| Citation: | XU Feng, MA Yan-hong, ZHANG Li, HONG Jie. Non-deformability evaluation of aero-engine's case[J]. Journal of Aerospace Power, 2016, 31(8): 1921-1928. doi: 10.13224/j.cnki.jasp.2016.08.017 |
| [1] |
Wu R W H,Witmer E A.Approximate analysis of containment/deflection ring responses to engine rotor fragment impact[J].Journal of Aircraft,1973,10(1):28-37.
|
| [2] |
European Aviation Safety Agency.CS-E Initial issue certification specifications for engines[S].Cologne,German:European Aviation Safety Agency,2009:11-13.
|
| [3] |
国防科学技术工业委员会.GJB241/87航空涡轮喷气和涡轮风扇发动机通用规范[S].北京:航空工业部三〇一所,1987:56-57.
|
| [4] |
国防科学技术工业委员会.GJB/Z 101航空发动机结构完整性指南[S].北京:中国航空工业总公司,1997:34-35.
|
| [5] |
秦丽晔,吴素君,赵海涛,等.航空发动机机匣损伤容限评估及剩余寿命预测[J].北京航空航天大学学报, 2011,37(7):895-900. QIN Liye,WU Sujun,ZHAO Haitao,et al.Determination of damage tolerance and remaining life for aeroengine crankcase[J].Journal of Beijing University of Aeronautics and Astronautics,2011,37(7):895-900.(in Chinese)
|
| [6] |
何俊杰,蔚夺魁,张德平.某型燃气轮机内、外机匣振动传递的动力学分析[J].航空发动机,2009,35(2):34-36,12. HE Junjie,YU Duokui,ZHANG Deping.Dynamics analysis of vibration transmission for inner and outer cases of a gas turbine[J].Aeroengine,2009,35(2):34-36,12.(in Chinese)
|
| [7] |
赵文涛,陈果,李琼,等.航空发动机机匣支承动刚度有限元计算及验证[J].航空计算技术,2011,41(5):34-38,41. ZHAO Wentao,CHEN Guo,LI Qiong,et al.Finite element modeling and experiment verification of dynamic stiffness of casing bearing in aircraft engine[J].Aeronautical Computing Technique,2011,41(5):34-38,41.(in Chinese)
|
| [8] |
《航空发动机设计手册》总编委会.航空发动机设计手册:第17册载荷及机匣承力件强度分析[M].北京:航空工业出版社,2001:387-392.
|
| [9] |
王海涛.某型航空发动机整机振动特性分析[D].南京:南京航空航天大学,2010. WANG Haitao.Research on whole body vibration of aero-engine[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2010.(in Chinese)
|
| [10] |
张本斌.某型航空发动机轴承机匣使用变形问题分析[J].装备制造技术,2006(3):92-93. ZHANG Benbin.Deflection analysis on bearing case of aero engine[J].Equipment Manufacturing Technology,2006(3):92-93.(in Chinese)
|
| [11] |
任兴民,顾家柳.转子机匣系统的瞬态动力响应计算[J].西北工业大学学报,1996,14(2):234-238. REN Xingmin,GU Jialiu.On improved calculation of transient dynamic response of rotor-stator system[J].Journal of Northwestern Polytechnical University,1996,14(2):234-238.(in Chinese)
|
| [12] |
张大义,母国新,洪杰.航空发动机转子支承系统刚度计算中的几个问题[J].战术导弹技术,2005(2):20-23. ZHANG Daying,MU Guoxin,HONG Jie.Rigidity calculation methods for rotor supporting system in gas engine[J].Tactical Missile Technology,2005(2):20-23.(in Chinese)
|
| [13] |
史海秋,赵福星.某型发动机承力机匣疲劳载荷谱研究[J].燃气涡轮试验与研究,2005,18(1):41-44. SHI Haiqiu,ZHAO Fuxing.Loading spectrum study of aeroengine cases[J].Gas Turbine Experiment and Research,2005,18(1):41-44.(in Chinese)
|
| [14] |
Jay A,Todd E S.Effect of flight loads on turbofan engine performance deterioration[R].NASA-TM-79041,1978.
|
| [15] |
Olsson W J,Martin R L.B747/JT9D flight loads and their effect on engine running clearances and performance deterioration[R].NASA-CR-165573,1982.
|
| [16] |
Husband J B.Developing an efficient FEM structural simulation of a fan blade off test in a turbofan jet engine[D].Saskatchewan,Canada:University of Saskatchewan 2007.
|
| [17] |
蔡显新,肖新红,王涛,等.风扇机匣的减振优化设计[J].航空动力学报,2010,25(2):396-401. CAI Xianxin,XIAO Xinhong,WANG Tao,et al.Optimization design of a fan casing for reducing vibration[J].Journal of Aerospace Power,2010,25(2):396-401.(in Chinese)
|
| [18] |
高金海,洪杰.航空发动机整机动力特性建模技术研究[J].战术导弹技术,2006(3):29-35. GAO Jinhai,HONG Jie.Study of modeling technique for dynamic characteristics of engine casing[J].Tactical Missile Technology,2006(3):29-35.(in Chinese)
|