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涡轴发动机动力涡轮转子失去负载转速预测

龚立锋 熊清勇 罗明志 付秋菊

龚立锋, 熊清勇, 罗明志, 付秋菊. 涡轴发动机动力涡轮转子失去负载转速预测[J]. 航空动力学报, 2021, 36(2): 352-357. doi: 10.13224/j.cnki.jasp.2021.02.013
引用本文: 龚立锋, 熊清勇, 罗明志, 付秋菊. 涡轴发动机动力涡轮转子失去负载转速预测[J]. 航空动力学报, 2021, 36(2): 352-357. doi: 10.13224/j.cnki.jasp.2021.02.013
GONG Lifeng, XIONG Qingyong, LUO Mingzhi, FU Qiuju. Speed prediction for power turbine rotors of turboshaft engine on loss-of-load[J]. Journal of Aerospace Power, 2021, 36(2): 352-357. doi: 10.13224/j.cnki.jasp.2021.02.013
Citation: GONG Lifeng, XIONG Qingyong, LUO Mingzhi, FU Qiuju. Speed prediction for power turbine rotors of turboshaft engine on loss-of-load[J]. Journal of Aerospace Power, 2021, 36(2): 352-357. doi: 10.13224/j.cnki.jasp.2021.02.013

涡轴发动机动力涡轮转子失去负载转速预测

doi: 10.13224/j.cnki.jasp.2021.02.013

Speed prediction for power turbine rotors of turboshaft engine on loss-of-load

  • 摘要: 为满足发动机适航规章CCAR33.27对涡轮失去负载时转子完整性的设计要求,研究涡轮失去负载瞬间转速随时间变化规律。采用多点稳态法对动力涡轮超转瞬时气动效率与转速对应关系进行研究,在此基础上,假设动力涡轮进口燃气能量不变,进而分析动力涡轮扭矩与转速的变化关系。然后采用理论力学和工程分析相结合的方法建立了动力涡轮失去负载瞬间转子转速随时间变化预测模型,并采用整机试验数据对该模型进行了验证,证明了该预测模型的合理性和准确性,建立的预测模型可为动力涡轮强度和超转保护设计提供理论依据。研究结果表明,动力涡轮转子失去负载后转速在200~300 ms上升至160%,接近大部分轮盘破裂转速,需要在涡轴发动机超转保护设计中引起足够重视。

     

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出版历程
  • 收稿日期:  2020-06-07
  • 刊出日期:  2021-02-28

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