| [1] |
孟憬非,黄庆南,赵光电,等.某型发动机新件涡轮叶片叶冠掉块故障分析[J].航空发动机,2006,32(2):17-22. MENG Jingfei,HUANG Qingnan,ZHAO Guangdian,et al.Failure analysis of turbine blade shroud loss for an aeroengine[J].Aeroengine,2006,32(2):17-22.(in Chinese)
|
| [2] |
李桂英,闻雪友,李东明,等.燃气轮机带冠涡轮动叶故障分析及改进[J].热能动力工程,2008,23(1):28-31. LI Guiying,WEN Xueyou,LI Dongming,et al.Failure analysis and improving of turbine blade with shroud for a gas turbine[J].Journal of Engineering for Thermal Energy and Power,2008,23(1):28-31.(in Chinese)
|
| [3] |
《航空发动机设计手册》总编委会.航空发动机设计手册(第10册):涡轮[M].北京:航空工业出版社,2001.
|
| [4] |
汤凤,孟光.带冠涡轮叶片的接触分析[J].噪声与振动控制,2005(4):5-7,17. TANG Feng,MENG Guang.Contact analysis of shrouded turbine blade[J].Noise and Vibration Control,2005(4):5-7,17.(in Chinese)
|
| [5] |
郑君,罗贵火.某型发动机涡轮盘片叶冠有限元边界条件的计算对比分析[J].振动工程学报,2004,17(增刊):110-112. ZHENG Jun,LUO Guihuo.Finite element method contrast and analysis of turbine with different blases’ boundary conditions[J].Journal of Vibration Engineering,2004,17(supl.):110-112.(in Chinese)
|
| [6] |
朱永新.带冠叶片摩擦减振特性研究 .南京:南京航空航天大学,2007. ZHU Yongxin.Research on characteristic of the forced response of shrouded blades .Nanjing:Nanjing University of Aeronautics and Astronautics,2007.
|
| [7] |
杨鑫.带冠涡轮叶片动力响应设计技术研究 .北京:北京航空航天大学,2008. YANG Xin.Study on design technology of dynamic response of shrouded turbine blade .Beijing:Beijing University of Aeronautics and Astronautics,2008.
|
| [8] |
Porreca L,Kalfas A I,Abhari R S.Optimized shroud design for axial turbine aerodynamic performance[J].Journal of Turbomachinery,2008,130(3):031016.1-031016.12.
|
| [9] |
Porreca L,Behr T,Schlienger J,et al.Fluid dynamics and performance of partially and fully shrouded axial turbines[J].Journal of Turbomachinery,2005,127(4):668-678.
|
| [10] |
田文正,王荣桥.基于MDO体系的涡轮叶片热-结构耦合分析[J].航空发动机,2008,34(2):5-9,12. TIAN Wenzheng,WANG Rongqiao.Coupled thermal-structural analysis of turbine blade based on MDO system[J].Aeroengine,2008,34(2):5-9,12.(in Chinese)
|
| [11] |
蔡显新,尹泽勇,高德平.航空发动机涡轮叶片的多学科设计优化[J].航空动力学报,2004,20(5):795-801. CAI Xianxin,YIN Zeyong,GAO Deping.MDO technology applied to the aeroengine turbine blade design[J].Journal of Aerospace Power,2004,20(5):795-801.(in Chinese)
|
| [12] |
EGD-3斯贝MK202发动机应力标准[M].丁爱祥,吴君,译.北京:国际航空编辑部,1979.
|