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前后可调变弯度导叶在高负荷风扇中的应用

雷鹏 金东海 桂幸民

雷鹏, 金东海, 桂幸民. 前后可调变弯度导叶在高负荷风扇中的应用[J]. 航空动力学报, 2019, 34(1): 177-188. doi: 10.13224/j.cnki.jasp.2019.01.020
引用本文: 雷鹏, 金东海, 桂幸民. 前后可调变弯度导叶在高负荷风扇中的应用[J]. 航空动力学报, 2019, 34(1): 177-188. doi: 10.13224/j.cnki.jasp.2019.01.020
Application of variable inlet guide vane with adjustable front and back vane parts in highly loaded fan[J]. Journal of Aerospace Power, 2019, 34(1): 177-188. doi: 10.13224/j.cnki.jasp.2019.01.020
Citation: Application of variable inlet guide vane with adjustable front and back vane parts in highly loaded fan[J]. Journal of Aerospace Power, 2019, 34(1): 177-188. doi: 10.13224/j.cnki.jasp.2019.01.020

前后可调变弯度导叶在高负荷风扇中的应用

doi: 10.13224/j.cnki.jasp.2019.01.020
基金项目: 国家自然科学基金(51236001);国家重点基础研究发展计划(2012CB720201);北京市自然科学基金(3151002)

Application of variable inlet guide vane with adjustable front and back vane parts in highly loaded fan

  • 摘要: 针对某高负荷双级风扇非设计转速裕度不足的问题,通过NUMECA三维(CFD)数值模拟软件,对比分析了可变弯度导叶(VIGV)前后可偏转调节对导叶气动性能的影响,以及导叶大角度范围内变弯度调节对提高风扇中低转速性能的作用。结果表明:可变弯度导叶偏转调节后的叶型实际弯角是影响导叶气动损失的重要因素之一;通过导叶前段适当变角度调节能减小导叶的实际弯角,推迟了导叶吸力面气流分离的出现,拓宽了变弯度导叶低损失可调角度范围;同时导叶适当的前后偏转调节能够降低导叶对缝隙位置的敏感性;此外前后可调变弯度导叶能够使高负荷风扇非设计工况实现更高的绝热效率,在90%转速、80%转速、70%转速和60%转速下的风扇绝热效率分别提高了2.04%、5.48%、6.18%和6.82%;且由于风扇喘振边界进一步远离风扇阀门线,使得风扇中低转速的稳定工作范围显著拓展。

     

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出版历程
  • 收稿日期:  2017-11-27
  • 刊出日期:  2019-01-28

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