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航空发动机寿命限制件工作边界系统级分析模型

丁水汀 邱天

丁水汀, 邱天. 航空发动机寿命限制件工作边界系统级分析模型[J]. 航空动力学报, 2013, 28(7): 1666-1674.
引用本文: 丁水汀, 邱天. 航空发动机寿命限制件工作边界系统级分析模型[J]. 航空动力学报, 2013, 28(7): 1666-1674.
DING Shui-ting, QIU Tian. Systematic model for operating boundary analysis of aero-engine life limited parts[J]. Journal of Aerospace Power, 2013, 28(7): 1666-1674.
Citation: DING Shui-ting, QIU Tian. Systematic model for operating boundary analysis of aero-engine life limited parts[J]. Journal of Aerospace Power, 2013, 28(7): 1666-1674.

航空发动机寿命限制件工作边界系统级分析模型

基金项目: 教育部长江学者创新团队“航空发动机复杂系统安全性”(IRT0905);国家自然科学基金(61104146)

Systematic model for operating boundary analysis of aero-engine life limited parts

  • 摘要: 针对提高航空发动机系统安全性的迫切需求,以发动机本质特征和探索性研究成果为依据,分析了寿命限制件工作边界系统级分析模型(systematic model for engine life limited parts operating boundary analysis,SMELLIPOBA)的必要属性及各属性对应的技术基础,总结了相关技术基础领域的研究进展,介绍了SMELLIPOBA的发展现状,展望了这一领域未来研究方向.得出如下结论:满足适航性设计需求的SMELLIPOBA需具备耦合性、动态性、不确定性、学科交叉、多尺度等属性,未来SMELLIPOBA的发展仍将以上述属性为主线.

     

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  • 收稿日期:  2012-07-09
  • 刊出日期:  2013-07-28

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