2021
DOI: 10.3390/machines9090189
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A Vibration Suppression Method for the Multistage Rotor of an Aero-Engine Based on Assembly Optimization

Abstract: The assembly quality of the multistage rotor is an essential factor affecting its vibration level. The existing optimization methods for the assembly angles of the rotors at each stage can ensure the concentricity and unbalance meet the requirements, but it cannot directly ensure its vibration responses meet the indexes. Therefore, in this study, we first derived the excitation formulas of the geometric and mass eccentricities on the multistage rotor and introduced it into the dynamics model of the multistage … Show more

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Cited by 7 publications
(5 citation statements)
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“…Saldarriaga and Steffen [33], Mohammadzadeh and Ghoddoosian [34], and Yao et al [35] dealt with balancing the rotors based on the utilization of different optimization methods. Chen et al [36] used an optimization technique for increasing the efficiency of vibration attenuation of an aero-engine rotor.…”
Section: Introductionmentioning
confidence: 99%
“…Saldarriaga and Steffen [33], Mohammadzadeh and Ghoddoosian [34], and Yao et al [35] dealt with balancing the rotors based on the utilization of different optimization methods. Chen et al [36] used an optimization technique for increasing the efficiency of vibration attenuation of an aero-engine rotor.…”
Section: Introductionmentioning
confidence: 99%
“…One of the core problems currently limiting the development of the engine is the vibration of the rotor structure when rotating at high speed. According to the statistics, the number of engine failures caused by vibration accounts for 50% to 60% of the total number of engine failures [1]. It has been proven that rotor unbalance is the main factor that generates vibration during the operation of an aero engine [2].…”
Section: Introductionmentioning
confidence: 99%
“…The current process for optimizing balance in aero engine assembly plants has the following main problems: (1) The blade sorting process only considers flushness and randomly selects pieces from the blades according to the blade code. Due to the blade manufacturing error with individual differences, randomly selected parts not only cause assembly quality dispersion, but poor connection performance consistency and often need to be repeatedly disassembled and adjusted to meet the assembly balance requirements, resulting in low assembly efficiency and high cost due to its "trial and error" nature.…”
Section: Introductionmentioning
confidence: 99%
“…It is a typical multistage disk structure. The unbalance is the result of the superposition of unbalance vectors distributed on every single piece [6]. The changing and coupled assembly processes lead to the following difficulties in predicting low-pressure rotor unbalance during assembly:…”
Section: Introductionmentioning
confidence: 99%