| Citation: | SHEN Xiu-li, ZHOU Ying-lu. Numerical calculation and analysis of arc tooth tenon joint[J]. Journal of Aerospace Power, 2012, 27(3): 610-616.
|
| [1] |
宋兆泓.航空燃气涡轮发动机强度设计[M].北京:北京航空航天大学出版社,2008.
|
| [2] |
Kosing O E,Scharl R,Shchmuhl H J.Design Improvements of the EJ200 HP compressor.ASME-2001-GT-0283,2001.
|
| [3] |
Meguid S A,Kanth P S,Czekanski A.Finite element analysis of fir-tree region in turbine discs[J].Finite Elements in Analysis and Design,2000,35(4):305-317.
|
| [4] |
SONG Wenbin,Keane A J.An efficient evolutionary optimisation framework applied to turbine blade firtree root local profiles[J].Structural Multidisciplinary Optimization,2005,29(5):382-390.
|
| [5] |
陈光.航空燃气涡轮发动机结构设计[M].北京:北京航空航天大学出版社,1988.
|
| [6] |
Sinclair G B,Cormier N G,Griffin J H,et al.Contact stresses in dovetail attachments:finite element modeling[J].Journal of Engineering for Gas Turbines and Power,2002,124(1):182-189.
|
| [7] |
Johnson.接触力学[M].徐秉业,罗学富,刘信声,译.北京:高等教育出版社,1992.
|
| [8] |
孙锡环,秦晓桐.烟气轮机盘榫槽部位的实验应力分析[J].北京理工大学学报,1996,16(4):361-366. SUN Xihuan,QIN Xiaotong.Stress analysis of experiment about mortise of flue gas turbine[J].Journal of Beijing Institute of Technology,1996,16(4):361-366.(in Chinese)
|
| [9] |
张如一.实验应力分析[M].北京:机械工业出版社,1982.
|
| [10] |
陈开军,马枚.航空发动机叶片榫头优化设计研究[J].航空动力学报,1995,10(2):190-192. CHEN Kaijun,MA Mei.Optimization of turbine blade fir-tree roots[J].Journal of Aerospace Power,1995,10(2):190-192.(in Chinese)
|
| [11] |
Song W,Keane A.Turbine blade fir-tree root design optimisation using intelligent CAD and finite element analysis[J].Computers and Structures,2002,80(24):1853-1867.
|
| [12] |
EGD-3斯贝MK202发动机应力标准[S].丁爱祥,吴君可,译.北京:国际航空编辑部,1979.
|
| [13] |
邢誉峰,诸德超.航空发动机涡轮盘榫槽的形状优化设计[J].航空学报,1995,16(4):488-491. XING Yufeng,ZHU Dechao.Shape optimization of aero engine disc groove[J].Acta Aeronautical et Astronautcia Sinica,1995,16(4):488-491.(in Chinese)
|
| [14] |
申秀丽,齐晓东.航空发动机涡轮榫接结构齿形基本参数研究[J].航空动力学报,2011,26(4):735-744. SHEN Xiuli,QI Xiaodong.Research of the basic parameters about tooth shape of tenon joint of aero engine turbine[J].Journal of Aerospace Power,2011,26(4):735-744.(in Chinese)
|
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