Finite element method for disc-rotor dynamic characteristics analysis of gas turbine rotor considering contact effects and rod preload

Author(s):  
Mingjian Lu ◽  
Haipeng Geng ◽  
Baisong Yang ◽  
Lie Yu
2002 ◽  
Vol 122 (2) ◽  
pp. 144-149 ◽  
Author(s):  
Tadashi Yamaguchi ◽  
Yoshihiro Kawase ◽  
Masataka Torizawa ◽  
Hirokazu Sekino ◽  
Kinya Matsuzawa

2020 ◽  
Vol 37 (1) ◽  
pp. 31-39 ◽  
Author(s):  
Jia Shengxi ◽  
Zheng Longxi ◽  
Jingjing Huang ◽  
Qing Mei

AbstractThe vibration optimum design for a simulated power turbine rotor without blades on the disk by using an optimization method based on the finite element method is described in this paper. The installation position of the two-stage turbine disks is chosen as design variables under the constraints of feasible regions for the critical speeds of the rotor. The objective functions are to minimize the transient response of the acceleration at the bearings and the amplitude of the disks. Predictions of the dynamic characteristics of the rotor are obtained by using ANSYS code. The optimization problem is solved by using commercial optimization code ISIGHT. The optimum installation position of the two-stage turbine disks is determined after optimization design. Experimental tests under the optimized structure show that the amplitude of the two-stage turbine disks which are recognized as the most concerned optimization objectives are reduced by 59 % and 56 % respectively in comparison with the comparative structure. The encouraging results demonstrate the potential of the presented method as an engineering design tool and also lay a foundation for the design of the real power turbine rotor used in turbo-shaft engine.


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