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涡轮盘概率风险的评估方法

孙杨慧 杨坤 侯乃先 陈健 白国娟

孙杨慧, 杨坤, 侯乃先, 陈健, 白国娟. 涡轮盘概率风险的评估方法[J]. 航空动力学报, 2016, 31(9): 2195-2202. doi: 10.13224/j.cnki.jasp.2016.09.019
引用本文: 孙杨慧, 杨坤, 侯乃先, 陈健, 白国娟. 涡轮盘概率风险的评估方法[J]. 航空动力学报, 2016, 31(9): 2195-2202. doi: 10.13224/j.cnki.jasp.2016.09.019
SUN Yang-hui, YANG Kun, HOU Nai-xian, CHEN Jian, BAI Guo-juan. Probabilistic risk assessment method for turbine disk[J]. Journal of Aerospace Power, 2016, 31(9): 2195-2202. doi: 10.13224/j.cnki.jasp.2016.09.019
Citation: SUN Yang-hui, YANG Kun, HOU Nai-xian, CHEN Jian, BAI Guo-juan. Probabilistic risk assessment method for turbine disk[J]. Journal of Aerospace Power, 2016, 31(9): 2195-2202. doi: 10.13224/j.cnki.jasp.2016.09.019

涡轮盘概率风险的评估方法

doi: 10.13224/j.cnki.jasp.2016.09.019
详细信息
    作者简介:

    孙杨慧(1985-),女,江苏徐州人,工程师,博士,主要从事航空发动机系统安全性与结构可靠性研究.

  • 中图分类号: V231.91

Probabilistic risk assessment method for turbine disk

  • 摘要: 针对CCAR33.70条款对涡轮盘开展概率风险评估的要求,研究了响应面法在定义重点采样区间以及计算裂纹扩展寿命中的应用,给出了在蒙特卡洛模拟过程中应用响应面法定义失效域,缩短样本方差、提高抽样效率的方法.分析结果表明应用重点采样法可以极大地提高抽样效率.采用重点采样法获得的失效样本数与总样本数的比例高达94%,远大于传统的直接抽样法获得的失效样本数与总样本数的比例(仅为33%).该方法可以在保证分析精度的条件下减少样本的数量.另外,应用响应面法拟合寿命近似方程,可以极大地缩减裂纹扩展寿命的计算时间:利用寿命近似方程开展104次随机抽样所花费的时间仅有2min,远低于应用传统寿命计算方法所花费的时间(288 min).通过对寿命近似方程的寿命计算误差分析可以看出:最大计算误差仅有1.0%,计算结果与传统裂纹扩展寿命模型的计算结果吻合度高.该研究成果可以提高涡轮盘概率风险评估的效率.

     

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出版历程
  • 收稿日期:  2015-05-07
  • 刊出日期:  2016-09-28

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