù)和各種尋優(yōu)算法的不斷發(fā)展,在葉輪機(jī)械領(lǐng)域,利用某些算法進(jìn)行葉片的優(yōu)化設(shè)計(jì)來提高葉輪的性能已經(jīng)成為可能。許多學(xué)者利用遺傳算法、模擬退火法、梯度法、響應(yīng)面法等對(duì)各種葉輪的靜子和轉(zhuǎn)子葉型進(jìn)行了優(yōu)化設(shè)計(jì),結(jié)果顯示,通過一些優(yōu)化方法可以進(jìn)一步地提高葉輪的效率,改善葉片表面的壓力分布,降低了邊界層的流動(dòng)損失,同時(shí)也縮短了設(shè)計(jì)周期【1-7】。

  然而,當(dāng)前的優(yōu)化設(shè)計(jì)多是針對(duì)改進(jìn)二維葉型,對(duì)于能夠減小葉輪的內(nèi)部流動(dòng)損失、提高氣動(dòng)效率最為重要的手段之一的彎掠葉片技術(shù)【8-10】,在葉片優(yōu)化計(jì)算中應(yīng)用的公開報(bào)告還比較少。

  本文利用雷諾平均N-S方程組數(shù)值計(jì)算程序,基于人工神經(jīng)網(wǎng)絡(luò)BP算法和遺傳算法的數(shù)值優(yōu)化程序,基于葉片彎掠技術(shù)對(duì)一軸流風(fēng)扇轉(zhuǎn)子葉片進(jìn)行了優(yōu)化設(shè)計(jì),通過尋找合適的周向彎曲角度,來獲得具有最優(yōu)氣動(dòng)性能的風(fēng)扇葉片,并對(duì)優(yōu)化前、后的葉片在葉片形狀、氣動(dòng)性能以及出口流場進(jìn)行了對(duì)比分析。

  2研究模型