Detection of Blade Mistuning in a Low Pressure Turbine Rotor Resulting from Manufacturing Tolerances and Differences in Blade Mounting
Detection of Blade Mistuning in a Low Pressure Turbine Rotor Resulting from Manufacturing Tolerances and Differences in Blade Mounting
关键词
涡轮转子叶片
制造公差
低压涡轮
检测
失谐
测振系统
测量过程
振动特性
Mistuning, modal characteristics, low pressure turbine, rotor blading, numerical and experimental modal analysis.
参考文献29
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1SchSnenbom, H., Retze, U., Ziller, G., and Waniczek, P. 2010. "Experimental and Analytical Mistuning Analysis of a Blisk at Lab Conditions and under Rig Conditions Using Tip Timing." In Proceedings of the ASME TurboExpo, 855-64.
-
2Ewins, D. 2009. "The Mistuned Blade Vibration Problem Re-visited." In Proceedings of the 12th International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines, 323-4.
-
3Ewins, D. 1991. "The Effect of Blade Misaming on Vibration Response---A Survey." Presented at the IFToMM 4th International Conference on Rotordynamics, Prague.
-
4Castanier, M., and Pierre, C. 2006. "Modeling and Analysis of Mistuned Bladed Disk Status and Emerging Directions." Journal of Propulsion and Power 22 (2): 384-96.
-
5Chan, Y. J. 2009. "Variability of Blade Vibration in Mistuned Bladed Discs." Ph.D. thesis, Imperial College.
-
6Khemiri, O., Martel, C., and Corral, R. 2014. "Forced Response of Mistuned Bladed Disks: Quantitative Validation of the Asymptotic Description." Journal of Propulsion andPower 30 (2): 397-406.
-
7Martel, C., Corral, R., and Llorens, J. 2008. "Stability Increase of Aerodynamically Unstable Rotors Using Intentional Mistuning." Journal of Turbomachinery 130 (1): O11006.
-
8Martel, C., and Corral, R. 2009. "Asymptotic Discribtion of Maximum Mistuning Amplification of Bladed Disk Forced Response." Journal of Engineering for Gas Turbines and Power 131: 022506.
-
9Sinha, A. 1997. "Computation of the Maximum Amplitude of a Mistuned Bladed Disk Assembly via Infinity Norm." In Proceedings of the ASME International Mechanical Engineering Congress and Exposition, 427-32.
-
10Whitehead, D. 1996. "Effect of Mistuning on the Vibration of Turbomachine Blades Induced by Wakes." Journal of Mechanical Engineering Science 8 (1): 15 -21.
-
1Cros.,JE,纪丽伟.制造公差和圆角半经对气缸体上气缸套支承处应力的影响[J].柴油机设计与制造,1989(2):62-66.
-
2金绍忠,程普强.确定航空轮胎与相邻结构间隙的方法研究[J].飞机工程,2003(3):39-43.
-
3Infantino Daniele,Satta Francesca,Simoni Daniele,Ubaldi Marina,Zunino Pietro,Bertini Francesco.Experimental Analysis of the Aerodynamic Performance of an Innovative Low Pressure Turbine Rotor[J].Journal of Thermal Science,2016,25(1):22-31.
-
4赵丽滨,山美娟,彭雷,季少华,贾西文,徐吉峰.制造公差对复合材料螺栓连接结构强度分散性的影响[J].复合材料学报,2015,32(4):1092-1098. 被引量：8
-
5Bian Ji.10 Differences between Shenzhou 8 and Shenzhou 9 Missions[J].Aerospace China,2012,13(3):4-5.
-
6李凡,杨权,等.批生产及翻修发动机稳定性检查研究[J].红旗技术,2001(4):3-10.
-
7应财德.大型涡轮转子叶片熔模精铸特点[J].机械,1995,22(2):31-32. 被引量：1
-
8Bian Ji.Major Differences between Chang'e 2 and Chang'e 1 Satellites[J].Aerospace China,2010,11(4):8-9.
-
9朱永平,程岩,苏黎,李凌.N100-90/535 型汽轮机高压缸通流部分改造[J].云南电力技术,1998,26(4):16-19. 被引量：2
-
10蒋有年.编制飞机制造用工艺装备公差分配行业标准的探讨[J].航空标准化与质量,1992(4):13-15.
