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可调高压导叶对1+1/2对转涡轮性能影响的数值研究

雒伟伟 张磊 王会社 徐建中

雒伟伟, 张磊, 王会社, 徐建中. 可调高压导叶对1+1/2对转涡轮性能影响的数值研究[J]. 航空动力学报, 2011, 26(12): 2741-2748.
引用本文: 雒伟伟, 张磊, 王会社, 徐建中. 可调高压导叶对1+1/2对转涡轮性能影响的数值研究[J]. 航空动力学报, 2011, 26(12): 2741-2748.
LUO Wei-wei, ZHANG Lei, WANG Hui-she, XU Jian-zhong. Effects of high-pressure guide vane adjustment on 1+1/2 counter-rotating turbine[J]. Journal of Aerospace Power, 2011, 26(12): 2741-2748.
Citation: LUO Wei-wei, ZHANG Lei, WANG Hui-she, XU Jian-zhong. Effects of high-pressure guide vane adjustment on 1+1/2 counter-rotating turbine[J]. Journal of Aerospace Power, 2011, 26(12): 2741-2748.

可调高压导叶对1+1/2对转涡轮性能影响的数值研究

基金项目: 国家自然科学基金重大研究计划(90718025); 国家重点基础研究发展计划(2010CB227302)

Effects of high-pressure guide vane adjustment on 1+1/2 counter-rotating turbine

  • 摘要: 对1+1/2对转涡轮高压导叶转动不同角度后不同落压比时的涡轮性能进行了数值计算和分析,获得了不同导叶开度和不同落压比对涡轮性能影响的关系曲线.结果表明,高压导叶转角的变化可以有效地调节1 1/2对转涡轮的流量;当导叶打开时,随着落压比的变化涡轮效率存在一个峰值,当导叶关闭时,涡轮效率随落压比的减小持续降低,并且降低的幅度更加明显;当涡轮压比较低时,导叶开大时的涡轮效率略高于导叶未动时的效率,并且随着落压比的进一步降低,差异更加明显,这与文献中常规涡轮导叶调整后涡轮效率均会降低明显不同;在保证效率和功量的前提下,高压导叶开大对于1 1/2对转涡轮高低压级出功比保持在合理范围内是有利的.

     

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出版历程
  • 收稿日期:  2010-12-22
  • 修回日期:  2011-05-13
  • 刊出日期:  2011-12-28

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