According to the assembly process parameters features of turbine supports of an aero-engine
the vibration characteristics in a rotor system with different assembly process parameters between an outer ring of the bearing and a casing were carried out experimentally. The parameters of assembly process of a bearing outer ring were interference fit
clearance fit and transition fit. The influence on the fit of bearing outer ring and vibration of the rotor caused by casing temperature field and outer ring tinghtening torque were also carried out. The results show that: when assembly process of a bearing outer ring is clearance fit
subharmonic
super-subharmonic frequencys
nonlinear resonances occur and outer ring tightening torque in increases is one of the main factors that suppress rotor vibration. Assembly relationship of bearing out ring from the transition to the clearence occurs which is caused by temperature field of the casing.
Analysis of thermal characteristics of oil⁃cooled aviation wet friction clutch
Experimental investigation on contact thermal resistance characteristics of aero⁃engine flange
Thermal characteristics for bearing combined EHL theory with CFD method
Clamp assembly stress test of aero-engine and assembly parameter control method
Fretting wear of discontinuous interface considering centrifugal force and thermal stress
Related Author
Heyun BAO
Weidi KONG
Wuzhong TAN
Wei HUANG
Rupeng ZHU
Yan CHEN
Guangya FAN
Zhihui LIN
Related Institution
National Key Laboratory of Science and Technology on Helicopter Transmission, Nanjing University of Aeronautics and Astronautics
National Key Laboratory of Science and Technology on Helicopter Transmission,Hunan Aviation Powerplant Research Institute,Aero Engine Corporation of China
Shaanxi Key Laboratory of Thermal Science in Aero⁃engine System,Northwestern Polytechnical University
Commercial Aircraft Engine Company Limited,Aero Engine Corporation of China
School of Power and Energy,Northwestern Polytechnical University